AERO B.E. Final Syllabus

SATHYABAMA UNIVERSITY(Established under section 3 of UGC Act, 1956)

Jeppiaar Nagar, Rajiv Gandhi Road, Chennai – 119.

SYLLABUSBACHELOR OF ENGINEERING PROGRAMME

INAERONAUTICAL ENGINEERING (8 SEMESTERS)

REGULATIONS 2010

SATHYABAMA UNIVERSITYREGULATIONS – 2010

Effective from the academic year 2010-2011 and applicable to the students admitted to the Degree of Bachelorof Engineering / Technology. (Eight Semesters)

1. Structure of Programme:

1.1 Every Programme will have a curriculum with syllabi consisting theory and practical such as:

(i) General core courses comprising Mathematics, Basic Sciences, Engineering Sciences.

(ii) Core course of Engineering / Technology.

(iii) Elective course for specialization in related fields.

(iv) Workshop practice, Computer Practice, Engineering Graphics, Laboratory Work, IndustrialTraining, Seminar Presentation, Project Work, Educational Tours, Camps etc.

1.2 Each semester curriculum shall normally have a blend of lecture courses not exceeding 7 andpractical courses not exceeding 4.

1.3 The medium of instruction, examinations and project report will be in English.

2. Duration of the Programme

A student is normally expected to complete the B.E/B.Tech. Programme in 8 semesters but in any case notmore than 12 consecutive semesters from the time of commencement of the course (not more than 10semesters for those who join 3rd semester under Lateral entry system) The Head of the Department shallensure that every teacher imparts instruction as per the number of hours specified in the syllabus and that theteacher teaches the full content of the specified syllabus for the course being taught.

3. Requirements for Completion of a Semester

A candidate who has fulfilled the following conditions shall be deemed to have satisfied the requirement forcompletion of a semester.

3.1 He/She secures not less than 90% of overall attendance in that semester.

3.2 Candidates who do not have the requisite attendance for the semester will not be permitted to writethe University Exams.

4. Examinations

The examinations shall normally be conducted between October and December during the odd semesters andbetween March and May in the even semesters. The maximum marks for each theory and practical course(including the project work and Viva Voce examination in the Eighth Semester) shall be 100 with the followingbreakup.

(i) Theory Courses

Internal Assessment : 20 Marks

University Exams : 80 Marks

(ii) Practical Courses

Internal Assessment : - -

University Exams : 100 Marks

SATHYABAMA UNIVERSITY FACULTY OF MECHANICAL ENGINEERING

B.E. (AERONAUTICAL ENGINEERING) i REGULATIONS 2010

5. Passing requirements:

(i) A candidate who secures not less than 50% of total marks prescribed for the course (For all coursesincluding Theory, Practicals and Project work) with a minimum of 35 marks out of 80 in the UniversityTheory Examinations, shall be declared to have passed in the Examination.

(ii) If a candidate fails to secure a Pass in a particular course, it is mandatory that he/she shall reappearfor the examination in that course during the next semester when examination is conducted in thatcourse. However the Internal Assessment marks obtained by the candidate in the first attempt shallbe retained and considered valid for all subsequent attempts.

6. Eligibility for the Award of Degree

A student shall be declared to be eligible for the award of the B.E/B.Tech. degree provided the student hassuccessfully completed the course requirements and has passed all the prescribed examinations in all the 8semesters within the maximum period specified in clause 2.

7. Award of Credits and Grades:

All assessments of a course will be done on absolute marks basis. However, for the purpose of reporting theperformance of a candidate, Letter Grades will be awarded as per the range of total marks (out of 100) obtainedby the candidate as given below:

RANGE OF MARKS FOR GRADES

Range of Marks Grade Grade Points (GP)

90-100 A++ 10

80-89 A+ 9

70-79 B++ 8

60-69 B+ 7

50-59 C 6

00-49 F 0

ABSENT W 0

CUMULATIVE GRADE POINT AVERAGE CALCULATION

The CGPA calculation on a 10 scale basis is used to describe the overall performance of a student inall courses from first semester to the last semester. F and W grades will be excluded for calculatingGPA and CGPA.

CGPA = Σi Ci GPi

Σi Ci

where Ci - Credits for the subject

GPi - Grade Point for the subject

Σi - Sum of all subjects successfully cleared during all the semesters

8. Classification of the Degree Awarded

1. A candidate who qualifies for the award of the Degree having passed the examination in all thecourses of all the semesters in his/her first appearance within a maximum period of 8 consecutivesemesters after commencement of study (maximum of 6 semesters for Lateral entry system whojoin the course in the third semester) securing a CGPA not less than 9.0 shall be declared tohave passed the examination in First Class – Exemplary.


B.E. (AERONAUTICAL ENGINEERING) ii REGULATIONS 2010

2. A candidate who qualifies for the award of the Degree having passed the examination in all thecourses of all the semesters in his/her first appearance within a maximum period of 8 consecutivesemesters after commencement of study (maximum of 6 semesters for Lateral entry system whojoin the course in the third semester) securing a CGPA not less than 7.5 shall be declared tohave passed the examination in First Class with Distinction.

3. A candidate who qualifies for the award of the Degree having passed the examination in all thecourses of all the semesters within a maximum period of 8 consecutive semesters aftercommencement of study (maximum of 6 semesters for Lateral entry system who join the course inthe third semester) securing a CGPA not less than 6.0 shall be declared to have passed theexamination in First Class.

4. All other candidates who qualify for the award of the Degree having passed the examination in allthe courses of all the 8 semesters within a maximum period of 12 consecutive semesters (10consecutive semesters for Lateral Entry system who join the course in the third semester) afterhis/her commencement of study securing a CGPA not less than 5.0 shall be declared to havepassed the examination in Second Class.

5. A candidate who is absent in semester examination in a course/project work after having registeredfor the same, shall be considered to have appeared in that examination for the purpose ofclassification of degree. For all the above mentioned classification of Degree, the break of studyduring the programme, will be counted for the purpose of classification of degree.

6. A candidate can apply for revaluation of his/her semester examination answer paper in a theorycourse, within 1 week from the declaration of results, on payment of a prescribed fee along withprescribed application to the Controller of Examinations through the Head of Department. TheController of Examination will arrange for the revaluation and the result will be intimated to thecandidate concerned through the Head of the Department. Revaluation is not permitted for practicalcourses and for project work.

Final Degree is awarded based on the following:

CGPA ≥ 9.0 - First Class - Exemplary

CGPA ≥ 7.50 < 9.0 - First Class with Distinction

CGPA ≥ 6.00 < 7.50 - First Class

CGPA ≥ 5.00 < 6.00 - Second Class

Minimum CGPA requirements for award of Degree is 5.0 CGPA.

9. Discipline

Every student is required to observe disciplined and decorous behaviour both inside and outside the Universityand not to indulge in any activity which will tend to bring down the prestige of the University. If a studentindulges in malpractice in any of the University theory / practical examination, he/she shall be liable for punitiveaction as prescribed by the University from time to time.

10. Revision of Regulations and Curriculum

The University may revise, amend or change the regulations, scheme of examinations and syllabi from time totime, if found necessary.


B.E. (AERONAUTICAL ENGINEERING) iii REGULATIONS 2010

B.E. AERONAUTICAL ENGINEERING

REGULATIONS - 2010 CURRICULUM

SEMESTER I

Sl. No. SUBJECT CODE SUBJECT TITLE L T P C Page No.

THEORY

1 SMTX 1001 Engineering Mathematics – I 3 1 0 4 1

2 SCHX 1001 Environmental Science & Engineering 3 0 0 3 2

3 SPHX 1001 Physics of Materials 3 0 0 3 3

4 SCYX 1001 Engineering Chemistry 3 0 0 3 4

5 SCSX 1002 Programming in C 3 0 0 3 5

6 SMEX 1001 Engineering Graphics 2 1 0 3 6

7 SMEX 1002 Engineering Mechanics 2 1 0 3 7

PRACTICALS

8 SCSX 4002 Programming in C Lab 0 0 4 2 8

9 SPR 4002 CAD Lab – I 0 0 4 2 8

TOTAL CREDITS 26

SEMESTER II


THEORY

1 SMTX 1002 Engineering Mathematics – II 3 1 0 4 9

2 SHSX 1001 English For Science & Technology 3 0 0 3 10

3 SPHX 1002 Applied Physics 3 0 0 3 11

4 SCYX 1003 Chemistry of Industrial Materials 3 0 0 3 12

5 SCSX 1003 Programming in C++ 3 0 0 3 13

6 SEEX 1002 Basic Electrical & Electronics Engineering 2 1 0 3 14

7 SAEX 1001 Aircraft Production Techniques 3 0 0 3 15

PRACTICALS

8 SPRX4007 Production Technology Lab - I 0 0 4 2 16

9 SCSX4007 Programming in C++ Lab 0 0 4 2 16

TOTAL CREDITS 26

L - Lecture hours; T - Tutorial hours; P - Practical hours; C - Credits


B.E. (AERONAUTICAL ENGINEERING) iv REGULATIONS 2010

SEMESTER III


THEORY

1 SMTX 1009 Engineering Mathematics – III 3 1 0 4 17

2 SMEX 1004 Engineering Thermodynamics 3 0 0 3 18

3 SMEX 1005 Fluid Mechanics & Machinery 3 0 0 3 19

4 SAEX 1002 Solid Mechanics 3 0 0 3 20

5 SMEX 1007 Machine Drawing 3 0 0 3 21

6 SAEX 1003 Introduction to Aeronautics 3 0 0 3 22

7 SAEX 1004 Mechatronics & Microprocessors 3 0 0 3 23

PRACTICALS

8 SAEX 4001 Aero CAD Lab - I 0 0 4 2 24

9 SPRX 4003 Strength of Materials Laboratory 0 0 2 1 24

10 SPRX 4004 Fluid Mechanics & Machinery Laboratory 0 0 2 1 24

TOTAL CREDITS 26

SEMESTER IV


THEORY

1 SMTX 1010 Engineering Mathematics – IV 3 1 0 4 25

2 SAEX 1005 Modern Avionics 3 0 0 3 26

3 SPRX 1005 Mechanics of Machines 3 1 0 4 27

4 SAEX 1006 Aerodynamics 3 0 0 3 28

5 SAEX 1007 Aircraft Structures – I 2 1 0 3 29

6 SAEX 1008 Aircraft Systems & Instruments 3 0 0 3 30

PRACTICALS

7 SAEX 4002 Aerodynamics Lab 0 0 4 2 31

8 SAEX 4003 Avionics Lab 0 0 2 1 31

9 SAEX 4004 Aero Modeling Lab 0 0 2 1 31

TOTAL CREDITS 24


B.E. (AERONAUTICAL ENGINEERING) v REGULATIONS 2010

SEMESTER V


THEORY

1 SMTX 1011 Applied Numerical Methods 3 1 0 4 32

2 SAEX 1009 Supersonic Aerodynamics 3 0 0 3 33

3 SAEX 1010 Aircraft Structures – II 3 1 0 4 34

4 SAEX 1011 Experimental Stress Analysis 3 0 0 3 35

5 SAEX 1012 Aircraft Performance 3 0 0 3 36

6 SAEX 1013 Airframe Maintenance and Repair Practices 3 0 0 3 37

7 SAEX 1014 Control Systems for Aircraft 3 0 0 3 38

PRACTICALS

8 SAEX 4005 Aircraft Structures – lab 0 0 4 2 39

9 SAEX 4006 Computation Lab 0 0 2 1 39

10 SAEX 4007 Aircraft Systems Lab 0 0 2 1 39

TOTAL CREDITS 27

SEMESTER VI


THEORY

1 SMEX 1017 Resource Management Techniques 3 0 0 3 40

2 SAEX 1015 Aircraft Stability and Control 3 0 0 3 41

3 SAEX 1016 Propulsion – I 3 0 0 3 42

4 SAEX 1017 Finite Element Methods 3 1 0 4 43

5 Elective I 3 0 0 3

6 Elective II 3 0 0 3

PRACTICALS

8 SAEX 4008 Aircraft Structural Repair & Practice Lab 0 0 4 2 44

9 SAEX 4009 Propulsion Lab 0 0 4 2 44

TOTAL CREDITS 23


B.E. (AERONAUTICAL ENGINEERING) vi REGULATIONS 2010

SEMESTER VII


THEORY

SBAX 1001 Principles of Management & Professional Ethics 3 0 0 3 45

SMEX 1018 Heat and Mass Transfer 3 1 0 4 46

SAEX 1018 Propulsion – II 3 0 0 3 47

SAEX 1019 Theory of Vibrations 3 1 0 4 48

Elective – III 3 0 0 3

Elective – IV 3 0 0 3

PRACTICALS

SAEX 4010 Aircraft Design Project 0 0 4 2 44

TOTAL CREDITS 22

SEMESTER VIII


THEORY

SAEX 1020 Aircraft Composite Materials 3 0 0 3 49

SAEX 1021 Rockets and Missiles 3 0 0 3 50

SAEX 1022 Aircraft Engine Maintenance & Repair Practices 3 0 0 3 51

PRACTICALS

SAEX 4011 Composite Structures Lab 0 0 2 1 52

SAEX 4012 Aircraft Engine Repair and Maintenance Lab 0 0 2 1 52

S26X PROJ Project Work & Viva Voce 0 0 0 15 52

TOTAL CREDITS 26

TOTAL CREDITS FOR THE COURSE 200


B.E. (AERONAUTICAL ENGINEERING) vii REGULATIONS 2010

LIST of ELECTIVES NOTE: ONE SUBJECT FROM EACH GROUP SHOULD BE CHOSEN COMPULSORILY


Group I: AERODYNAMICS

1 SAEX 1023 Computational Fluid Dynamics 3 0 0 3 53

2 SAEX 1024 Wind Tunnel Techniques 3 0 0 3 54

3 SAEX 1025 Aircraft Design 3 0 0 3 55

4 SAEX 1026 Helicopter Aerodynamics 3 0 0 3 56

5 SAEX 1027 Advanced Flight Dynamics 3 0 0 3 57

Group II: AIRCRAFT MAINTENANCE

6 SAEX 1028 Helicopter Maintenance 3 0 0 3 58

7 SAEX 1029 Air Transportation and Aircraft Maintenance 3 0 0 3 59

8 SAEX 1030 Aircraft Rules and Regulations 3 0 0 3 60

9 SAEX 1031 Airline Operations and Management 3 0 0 3 61

10 SAEX 1032 Aircraft Maintenance Management 3 0 0 3 62

Group III: AIRCRAFT STRUCTURES

11 SAEX 1033 Computer Aided Design and Analysis 3 0 0 3 63

12 SAEX 1034 Aircraft Materials 3 0 0 3 64

13 SAEX 1035 Aeroelasticity 3 0 0 3 65

Group IV: AVIONICS AND AEROSPACE

14 SAEX 1036 Advanced Control System Design for AerospaceVehicles

3 0 0 3 66

15 SAEX 1037 Aircraft Navigation, Guidance and Control 3 0 0 3 67

16 SAEX 1038 Flight Control Systems Design 3 0 0 3 68

17 SAEX 1039 Unmanned Aircraft Systems 3 0 0 3 69

18 SAEX 1040 Robotics Engineering 3 0 0 3 70

19 SAEX 1041 Cryogenics 3 0 0 3 71

20 SAEX 1042 Spacecraft Technology 3 0 0 3 72

21 SAEX 1043 Launch Vehicles and Spacecraft Propulsion 3 0 0 3 73

22 SAEX1044 Orbital Mechanics 3 0 0 3 74


B.E. (AERONAUTICAL ENGINEERING) viii REGULATIONS 2010

SMTX1001ENGINEERING MATHEMATICS – I

(Common to all branches except Bio Groups)

L T P Credits Total Marks

3 1 0 4 100

UNIT I TRIGONOMETRY 10 hrs.

Review of Complex numbers and De Moivre’s Theorem. Expansions of Sinnθ and Cosnθ; Sinθ and Cosθ inpowers of θ, Sinnθ and Cosnθ in terms of multiples of θ. Hyperbolic functions – Inverse hyperbolic functions. Separationinto real and imaginary parts of complex functions

UNIT II MATRICES 10 hrs.

Characteristic equation of a square matrix - Eigen values and Eigen vectors of a real matrix- properties of Eigenvalues and Eigen vectors, Cayley-Hamilton theorem (without proof) verification – Finding inverse and power of a matrix.Diagonalisation of a matrix using similarity transformation (concept only) , Orthogonal transformation – Reduction ofquadratic form to canonical form by orthogonal transformation.

UNIT III GEOMETRICAL APPLICATIONS OF DIFFERENTIAL CALCULUS 10 hrs.

Curvature –centre, radius and circle of curvature in Cartesian co-ordinates only – Involutes and evolutes –envelope of family of curves with one and two parameters – properties of envelopes and evolutes – evolutes asenvelope of normal.

UNIT IV FUNCTIONS OF SEVERAL VARIABLES 10 hrs.

Functions of two variables – partial derivatives – Euler’s theorem and problems - Total differential – Taylor’sexpansion – Maxima and minima – Constrained maxima and minima – Lagrange’s multiplier method – Jacobian –Differentiation under integral sign.

UNIT V ORDINARY DIFFERENTIAL EQUATION 10 hrs.

Second order linear differential equation with constant coefficients – Particular Integrals for eax, sin ax, cos ax,xn, xneax, eax sinbx, eax cos bx. Equations reducible to Linear equations with constant co-efficient using x=et.Simultaneous first order linear equations with constant coefficients - Method of Variations of Parameters.

TEXT / REFERENCE BOOKS:1. Veerarajan. T , “Engineering Mathematics for First Year”, Tata McGraw Hill Publishers ,II Edition ,2008.2 Kandaswamy.P. & co., “Engineering Mathematics for First Year”, S.Chand & Co Pub., IX revised edition, 2010.3 Moorthy M.B.K, Senthilvadivu. K ,”Engineering Mathematics-I”, VRB Pub., Revised Edition, 2010.4. Arumugam. S & co. “Engineering Mathematics Vol-I”, SciTech Pub., Revised Edition, 2010.5. Venkataraman M.K.,”Engineering Mathematics – First Year” (2nd edition), National Publishing Co., 2000.

UNIVERSITY EXAM QUESTION PAPER PATTERN

Max Marks : 80 Exam Duration : 3 hrs.

PART A : 2 Questions from each unit, each carrying 2 marks 20 marks

PART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks


B.E. (AERONAUTICAL ENGINEERING) 1 REGULATIONS 2010

SCHX1001ENVIRONMENTAL SCIENCE AND ENGINEERING

(Common to all branches)


3 0 0 3 100

UNIT I INTRODUCTION TO ENVIRONMENTAL STUDIES AND NATURAL RESOURCES 12 hrs.

Definition, scope and importance - need for public awareness - forest resources: use and over-exploitation,deforestation, case studies. Timber extraction, mining, dams, floods, drought, conflicts over water, dams-benefits andproblems - mineral resources: use effects on forests and tribal people - water resources: use and over-utilization ofsurface and ground water - exploitation, environmental effects of extracting and using mineral resources, case studies- food resources: world food problems, changes caused by agriculture and overgrazing, effects of modern agriculture,fertilizer-pesticide problems, water logging, salinity, case studies - energy resources: growing energy needs, renewableand non renewable energy sources, use of alternate energy sources. Case studies - land resources: land as a resource,land degradation, man induced landslides, soil erosion and desertification - role of an individual in conservation ofnatural resources - equitable use of resources for sustainable lifestyles. UNIT II ECOSYSTEMS AND BIODIVERSITY 12 hrs.

Concept of an ecosystem - structure and function of an ecosystem - producers, consumers and decomposers- energy flow in the ecosystem - ecological succession - food chains, food webs and ecological pyramids - introduction,types, characteristic features, structure and function of the (a) forest ecosystem (b) grassland ecosystem (c) desertecosystem (d) aquatic ecosystems (ponds, streams, lakes, rivers, oceans, estuaries) - introduction to biodiversity -definition: genetic, species and ecosystem diversity - biogeographical classification of India - value of biodiversity:consumptive use, productive use, social, ethical, aesthetic and option values - biodiversity at global, national and locallevels - India as a mega-diversity nation - hot-spots of biodiversity - threats to biodiversity: habitat loss, poaching ofwildlife, man-wildlife conflicts - endangered and endemic species of India - conservation of biodiversity: in-situ andex-situ conservation of biodiversity.UNIT III ENVIRONMENTAL POLLUTION 10 hrs.

Definition - causes, effects and control measures of: (a) air pollution (b) water pollution (c) soil pollution (d)marine pollution (e) noise pollution (f) thermal pollution (g) nuclear hazards - solid waste management: causes, effectsand control measures of urban and industrial wastes - role of an individual in prevention of pollution - pollution casestudies - disaster management: floods, earthquake, cyclone and landslides.UNIT IV SOCIAL ISSUES AND THE ENVIRONMENT 8 hrs.

From unsustainable to sustainable development - urban problems related to energy - water conservation, rainwater harvesting, watershed management - resettlement and rehabilitation of people; its problems and concerns, casestudies - environmental ethics: issues and possible solutions - climate change, global warming, acid rain, ozone layerdepletion, nuclear accidents and holocaust, case studies. - wasteland reclamation - consumerism and waste products- environment protection act - air (prevention and control of pollution) act - water (prevention and control of pollution)act - wildlife protection act - forest conservation act - issues involved in enforcement of environmental legislation -public awareness.UNIT V HUMAN POPULATION AND THE ENVIRONMENT 8 hrs.

Population growth, variation among nations - population explosion - family welfare programme - environmentand human health - human rights - value education - HIV / AIDS - women and child welfare - role of informationtechnology in environment and human health - case studies.

Visit to a local area to document environmental assets-river/forest/grassland/hill/mountain. Visit to a local pollutedsite-urban/rural/ industrial/agricultural-study of common plants, insects, birds-study of simple ecosystems-pond, river, hillslopes etc.TEXTBOOK / REFERENCE BOOKS:1. Meenakshi.P, Elements of Environmental Science and Engineering, 1st edition, PHI New Delhi, 2009.2. Ravikrishnan. A, Environmental Science & Engineering, 3rdedition, Sri Krishna Publications, Chennai.3. Wrigh.R.T & Nebel B.J, Environmental science-towards a sustainable future by Richard 8th edition, prentice hall of India, Newdelhi4. Erach Bharucha ,Text Book of Environmental Studies, University Press, Chennai.5. Anjanayelu.Y, Introduction to Environmental Engineering, B.S.Publications.

UNIVERSITY EXAM QUESTION PAPER PATTERNMax. Marks: 80 Exam Duration: 3 hrs.





SPHX1001PHYSICS OF MATERIALS

(Common to all Branches of B.E / B.Tech)


3 0 0 3 100

UNIT I CONDUCTING AND SUPERCONDUCTING MATERIALS 10 hrs.Classical Free electron theory of Metals-Derivation of Electrical and Thermal Conductivity- Deduction of

Wiedemann Franz law-Lorentz number. Introduction to Band theory, Difference between Conductors, Semiconductorsand Insulators - Superconductivity-Transition temperature - occurrence of superconductivity - BCS Theory(Qualitative),properties of superconductors -Type I &Type II superconductors, High Tc superconductors, AC & DC Josephson effects.Applications of superconductors – basic concepts of SQUID, cryotron, magnetic levitation.UNIT II MAGNETIC AND DIELECTRIC MATERIALS 10 hrs.

Types based on spin. Hard and soft magnetic materials, domain theory of Ferromagnetism, magnetic bubbles,formation and propagation of magnetic bubbles, applications of magnetic materials - Magnetic storage devices. Dielectricparameters, polarization, polarisability, types of polarization. Internal or local electric field - derivation of Lorentz Equationand Clausius - Mossotti Equation, dielectric loss and breakdown, types of dielectric breakdown, types of dielectricmaterials, applications.UNIT III OPTICAL MATERIALS 10 hrs.

Optical processes and Excitons - types, Traps - Trapping and recombination, types, Point defects –Frenkel andSchottky defects - Colour centers - types and their mechanisms, Luminescence - Photoluminescence - Types-Fluorescence and Phosphorescence- Mechanism and its applications, Cathodoluminescence, Electroluminescence.Non-linear Optical Materials – Basic Principle, Classifications, Properties - Frequency Doubling or Tripling, Optical Mixing- Applications.UNIT IV MODERN ENGINEERING MATERIALS 10 hrs.

Metals and alloys – steel and its properties - Iron-carbon phase diagram, Titanium and Aluminium based alloys- Introduction, properties and Applications. Shape Memory Alloys (SMA) - Principle of shape memory effects, Hysteresiscurve, Two way shape memory alloys, super-elasticity and thermo-mechanical behavior. Characterization methods toidentify the phase transformation of SMA, commercial SMA – Ni-Ti alloys, copper alloys and Cu-Al alloys, Applications.Ceramics – Classification, Properties, fabrication, advanced ceramics and applications. Composites – particle reinforcedcomposites and fiber reinforced composites – processing and applications.UNIT V CHARACTERIZATION OF MATERIALS 10 hrs.

Structural characterization – X-ray diffraction, electron diffraction and neutron diffraction – Determination of crystalstructure. Difference among these diffraction techniques.Micro structural characterization – optical microscope, scanningelectron microscope, transmission electron microscope, atomic force microscopy, micro and nano hardness testing –principle and applications.REFERENCE BOOKS : 1. Ragavan.V, Material science and Engineerimg, 5th Edition, Eastern Eco, 2004. 2. Suresh.R and Jayakumar.V, Materials Science, 1st Edition, Lakshmi Publication, 2003. 3. Wilson.J and Hawkes.J.F.B, Optoelectronics- An Introduction, 2nd Edition, Prentice-Hall of India, 2001. 4. Dr.Arumugam M., Semiconductor Physics and Opto electronics, 1st Edition, Anuradha Publishers, 2003. 5. Gaur.R.K and Gupta.S.L, Engineering Physics, 8th Edition, Dhanbat Rai Publications,2007. 6. Palanisamy.P.K, Engineering Physics, 1st Edition, SCITECH Publications, 2007. 7. Sankar.B.N and Pillai.S.O, A text book of Engineering Physics, 1st Edition, New Age international Publishers, 2007. 8. Rajendran.V, Engineering Physics, 2nd Edition, Tata McGraw-Hill, 2008. 9. Avadhanulu.M.N and P.G. Kshirsagar.P.G, Engineering Physics, 2nd Edition, S. Chand & Company, 2007.10. Dr. Arumugam M., Engineering Physics, 2nd Edition, Anuradha Publications, 2002.11. William D.Callister,Jr, Materials Science and Engineering An introduction, 6th Edition, John-Wiley and Sons,2004.12. Cullity.B.D, Principles of X-ray diffraction, 3rd Edition, Prentice Hall, 2001



Out of 20 marks, maximum of 10% problems may be asked. PART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks

Out of 60 marks, maximum of 10% problems may be asked

‘Applications’ mentioned in the syllabus refer to the basic applications and not to any specific case.



SCYX1001ENGINEERING CHEMISTRY

(Common to all branches)


3 0 0 3 100

UNIT I WATER TECHNOLOGY 10 hrs.

Introduction: Impurities present in water, Hardness: Types of hardness, Expression, Units. Estimation of hardnessby EDTA method, Problems. Boiler Troubles: Sludge & Scales, Boiler Corrosion. Water Softening: Zeolite process,Demineralization process, Merits and Demerits. Reverse osmosis, Merits and Demerits. Domestic water treatment: Flowchart diagram only.UNIT II BATTERIES AND FUEL CELLS 10 hrs.

Introduction - Battery terminology: Primary cells, Secondary batteries, Charging and Discharging characteristics,Capacity, Energy density, Cycle life, Internal resistance. Secondary batteries: Lead-acid accumulator, Nickel-cadmiumbatteries , Lithium primary cells: Lithium-thionyl chloride cell, Lithium-iodine cell. Lithium secondary batteries: Lithium-ionbatteries. Fuel cells: Hydrogen-Oxygen fuel cell, Solid oxide fuel cell (SOFC): Principle, construction, anode cathodeand electrolyte. Proton Exchange Membrane Fuel Cell.UNIT III CORROSION SCIENCE 10 hrs.

Introduction - Electrochemical cell representation. Electrochemical series: Significance. Galvanic series.Corrosion: Definition of corrosion, Dry corrosion: Mechanism of Dry corrosion, Pilling-Bedworth rule, Wet Corrosion:

Mechanism. Types of corrosion: Galvanic corrosion, Differential aeration corrosion, Pitting corrosion, Microbial Corrosion.Factors influencing corrosion: Nature of the metal, nature of the environment. Corrosion control: Material selection andDesign, Cathodic protection. Corrosion inhibitors: Anodic, cathodic and Vapour phase inhibitors.UNIT IV EXPLOSIVES AND ROCKET PROPELLANTS 10 hrs.

Introduction - Explosives: Requirements, Classification of Explosives: Low explosives, primary explosives andhigh explosives. Assessment of explosives.

Rocket engines: Types of rocket engines. Basic principle, Mass fraction, Specific impulse, Thrust, Effective exhaustvelocity, Specific propellant consumption. Chemical propellants: Requirements, Classification: Liquid fuels, Liquidoxidizers, Solid fuels, Solid oxidizers.UNIT V SURFACE CHEMISTRY 10 hrs.

Introduction. Adsorption: Types, Adsorption of gases on solids, Adsorption of solutes from solution. Adsorptionisotherms: Freundlich adsorption isotherm, Langmuir adsorption isotherm. Industrial adsorbent materials: Role ofadsorbents in catalysis and water softening. Emulsion: Types: water/oil, oil/water. Applications of adsorption: Cottrell’sprecipitator, Coating of rubber on metals, Electrostatic painting.TEXT / REFERENCE BOOKS:1. Jain P.C. and Monica Jain,Engineering Chemistry, 15th Edition Dhanpat Rai Publishing Co. 20092. Dara S.S., Text Book of Engineering Chemistry, S.Chand & Co, 20083. Sheik Mideen A., Engineering Chemistry (I & II),13th Edition, Shruthi Publishers, 20104. Parameswara Murthy C, Agarwal C V, Andra Naidu, Textbook of Engineering Chemistry, B S Publications, 20065. Kuriakose J.C. and Rajaram J., Chemistry in Engineering and Technology",. Vol.1 & 2, 5th reprint, Tata McGraw Hill Publishing

Company (P) Ltd., 2010.6. Sharma B.K., Engineering Chemistry, 2nd Edition, Krishna Prakasam Media (P) Ltd., 20017. Puri Br, Sharma Lr, Madhan S Pathania, Principles of Physical Chemistry, 41st Edition, Vishal Publishing Co., 20048. Mars G Fontana, Corrosion Engineering, 3rd Edition, Tata McGraw Hill, 20089. David Linden, Thomas B Reddy, Handbook of Batteries, 4th Edition, McGraw-Hill, 201010. George Paul Sutton, Oscar Biblarz, Rocket Propulsion Elements, 8th Edition, John Wiley & Sons, 2010


Max. Marks: 80 Exam Duration: 3 hrs



One problem for 5 marks may be asked in Unit 1 - Water Technology



SCSX1002PROGRAMMING IN C

(Common to all branches of B.E / B.Tech.)


3 0 0 3 100

UNIT I 10 hrs.Introduction: Algorithms & flowcharts-Overview of C-Features of C-IDE of C Structure of C program-Compilation

& execution of C program-Identifiers, variables, expression, keywords, data types, constants, scope and life of variables,local and global variables. Operators: arithmetic, logical, relational, conditional and bitwise operators- Special operators:size of () & comma (,) operator-Precedence and associativity of operators & Type conversion in expressions.

Basic input/output and library functions: Single character input/output i.e. getch(), getchar(), getche() &putchar()-Formatted input/output: printf() and scanf()-Library Functions: concepts, mathematical and character functions.

UNIT II 10 hrs.Control structures: Conditional control-Loop control and Unconditional control structures.

Functions: The Need of a function-User defined and library function- Prototype of a function-Calling of afunction-Function argument-Passing arguments to function- Return values-Nesting of function- main()-Command linearguments and recursion. Storage class specifier – auto, extern, static, & register.

UNIT III 10 hrs.Arrays: Single and multidimensional arrays-Array declaration and initialization of arrays-Array as function

arguments.

Strings: Declaration-Initialization and string handling functions.

Structure and Union: Defining structure-Declaration of structure variable-Accessing structure members-Nestedstructures-Array of structures-Structure assignment-Structure as function argument-Function that returns structure- Union.

UNIT IV 10 hrs.Pointers: The ‘&’ and ‘ ’ operators-Pointers expressions-Pointers vs arrays-Pointer to functions-Function returning

pointers-Static and dynamic memory allocation in C.

DMA functions: malloc(), calloc(), sizeof(), free() and realloc()-Preprocessor directives.

UNIT V 10 hrs.File management: Defining, opening & closing a file, text file and binary file- Functions for file handling: fopen,

fclose, gets, puts,fprint, fscanf, getw, putw, fputs, fgets, fread, fwrite-Random access to files: fseek, ftell, rewind-Filename as Command Line Argument.

Graphics in PC-Initialize Graphics Mode-Functions used In Graphics - Drawing a Point on the Screen-Drawinglines, rectangles, ovals, circles, arcs, polygon, filling colors-Using Text in Graphics Display.

REFERENCE BOOKS: 1. Balaguruswami.E, ‘Programming in C’, TMH Publications,1997 2. Behrouz A. Forouzan & Richard F. Gilberg, “Computer Science A Structured Programming using C”, Cengage Learning, 3rd Edition, 2007 3. Gottfried , ‘Programming with C’, schaums outline series, TMH publications,1997 4. Mahapatra , ‘Thinking in C’, PHI publications, 2nd Edition. 5. Stevens , ‘Graphics programming in C’, BPB publication,2006 6. Subbura.R , ‘Programming in C’, Vikas publishing, 1st Edition, 2000


Max Marks : 80 Exam Duration : 3 hrs.PART A : 2 Questions from each unit, each carrying 2 marks 20 marksPART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks



SMEX1001ENGINEERING GRAPHICS

(Common to all Branches of B.E / B.Tech)


1 2 0 3 100

UNIT I CONSTRUCTION OF PLANE CURVES 10 hrs.

Introduction - Importance of graphics in engineering applications – Use of drafting instruments – BIS specificationsand conventions – Size, layout and folding of drawing sheets – Lettering and dimensioning- Polygons used inengineering practice– methods of construction of pentagon and hexagon– Construction of ellipse, parabola andhyperbola.UNIT II PROJECTION OF POINTS AND LINES 10 hrs.

General principles of orthographic projection – first angle projection – layout of views – projections of points,straight lines located in the first quadrant – Determination of true lengths of lines and their inclinations to the planesof projection – TracesUNIT III PROJECTION OF SOLIDS AND SECTION OF SOLIDS 10 hrs.

Projection of solids like prism, pyramid, cylinder and cone when the axis is inclined to only one plane of projection– Change of position method only - Sectioning of above mentioned solids in simple vertical positions by cutting planeinclined to one reference plane and perpendicular to the other – True shapes of sectionsUNIT IV DEVELOPMENT OF SURFACES AND FREE HAND SKETCHING 10 hrs.

Need for development of surfaces – Development of lateral surfaces of simple and truncated solids – Prisms,pyramids, cylinders and cones.- Pictorial representation of engineering objects – Representation of three dimensionalobjects in two dimensional media – Need for multiple views – Developing visualization skills through free hand sketchingof three dimensional objects.UNIT V ISOMETRIC PROJECTIONS & PERSPECTIVE PROJECTIONS 10 hrs.

Principles of isometric projection – Isometric scale – Isometric projections of simple solids and combination ofsolids - Prisms, pyramids, cylinders, cones and spheres (excluding isometric projections of truncated solids) - Perspectiveprojections - Simple objects like – cube, prisms, pyramids by Vanishing point method & Visual Ray method (excludingperspective projections of truncated solids)TEXT BOOKS / REFERENCE BOOKS:1. Natarajan, K.V, “ A Textbook of Engineering Graphics”, Dhanalakshmi Publishers, Chennai, 2006 .2. Venugopal, K. and Prabhu Raja, V., “Engineering Graphics”, New Age International(P) Ltd.,2008.3. Ramachandran. S, Pandian. K, Ramanamurthy. E.V.V. and Devaraj. R “Engineering Graphics”, AirWalk Publications, Chennai, 20094. IS 10711-2001: Technical Products Documentation – Size and Layout of Drawing Sheets5. IS 9609 (Parts 0 & 1 )-2001: Technical Products Documentation – Lettering6. IS 10714(Part 20)-2001 & SP 46 -2003: Lines for Technical Drawings7. IS 11669-1986 & SP 46-2003: Dimensioning of Technical Drawings8. IS 15021(Parts 1 to 4)-2001: Technical Drawings-Projection Methods

UNIVERSITY EXAM QUESTION PAPER PATTERNMax. Marks : 80 Exam Duration : 3 hrs.

PART A: 2 Questions from each unit, each carrying 2 marks 20 marks

PART A: equal distribution of questions from each unit.


PART B - Split up:

Unit 1: 1 question from construction of hexagon / pentagon / ellipse &

1 question from construction of parabola / hyperbola

Unit 2: 1 question from projection of points & 1 question from projection of lines inclined to both the planes.

Unit 3: 1 question from projection of solids & 1 question from section of solids.

Unit 4: 1 question from development of surfaces & 1 question from orthographic projection.

Unit 5: 1 question from isometric projection & 1 question from perspective projection.



SMEX1002ENGINEERING MECHANICS

(Common to Mech, Mech & Prod, Aero, Auto and Civil)


2 1 0 3 100

UNIT I BASICS & STATICS OF PARTICLES 10 hrs.

Introduction - Units and Dimensions - Laws of Mechanics - Vectors - Vectorial representation of forces andmoments - Vector operations, Coplanar forces resolution and composition of forces - equilibrium of a particle - forcesin space - equilibrium of a particle in space - equivalent systems of forces - principle of transmissibility - Singleequivalent force.

UNIT II EQUILIBRIUM OF RIGID BODIES 10 hrs.

Free body diagram - Types of supports and their reactions - requirements of stable equilibrium - Moments andCouples - Varignon’s theorem - Equilibrium of Rigid bodies in two dimensions - Equilibrium of Rigid bodies in threedimensions

UNIT III PROPERTIES OF SURFACES AND SOLIDS 10 hrs.

Determination of Areas - First moment of Area and the centroid - simple problems involving composite figures.

Second moment of plane area - Parallel axis theorems and perpendicular axis theorems - Polar moment ofInertia - Principal moments of Inertia of plane areas - Principle axes of inertia - relation to area moments of Inertia.Second moment of plane area of sections like C,I,T,Z etc. - Basic Concept of Mass moment of Inertia

UNIT IV FRICTION 10 hrs.

Frictional Force - Laws of Coulomb friction - Cone of friction- Angle of repose- Simple contact friction - Screw- Wedge - Ladder - Rolling resistance - Belt friction.

UNIT V DYNAMICS OF PARTICLES 10 hrs.

Displacement, Velocity and acceleration their relationship - Relative motion - Curvilinear motion - Newton’s Law-D’Alembert’s Principle, Work Energy Equation - Impulse and Momentum - Impact of elastic bodies.

Translation and rotation of rigid bodies- General plane motion.

TEXT BOOKS / REFERENCE BOOKS:

1. Beer & Johnston,"Vector Mechanics for engineers - Vol I &II", 8th Edition,20052. Irving H Shames, "Engineering Mechanics - Statics and Dynamics" 3rd edition, Prentice Hall of India pvt ltd 1993.3. Timoshanko and Young, "Engineering Mechanics",4th Edition, Tata McGrawhill 2005.4. McLean, "Engineering Mechanics" 3rd Edition, Schaum Series 19955. Ramachandran S., “Engineering Mechanics” 4th Edition, Air Walk Publications, 2006


Max. Marks : 80 Exam Duration : 3 hrs.



80% Problems and 20% Theory Questions may be asked



SPRX4002 CAD LAB-IL T P Credits Total Marks

0 0 4 2 100

1. Introduction

Basics, Fundamentals of feature based modeling.

2. Two Dimensional objects:

Create basic drawing objects - Points, Lines, Circles / Arcs, Planes and their combination,

Setup a drawing with correct scales, Draw with precision using Coordinate input & object

Snaps. Isometric drawing, Orthographic projection, Auxiliary views,

Modify with edit commands, Dimension and add text to drawing, Plot drawings

3. Three Dimensional objects:

Creating and Editing 3D objects, Viewing in 3D

4. Drawing creation from 3D models: Creation of various views and dimensioning,

Dimensioning commands, Editing Dimensions and Dimension text, Creating and Saving

Dimension styles, Updating Dimensions, specification of tolerances and surface finish, annotations, symbols likewelding, fillet, threads.

SCSX4002 PROGRAMMING IN C LABORATORYL T P Credits Total Marks

0 0 4 2 100

1. To write a simple menu driven calculator program using switch statement.

2. To write a program to calculate the nCr using functions.

3. To write a program to find the largest and smallest number using arrays.

4. To write a program to generate Fibonacci series.

5. To write a program to find the factorial of a number using recursion.

6. To write a program to print the sum of elements of an array using pointers.

7. To write a program to implement file handling

8. To write a program to perform matrix addition and multiplication.

9. To write a program to check for perfect number.

10. To write a program to implement string manipulation functions without using library functions.

11. To write a program to perform ASCII equivalent keystrokes.

12. To write a program to solve a polynomial equation.



SMTX1002ENGINEERING MATHEMATICS II

(Common to all branches except BIO Groups)


3 1 0 4 100

UNIT I THEORY OF EQUATIONS 10 hrs.

Relation between roots and Co-efficient of equations – Symmetry function of roots – Formation of equations –To increase or decrease the roots of a given equation by a given quantity – Reciprocal equations – Descartes ruleof signs – Cardon’s method of solving cubic equations.

UNIT II THREE DIMENSIONAL ANALYTICAL GEOMETRY 10 hrs.

Direction cosines and ratios – The equation of a plane – Equation to a straight line – Shortest distance betweentwo skew lines –Coplanar lines – Sphere – Tangent line – Plane section of a sphere – Orthogonal spheres.

UNIT III INTEGRAL CALCULUS 10 hrs.

Double integrals – Change of order of integration – Change of Variables from Cartesian to Polar coordinates– Area - using double integral - Triple integrals - Volume using Triple integrals.

UNIT IV BETA AND GAMMA FUNCTIONS 10 hrs.

Properties of definite Integrals – Related definite Integrals – Reduction formulae for eax, xn sinax, xn cos ax,sinnx, cosnx and sinm x cosn x. Definitions of Beta and Gamma integrals – Relation between them – Properties –Evaluation of definite integrals in terms of Beta and Gamma function – Simple applications.

UNIT V VECTOR CALCULUS 10 hrs.

Differentiation of a vector function – Gradient, divergence and curl – Directional derivative – Identities (withoutproof) - Irrotational and Solenoidal fields, Vector Integration – Line, Surface and Volume Integrals, Integral theorems(without proof), Green’s theorem (in the plane), Gauss divergence theorem and Stoke’s theorem – Simple applicationsinvolving rectangles and cuboids.

TEXT / REFERENCE BOOKS:1. Veerarajan.T, “Engineering Mathematics for First Year”, 2nd Edition , Tata McGrawHill Publications ,20082. Kandaswamy. P & co., “Engineering Mathematics for First Year”, 9th revised Edition, S.Chand & Co Pub., 20103. Arumugam.S & co, “Engineering Mathematics Vol-II”, Revised Edition, SciTech Pub., 20104. Grewal. B.S, “Higher Engineering Mathematics”, 40th Edition, Khanna Publications, 20075. Chandrika Prasad, “Text book on Algebra and theory of equations”, Pothishala Private Ltd., Allahabad, 2009







SHSX1001 ENGLISH FOR SCIENCE AND TECHNOLOGYL T P Credits Total Marks

3 0 0 3 100

UNIT I 10 hrs.

Reading comprehension- Skimming and Scanning - Transcoding -Bar diagram, Tables and Pie chart –Discussingtopics of general interest or on current topics and making a presentation in the class - Conjunctions and discoursemarkers- cloze reading- affixes – definitions- tense- voice – jumbled sentences.

UNIT II 10 hrs.

Subject verb agreement - Idioms and phrases, reading passages to answer evaluative, inferential and hypotheticaltype of questions- Listening - Creative thinking and speaking- Formal letters - application for job- resume preparation-inviting dignitaries to department workshops, symposium and university functions - Letter to the editor.

UNIT III 10 hrs.

Reading and summarising reports - Writing a project proposal - Editing - Checking punctuation and grammaticalerrors- Types of Sentences – preparation of Check List- formulating questions and answers - communicating politely.

UNIT IV 10 hrs.

Reported speech- Parts of speech- confusable words - Report on industrial visit - project report - Making effectivePower Point presentations - speaking about the future plans-expressing opinions-reading and guessing meanings ofunknown words from the context – using appropriate verb forms

UNIT V 10 hrs.

Modal auxiliaries – Presentation of problems and solutions – wh- questions- question tags- punctuation- hyponymy-listening and taking notes – study skills – preparing notes

TEXT / REFERENCE BOOKS:1. Aeda Abidi & Ritu Chowdary, “English For Engineers Made Easy”, Cengage India Learning Limited, New Delhi. 20102. Geetha Nagaraj, “A Course In Grammar and Composition”, Foundation Books Pvt. Ltd., New Delhi, 2006.3. Hewings. M, “Advanced English Grammar”, Cambridge University Press, Chennai. 2000.4. Nagini, P S et al, “Excellence Through communication”, Shri Jai Publications, Chennai, 2005.5. Raman M & Sangeetha Sharma, “Technical Communication”, Oxford University Press, USA 2005.6. Reddy Devika and Chowdhary S, “Technical English”, Mac Millan, Chennai. 20097. Rizvi, M.A., “Effective Technical Communication”, Tata McGRaw Hill Publishing Company Limited, New Delhi, 2006.8. Verma. Shivendra K, “Interactive Grammar of Modern English”, Frank Brothers & Company, India, 2000.



PART A: 10 questions of 2 marks each – no choice 20 marks

PART B: 6 questions from the five units with internal choice, each carrying 10 marks 60 marks



SPHX1002APPLIED PHYSICS

(Common for all branches)


3 0 0 3 100

UNIT I FIBER OPTICS 10 hrs.

Introduction - Principle and structure of optical fibers-Acceptance angle-Numerical aperture-Types of opticalfibers-Preparation of fiber – Double crucible technique-Types of rays-Theory of propagation of light-Energy loss inoptical fiber- Attenuation and distortion-Fiber splicing – Fusion and mechanical splicing-Fiber connectors -Butt joint andexpanded beam connectors-Optical fiber communication system (block diagram) - Advantages and its applications.UNIT II ACOUSTICS OF BUILDINGS 10 hrs.

Introduction – Musical sound & noise-Characteristics of musical sound : pitch, loudness, quality – Weber-Fechnerlaw-Relation between pitch & frequency-Factors on which intensity & loudness depend-Decibel scale-Sound intensitylevel and sound pressure level-Sound absorption-OWU-Sound absorption coefficient and its measurements –Reverberation - Reverberation time – Standard Reverberation time – Sabine’s formula to determine the Reverberationtime (Jaegar method)- Factors affecting the acoustics of a building and the remedies-Principles to be followed in theacoustical design of a good auditorium.UNIT III FUNDAMENTALS OF DIGITAL ELECTRONICS 10 hrs.

Number systems - Binary, decimal, Hexadecimal and Octadecimal-Conversion from one number system toanother-Binary addition-Subtraction - Subtraction by 1’s & 2’s complement- BCD-ASCII-Excess 3 code and gray code.UNIT IV NANO DEVICES 10 hrs.

Definition-Fabrication-Top down approach and bottom up approach-Nanomagnets – Particulate Nanomagnets,Geometrical Nanomagnets-Magneto Resistance – Ordinary Magneto Resistance, Giant Magneto Resistance, TunnelingMagneto Resistance- Probing Nanomagnetic Materials-Nanomagnetism in Technology-Nano Devices – Injection Laser– Quantum Cascade Laser – Optical Memories and Coulomb Blockade DevicesUNIT V MEDICAL PHYSICS 10 hrs.

Ultrasonics –Introduction- Production of ultrasonic waves - Piezo-electric method-properties-Doppler effect - Bloodflow meter – Determination of upward and downward transit time- A- scan, B-scan and M-scan-X-rays –Introduction-Units of X-rays- Diagnostic technologies of X-rays – Radiography-Fluoroscopy-Image intensifier-Nuclearmedicine – Introduction-units of radioactivity, m

99Tc generator, nuclear medicine imaging devices - Gamma camera.REFERENCE BOOKS : 1. Mathur.D.S, Heat and Thermodynamics, 5th Edition, Sultan Chand & Sons, 2004. 2. Gerd Keiser, Optical fiber communication, 3rd Edition, Tata Mc Graw Hill, 2000. 3. John M. Senior, Optical fiber communications - Principle and Practice, 2nd Edition, Pearson Education, 2006. 4. Franz J.H, Jain V.K, Optical communication – Components and Systems,1st Edition, Narosa Publications, 2001. 5. Malvino,Leach & Gautam Saha, Digital Principles and applications, 6th Edition, McGraw Hill, 2006. 6. William H. Gothman, Digital electronics – An int. to theory and practice,2nd Edition, PHL of India, 2007. 7. Roy, Medical Bio Physics, 1st Edition, Saras Publications, 2001. 8. Vasantha Pattabhi, Bio Physics, 1st Edition, Narosa, 2004. 9. Gaur. R.K. and Gupta. S.L., Engineering Physics, 8th edition, Dhanbat Rai Publications,2007.10. Avadhanulu. M.N. and. Kshirsagar. P.G, Engineering Physics, 2nd edition, S. Chand & Company, 2007.11. Dr. Arumugam M., Engineering Physics, 2nd edition, Anuradha Publications, 2002.12. William D.Callister, Jr, Materials Science and Engineering An introduction, 6th Edition, John-Wiley and Sons, 2004.






‘Applications’ mentioned in the syllabus refer to the basic applications and not to any specific case



SCYX1003CHEMISTRY OF INDUSTRIAL MATERIALS

(Common to Mech, Mech & Prod, Chem, Civil, Auto andAero)


3 0 0 3 100

UNIT I FUELS 10 hrs.Introduction - Classification. Calorific values: GCV, NCV. Determination of calorific value by Bomb Calorimeter.

Liquid Fuels: Petroleum, Refining of petroleum. Cracking: Fluidized bed catalytic cracking. Knocking in InternalCombustion engines , Cetane number, Octane number, Antiknocking agents: MTBE, ETBE. Gaseous Fuels: Naturalgas, CNG. Flue gas analysis using Orsat’s apparatus. Calculation of minimum quantity of air for combustion of fuels(simple problems)

UNIT II LUBRICANTS AND ADHESIVES 10 hrs.Lubricants: Introduction. Lubrication mechanism: Hydrodynamic lubrication, Boundary lubrication, Extreme pressure

lubrication. Properties of lubricants: Viscosity index (VI), Flash and Fire point, Cloud and Pour point, Aniline point,Oiliness, Sligh oxidation test. Classification of lubricants: Liquid lubricants, Compounding of oil. Semi solid lubricants:Greases, Types of greases. Solid lubricants: Graphite and Molybdenum disulphide (MoS 2).

Adhesives: Classification: Natural and synthetic adhesives. Adhesive action. Development of bond strength.Physical and chemical factors influencing adhesive action.

UNIT III PHASE RULE 10 hrs.Introduction - Statement, Definition of terms involved with examples. Applications of phase rule to one component

system: Water system. Reduced Phase rule: Construction of simple eutectic phase diagram using Thermal analysis,Lead silver system, Iron carbon system: Allotropes of Iron, Micro constituents of Fe-C phase diagram.

UNIT IV ALLOYS AND COMPOSITES 10 hrs.Alloys: Definition, Purpose of making alloys, Effect of alloying elements, Ferrous alloys: Stainless Steel. Non

Ferrous alloys: Aluminium and Copper alloys.

Composites: Definition , Constituents: Matrix Phase and Dispersed phase. Types of Composites: Metal matrixcomposites (MMC), Ceramic matrix composites (CMC), Polymer matrix composites (PMC), Fiber reinforced plastics(FRP), Cermets.

UNIT V INTRODUCTION TO NANOMATERIALS 10 hrs.Introduction - Nanomaterials: definition, Nanoparticles: Synthesis by Chemical reduction method. Nanoporous

materials: Synthesis by Sol-gel method. Nanowires: Synthesis by VLS mechanism. Carbon Nanotubes: Singlewalledand multiwalled nanotubes, Mechanical and electrical properties, Applications. Synthesis of Carbon Nanotubes: Electricarc discharge method, Physical Vapour Deposition (PVD), Chemical Vapour Deposition (CVD), Laser Ablation method.

TEXT / REFERENCE BOOKS: 1. Jain.P.C and Monica Jain,"Engineering Chemistry", 15th Edition, Dhanpat Rai Publishing Co. (2009) 2. Charles P.Poole Jr, and Frank J Owens, "Introduction to Nanotechnology", John Wiley and Sons (2006). 3. Sheik Mideen.A, "Engineering Chemistry (I & II)", 13th Edition, Shruthi Publishers, (2010) 4. Dara.S.S, "Text Book of Engineering Chemistry", Reprint, S.Chand & Co, (2009) 5. Kuriakose.J.C and Rajaram.J, "Chemistry in Engineering and Technology",. Vol.1 & 2, 5th Rreprint, Tata McGraw Hill Publishing

Company (P) Ltd., 2009 6. Puri Br, Sharma Lr, Madhan S Pathania, "Principles of Physical Chemistry", 41st Edition, Vishal Publishing Co., (2004) 7. Uppal.M.M, "Engineering Chemistry", 6th Ed, Khanna Publ. (2006) 8. Aggrawal.O.P, "Engineering Chemistry", 3rd Ed, Khanna Publ. (2003)

UNIVERSITY EXAM QUESTION PAPER PATTERNMax. Marks : 80 Exam Duration : 3 hrs.





SCSX1003PROGRAMMING IN C++(Common to all Branches)


3 0 0 3 100

UNIT I INTRODUCTION TO C++ 10 hrs.Object Oriented Programming Paradigms - Comparison of Programming Paradigms – Object Oriented Languages

- Benefits of Object Oriented Programming - Comparison with C - Overview of C++ -Pointers-References and Structures- Functions - Scope and Namespaces - Source Files and Programs.

UNIT II CLASSES AND OBJECTS 10 hrs.Working with classes – Classes and objects – Class specification-Class objects-Accessing class members-Defining

class members-Inline functions-Accessing member functions within class-Data hiding-Class member accessibility-Emptyclasses, constructors-Parameterized constructors-Constructor overloading-Copy constructors-new, delete operators-”this”pointer-friend classes and friend functions-Function overloading-Operator overloading.

UNIT III DERIVED CLASSES 10 hrs.Base class and derived class relationship-Derived class declaration-Forms of inheritance-Inheritance and member

accessibility- Constructors in derived class-Destructors in derived class-Multiple inheritance-Multi level inheritance-Hybridinheritance-Virtual base classes-Member function overriding-Virtual functions.

UNIT IV I/O AND LIBRARY ORGANIZATION 10 hrs.I/O Stream - File I/O - Exception Handling - Templates - STL – Library Organization and Containers – Standard

Containers - Overview of Standard Algorithms-Iterators and Allocators.

UNIT V OBJECT ORIENTED DESIGN 10 hrs.Development Process – Management - Object Identification – Components - Object Oriented Design

Fundamentals – Case Studies.

TEXT BOOKS:1. Balagurusamy, ”Object Oriented Programming with C++”, Tata McGraw Hill,4th Edition,20102. Venu Gopal.K.R, Ravishankar.T, and Raj kumar, ”Mastering C++”, Tata McGraw Hill,1999.

REFERENCE BOOKS:1. Bjarne Stroustrup, ”The C++ programming language”, Addision Wesley, 3rd Edition,1998.2. John R Hubbard, “Programming with C++”, Shaums Outline Series, McGraw Hill, 2nd edition.3. James Martin & James J.Odell,”Object Oriented methods-A foundation”,Prentice Hall,1997.4. Grady Booch, “Object Oriented Analysis and Design with application”, Addission Wesley, II Edition ,1994.







SEEX1002BASIC ELECTRICAL AND ELECTRONICS ENGINEERING

(Common to Mech, Mech & Prod, Auto, Aero & Chem)


2 1 0 3 100

BASIC ELECTRICAL ENGINEERINGUNIT I D.C.CIRCUITS 11 hrs.

Electrical quantities, Ohm’s Law, Resistors - Series and parallel combinations, Kirchoff’s laws, Node and MeshAnalysis - Star delta Transformation

UNIT II MAGNETIC CIRCUITS 8 hrs.

Definition of MMF, Flux and reluctance - Leakage factor - Reluctances in series and parallel (series and parallelmagnetic circuits) - Electromagnetic induction - Fleming’s rule - Lenz’s law - Faraday’s laws - statically and dynamicallyinduced EMF - Self and mutual inductance - Energy stored and energy density - Analogy of electric and magneticcircuits

UNIT III A.C.CIRCUITS 11 hrs.

Sinusoidal functions - RMS(effective) and Average values- Phasor representation - J operator - sinusoidalexcitation applied to purely resistive , inductive and capacitive circuits - RL , RC and RLC series and parallel circuits- power and power factor - Three phase circuits - Star / Mesh connections - with balanced loads - measurement ofpower by two wattmeter method.

TEXT BOOKS:1. Mittle.B.N, Aravind Mittle, "Basic Electrical Engineering" , Tata McGraw Hill", 2nd Edition. Sep 20052. Theraja.B.L, "Fundamentals of Electrical Engineering and Electronics", S.Chand & Co., 1st Multicolor Edition, 2006 (Reprint 2009)

REFERENCE BOOKS:1. Smarajit Ghosh, "Fundamentals of Electrical and Electronics Engineering", PHI Learning Private Ltd, 2nd Edition, 2010.2. Wadhwa.C.L, "Basic Electrical Engineering", New Age International, 4th Edition, 2007. (Reprint June 2010)3. Abhijit Chakrabarti, Sudipta nath & Chandan Kumar Chanda, "Basic Electrical Engineering", Tata McGraw Hill, 1st Edition, 2009.4. T. Thyagarajan, “Fundamentals of Electrical Engineering”, SciTech Publications, 5th Edition, Reprint Jan 2010

BASIC ELECTRONICS ENGINEERINGUNIT I SEMICONDUCTOR DEVICES AND LOGIC GATES 10 hrs.

Discrete devices - PN junction diodes - Zener diodes - Tunnel diodes- Thermistors - Bipolar junction transistors- Field effect transistors (FET and MOSFET) - Uni junction transistors - Silicon controlled rectifiers and Triacs. UniversalGates - Half Adder - Full Adder.

UNIT II RECTIFIERS, AMPLIFIERS AND OSCILLATORS 10 hrs.

Half and full wave rectifiers- Capacitive and inductive filters- ripple factor- PIV-rectification efficiency. CB, CEand CC Configuration - RC coupled amplifier- positive and negative feedback - Barkhausen criterion for oscillations -RC and LC oscillators.

TEXT BOOK/REFERENCE BOOKS:1. Sedha.R.S, A Text book of Applied electronics, 2nd Edition, S.Chand & company, 2005.2. Dr.Bhattacharya.S.K and Dr.Renu vig, Principles of electronics, 3rd Edition, S.K.Kararia & Sons, 2002.




(Distribution may be 70% Theory and 30% Numerical)



SAEX1001 AIRCRAFT PRODUCTION TECHNIQUESL T P Credits Total Marks

3 0 0 3 0

UNIT I CLASSIFICATION OF TOOLS AND QUALITY CONTROL PROCESSES IN AIRCRAFT INDUSTRY 10 hrs.

Tools, Classification, Basic, detail and assembly tools - Interchangeability. Hand tools - precision instruments -special tools and equipments in an airplane maintenance shop - identification terminology - specification and correctuse of various aircraft hardware i.e., nuts, bots, rivets and screws etc., - American and British system of specification- threads, gears, bearings etc., Drills, taps and reamers. Identification of all types of fluid line fittings. Materials, metallicand non-metallic.

UNIT II CONVENTIONAL MACHINING PROCESSES 10 hrs.General principles of working, Types and commonly performed operation in the following machines:- Lathe,

Shaper, Planer, Milling Machine, Drilling Machine, Grinding Machine & Machining Centre

UNIT III UNCONVENTIONAL MACHINING PROCESSES 10 hrs.Principles and Application of the following Processes - Abrasive Jet Machining, Ultrasonic Machining, Electric

Discharge Machining, Electrochemical Machining, Chemical Machining, LASER Beam Machining, Electron BeamMachining, Plasma Arc Machining.

UNIT IV FABRICATION AND SURFACE FINISHING PROCESSES 10 hrs.Basic moulding, casting and welding processes - Corrosion - Types of Corrosions - Prevention - Protective

treatments.

UNIT V STRUCTURAL ASSEMBLY 10 hrs.Stages - Riveting types and techniques - Equipment - Fasteners - Integral tanks - Final assembly of aircraft -

Flight testing.

TEXT BOOK:1. Keshu, S.C., Ganapathy K.K., Aircraft Production Techniques - Interline Publishing House, Bangalore.

REFERENCE BOOKS:1. Kanna. O.P. Lal. M., Production Technology - Dhanpat Rai Publication, New Delhi, 1997.2. Champman W.A.J., Production Technology, 4th Edition, Arnold Publisher, New Delhi, 1994.3. Kroes, Watkins Delp, "Aircraft maintenance and repair", McGraw Hill.4. A & P Mechanics, "Aircraft Handbook - F.A.A. Himalayan book house, New Delhi.


Max. Marks: 80 Exam Duration: 3 hrs





SPRX4007 PRODUCTION TECHNOLOGY LAB - IL T P Credits Total Marks

0 0 4 2 100

1. Study of lathe and precision tools

2. Facing and plain turning

3. Step turning

4. Taper turning (compound slide swivel method)

5. Taper turning (taper turning attachment method)

6. External thread cutting (single start)

7. External thread cutting (double start)

8. Square thread cutting

9. Eccentric turning

10. Internal thread cutting (using taps)

11. Grooving & knurling

12. Drilling

13. Boring

14. Copy turning

SCSX4007 PROGRAMMING IN C++ LABL T P Credits Total Marks

0 0 4 2 100

1. Write a program to calculate final velocity using the formula: v=u + a*t, with initial velocity, acceleration and time as input.

2. Write a program to find the area of square, rectangle, circle using function overloading concept.

3. Write a program to change the sign of an operands using unary operator overloading concept.

4. Write a program to add two complex numbers using binary operator overloading concept.

5. Write a program to find mean value of two integers using friend function concept.

6. Write a program to multiple and divide two different data type using inline function concept.

7. Implement parametrized constructor, default conctructor, copy constructor and destructor

8. Write a program to enter the sale value and print the agent’s commission using single inheritance.

9. Write a program to enter salary and output income tax and net salary using multiple inheritance concept.

10. Write a program to enter the unit reading and output the customer’s telephone bill using hierarchical inheritance.

11. Write a program to find the grade of the students based on academic marks and sports using multilevel inheritance.

12. Write a program having student as an abstract class and create many derived classes such as Engineering, Medical etcfrom student’s class. Create their objects and process them.

13. Write a program to count the words and characters in given text using virtual function.

14. Write a program to calculate net pay of employee using virtual base class concept.

15. Write a program to calculate division of two number with a try block to detect and throw an exception if the condition""divide by-zero" occurs.

16. Write a program to merge two files into one single file

17. Write a program to swap two values using funtion templates

18. Write a program to sort the numbers using class templates



SMTX1009ENGINEERING MATHEMATICS III

(Common to all branches except Bioinformatics)


3 1 0 4 100

UNIT I LAPLACE TRANSFORM 10 hrs.

Transforms of simple functions – properties of transforms – Transforms of derivatives and Integrals – Periodicfunctions – Inverse transforms – Convolution theorems – Initial and final value theorems

UNIT II APPLICATIONS OF LAPLACE TRANSFORM 10 hrs.

Application of Laplace Transforms for solving : linear ordinary differential equations – simultaneous differentialequations – integral equations.

UNIT III COMPLEX VARIABLES 10 hrs.

Analytic functions – Cauchy – Riemann equations in Cartesian and Polar form – properties of analytic functions– construction of analytic functions – conformal mapping – standard types – bilinear transformations.

UNIT IV COMPLEX INTEGRATION 10 hrs.

Cauchy’s integral theorem – integral formula – Taylor’s and Laurent’s series (without proof) – Residues – Cauchy’sresidue theorem – Contour integration and the circle and semi circular contours.

UNIT V THEORY OF SAMPLING AND TEST OF HYPOTHESIS 10 hrs.

Test of Hypothesis – Large sample – test of significance – single proportion - difference of proportions – Singlemean - difference of means. Small sample – students ‘t’ test – single mean – difference of means – Fisher’s test –difference of variance, Exact sample – Chi square test – goodness of fit – independence of attributes.

TEXT / REFERENCE BOOKS: 1. Kandasamy, P., Thilagavathy, K., and Gunavathy, K., “Engineering Mathematics”, Volumes II & III (4th Revised Edition), S. Chand

& Co., New Delhi, 2001. 2. Venkataraman, M.K. “Engineering Mathematics” Volumes III - A & B, 13th Edition National Publishing Company, Chennai, 1998. 3. Veerarajan, T., “Engineering Mathematics”, Tata McGraw Hill Publishing Co., NewDelhi, 1999. 4. Grewal, B.S., “Higher Engineering Mathematics” (35th Edition), Khanna Publishers, Delhi, 2000. 5. Kreyszig, E., “Advanced Engineering Mathematics” (8th Edition), John Wiley and Sons (Asia) Pvt. Ltd., Singapore, 2001.







SMEX1004ENGINEERING THERMODYNAMICS

(Common to Mech, Aero & Auto)


2 1 0 3 100

(Use of standard thermodynamic tables, Mollier diagram, Psychometric chart and Refrigerant property tables arepermitted)

UNIT I BASIC CONCEPT AND FIRST LAW 10 hrs.

Basic concepts – concept of continuum, macroscopic approach, thermodynamic systems – closed, open andisolated. Property, state, path and process, quasi-static process, work, modes of work, Zeroth law of thermodynamics– concept of temperature and heat. Concept of ideal and real gases. First law of thermodynamics – application toclosed and open systems, internal energy, specific heat capacities, enthalpy, steady flow process with reference tovarious thermal equipments.

UNIT II SECOND LAW AND ENTROPY 10 hrs.

Second law of thermodynamics – Kelvin’s and Clausius statements of second law. Reversibility and irreversibility.Carnot theorem, Carnot cycle, reversed carnot cycle, efficiency, COP. Thermodynamic temperature scale, Clausiusinequality, concept of entropy, entropy of ideal gas, principle of increase of entropy, availability.

UNIT III PROPERTIES OF PURE SUBSTANCE 10 hrs.

Properties of pure substances – Thermodynamic properties of pure substances in solid, liquid and vapour phases,phase rule, P-V, P-T, T-V, T-S, H-S diagrams, PVT surfaces, thermodynamic properties of steam. Calculations of workdone and heat transfer in non-flow and flow processes.

UNIT IV IDEAL AND REAL GASES AND THERMODYNAMIC RELATIONS 10 hrs.

Gas mixtures – Properties of ideal and real gases – Equations of state – Avagadro’s law- Vanderwaal’s equationof state – compressibility factor – compressibility chart – Dalton’s law of partial pressure – Exact differentials – T-dsrelations – Maxwell’s relations – Clausius Clapeyron equations – Joule – Thomson coefficient.

UNIT V PSYCHROMETRY 10 hrs.

Psychrometry and psychrometric charts, property calculations of air vapour mixtures. Psychrometric process –Sensible heat exchange processes. Latent heat exchange processes. Adiabatic mixing, evaporative cooling, problems.

TEXT BOOKS: 1. Nag.P.K., “Engineering Thermodynamics”, 4th Edition, Tata McGraw-Hill, New Delhi,2008 2. Lynn D Russell, George A, Adebiyi “Engineering Thermodynamics”,6th Edition, Indian Edition, Oxford 3, University Press, New Delhi,

2008.

REFERENCE BOOKS: 1. Yunus A Cengel and Michael Boles, “Thermodynamics An Engineering Approach”, 6th Edition, McGraw Hill,2008 2. Ratha Krishnan.E, “Fundamentals of Engineering Thermodynamics”, 2nd Edition, Prentice – Hall of India Pvt. Ltd, 2006 3. Arora C.P, “ Thermodynamics”, 2nd Edition, Tata McGraw-Hill, New Delhi, 2003. 4. Merala C, Pother, Craig W, Somerton, “Thermodynamics for Engineers”, 2nd Edition,Schaum Outline Series, Tata McGraw-Hill, New

Delhi, 2009 5. Venwylen and Sontag, “Classical Thermodynamics”, Wiley Eastern, 1987 6. Holman.J.P., “Thermodynamics”, 3rd Ed. McGraw-Hill, 1995.

UNIVERSITY EXAM QUESTION PAPER PATTERNMax Marks : 80 Exam Duration : 3 hrs.



80% Problem and 20% Theory



SMEX1005 FLUID MECHANICS AND MACHINERYL T P Credits Total Marks

2 1 0 3 100

UNIT I 10 hrs.Fluid Properties: Density – Specific Weight – Specific Gravity – viscosity – surface tension – capillarity –compressibility.

Fluid Statics: Hydrostatic Law – Pressure Variation in static fluid – Hydrostatic force on a submerged planesurfaces – Location of hydrostatic force. Manometers – Simple U tube and differential manometers – Buoyancy –

Meta-centric height – determination of stability of floating bodies and submerged bodies.

UNIT II 10 hrs.Basic equations of motion: Types of fluid flow – Continuity, momentum and energy equations – Euler’s andBernoulli’s Equation and its applications.

Flow Measurement: Orifice meter, Venturi meter, Piezometer, Pitot Tube.

UNIT III 10 hrs.Flow through orifices: Classification – Hydraulic co-efficient – Flow through rectangular orifice, Notches and weirs.

Laminar and Turbulent flow: Reynolds experiment – Major and minor losses in pipes – Darcy weisbach’s equation,chezy’s formula – pipes in series and pipes in parallel – total energy line – hydraulic gradient line – Equivalent pipe

UNIT IV 10 hrs.Centrifugal Pumps: Definition – Operations – Velocity Triangles – Performance curves – Cavitations – Multistaging.

Reciprocating Pumps: Operation – Slip – indicator Diagram – Separation – Air vessels.

UNIT V 10 hrs.Hydraulic Turbines: Classification of hydraulic turbines – Working principle of Pelton wheel, Francis and Kaplanturbines – velocity triangles – draft tube – hydraulic turbine characteristics.

Dimensional Analysis: Buckingham’s Theorem, Non-Dimension Numbers, Similarities of Flow. Model studies

TEXT BOOK:1. Bansal.R.K,”. Fluid Mechanics & Hydraulics Machines”, 9th Edition,Laxmi Publications, 2005

REFERENCE BOOKS:1. Douglas. J. F., Gasiorek. J. M., Swaffield. J. A., “Fluid Mechanics ELBS”, 4th Edition,Prentice Hall,20002. Modi P. N., Seth S. M., “Hydraulics and Fluid Mechanics”, Standard Book House, 19873. Kumar K. L., “Engineering Fluid Mechanics”, 8th Edition, Eurasia Publication.20094. Govinda Rao N. S., “Fluid Flow Machines”, 2nd Edition,Tata McGraw Hill, New Delhi, 1990.





80% Problem and 20% Theory



SAEX 1002 SOLID MECHANICSL T P Credits Total Marks

2 1 0 3 100

UNIT I INTRODUCTION 10 hrs.Internal Forces – Stresses and Strains – Elasticity – Hook’s Law-Poisson’s Ratio – Elastic Constants and their

Relationship – Stress – Strain Diagrams for Ductile Materials –Thermal Stress – Statically Determinate and Indeterminatedefinition.

UNIT II BENDING OF BEAMS 10 hrs.Beams – Loads – shear force and Bending Moment diagrams for Simply supported, Cantilever Beams and

overhanging Beams – Pure Bending – Bending Stresses in Straight Beams – Shear Stresses in Bending of Rectangularand I Section Beams.

UNIT III TORSION OF CIRCULAR SHAFTS 10 hrs.Torsion of Circular Shafts – Shear Stresses and Twist in Solid and Hollow Shafts. Closely Coiled Helical springs.

UNIT IV BIAXIAL STRESSES 10 hrs.Analysis of Biaxial stresses – Mohr’s Circle – Principle Stresses and Maximum Shear Stress – Deductions from

Mohr’s Circle – Stresses in Thin Walled Pressure Vessels.

UNIT V DEFLECTION OF BEAMS 10 hrs.Differential Equation of the Elastic Axis- Double Integration, Area Moment and Macaulay’s methods for simply

supported, Cantilever and overhanging beams.

TEXT BOOK : 1. Timoshenko. S., Young, " Elements of Strength of Material", Vol II, T.Van Nostrand Co Inc, Princeton, N.J. 1988

REFERENCES: 1. Malhotra, D.R. and Gupta, H.C., “The Strength of Materials”, Satya Prakasan Tech. India Publications, New Delhi, 1987. 2. Kazimi.S.M.A., “Solid Mechanics”, Tata McGraw Hill, 1976. Dym.C.L. and Shames I.H., Solid Mechanics”, McGraw hill, Kogakusha,

Tokyo, 1973. 3. Subramanian R., "Strength of Materials", Oxford University


Max.Marks: 80 Exam Duration: 3 hrs.PART A : 2 Questions from each unit, each carrying 2 marks 20 marksPART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks (80% Problems and 20% Theory must be asked) 60 marks



SMEX1007MACHINE DRAWING

(Common to Mech, M & P, Auto, Aero)


1 2 0 3 100

UNIT I DRAWING STANDARDS 10 hrs. BIS code of practice for Engineering Drawing – Machine Drawing Conventions – Need for drawing conventions

– Conventional representation of common machine elements such as screws, bolts, nuts, keys, gears, bearings,couplings, webs, ribs etc., - Abbreviations and symbols for use in technical drawings - Types of sections – Parts notusually sectioned.

UNIT II FITS, TOLERANCES AND PREFERRED NUMBERS 10 hrs.Fits – Types of fits – Allocation of fits for various machine parts – Tolerances – Types – Representation on

the drawing – Tolerance data sheet – Geometric tolerance – Preferred numbers

UNIT III MANUFACTURING DRAWING (Only for practice; Not to be asked in the examination) 15 hrs. Preparation of manufacturing drawing for the following machine components: Hexagonal headed bolts- Nuts –

Square headed bolts – Cotter joints – Cotter joint with Sleeve – Socket and Spigot Cotter joint – Cotter joint withGib and Cotter – Knuckle joint

UNIT IV ASSEMBLY DRAWING 15 hrs.Preparation of assembled views from the given parts – Screw jack – Plummer block – Snug and octagonal

type – Swivel bearing – Lathe tail stock – Steam stop valve – Machine vice - Petrol Engine Connecting rod – Crosshead for horizontal and vertical steam engine.

TEXT BOOKS:1. Gopala Krishnan.K.R,”Machine Drawing “, 16th Edition, Sabhas Publications, 20082. N. D. Bhatt.N.D,” Machine Drawing”, 44th Edition, Charotar Publishing House, 20093. PSG Design Data Book

REFERENCE BOOKS:1. Gill.P.S,”Machine Drawing”. 5th Edition, S.K.Kataria & Sons,20092. Gupta.R.B,”Machine Drawing “, 1st Edition, Satya Prakash & Sons, 2006


Note: 1. Question Paper will consists of two parts (A & B) of 3 hours duration.

2. All the students will have to submit all the drawing sheets in a file periodically for continuous assessment.

Part A: Problems on Limits (finding upper limit and lower limit) : 10 Marks

Problems on Clearance Fit / Interference fit / Transition fit : 15 Marks

Conventions symbols and abbreviations : 5 Marks

Part B: Assembly Drawing (only full sectional front view / top view) : 50 Marks



SAEX 1003 INTRODUCTION TO AERONAUTICSL T P Credits Total Marks

3 0 0 3 100

UNIT I INTRODUCTION 10 hrs.Early Airplanes- Pre Wright Brothers era, Wright Flyer, Components of an Airplane and their functions. Different

Types of Flight Vehicles, Classifications. Conventional Control, Powered Controls, basic Instruments for flying, TypicalSystems for control Actuation.

UNIT II AERODYNAMICS 10 hrs.Evolution of Lift, Drag and Moment., types of wing planforms, aerodynamic characteristics of Airfoils, concept

of boundary layer, Mach Number, Maneuvers.

UNIT III AIRPLANE PROPULSION 10 hrs.Requirement of power to fly, balance of forces, various means of producing power for forward flight Basic Ideas

about Piston, Turboprop and Jet Engines, Use of Propeller and Jets for Thrust Production. Comparative Merits,Principles of Operation of Rocket, Types of Rocket and typical applications, Exploration into Space.

UNIT IV AIRPLANE STRUCTURES AND MATERIALS 10 hrs.General Types of Construction, Monocoque, Semi Monocoque and Geodesic Construction, Typical Wing and

Fuselage Structure.Different materials from wood to super alloys for airplane and engine applications. Materials forspace vehicles, FRP materials.

UNIT V AIRWORTHINESS 10 hrs.Airplane design, type certification and airworthiness certificate, Air Safety, Role of DGCA in air safety and

regulatory authority, accident investigation

TEXT BOOK:1. Anderson, J.D., “Introduction to flight”, McGraw Hill, 1995

REFERENCES:1. Ralph D. Bent & James L. Mackinley, Aircraft Basic Science, 19882. Kroes et Aircraft Maintenance and Repair al, GLENCOE,19933. Clark O. Millikan Airplane Aerodynamics, Wiley and sons 1942 Clark B.Millikan,19424. Richard S. Shevel, Fundamentals of flight Prentice Hall, 2010


Max. Marks: 80 Exam Duration: 3 hrsPART A : 2 Questions from each unit, each carrying 2 marks 20 marksPART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks (90% theory and 10% Problems must be asked)



SAEX 1004 MECHATRONICS AND MICROPROCESSORSL T P Credits Total Marks

3 0 0 3 100

UNIT I INTRODUCTION 10 hrs.Definition and key issues – evolution – elements – Role of various engineering disciplines in mechatronics –

mechatronic design elements – Applications of mechatronics - computer networks – basics of computer aided design-(CAD) – computer aided manufacturing (CAM)- Computer aided process planning – Computer integratedManufacturing-applications in manufacturing mechatronics, automobile mechatronics, medical mechatronics

UNIT II MEASUREMENTS USING SENSORS AND TRANSDUCERS 10 hrs.Measurement system, static and dynamic characteristics, classification of Transducers - Sensors - Actuators-

classifications –resistive, capacitive, inductive– strain gauges – manometers – diaphragm-bellows- manometers –LVDT-RVDT- measurement of temperature, pressure, force, thickness, humidity, vibration, level-accelerometers

UNIT III MICROPROCESSORS 10 hrs.Block Diagram of Microprocessors – Architecture of Intel 8085, Instruction Classification, Data format and storage,

Bus Structure of 8085,Addressing modes, Overview of the 8085 Instruction Set, Development of Simple AssemblyLanguage Program.

UNIT IV MICROPROCESSORS MEMORY & INTERFACING 10 hrs.RAM, ROM, EPROM, Memory Interfacing, Interfacing Input Devices, Memory Mapped I/O, Basic Concepts in

Serial I/O, Interfacing a matrix keyboard, 8255,8259,DMA Data transfer & 8237-comparitive study of 8086, 8088, 80186,80286, 80386, 80486 & Pentium microprocessors-Introduction to microcontrollers

UNIT V MODERN DEVELOPMENTS AND APPLICATIONS 10 hrs.Micro Electro Mechanical Systems ( MEMS ) - basic micro sensor and actuator micromachining – commonly

used MEMS -advantages – application of MEMS - Robotics introduction - types – robot control – selection parameters-applications of robots - CNC machine constructional details –classification –part programming- advantages anddisadvantages -types - programmable logic controllers ( PLC ) - applications – ladder diagrams – simple applications-advantages- Fibre Optic principles and applications

TEXT BOOKS:1. M.D.Singh, J.G.Joshi., Mechatronics, Prentice Hall India, 20062. Ramesh S Gaonkar, “Microprocessor Architecture, Programming, and Applications with the 8085, 5/e,Prentice Hall India, 2008

REFFERENCES:1. Bolton. N., Mechatronics: Electronics Control system for Mechanical and Electrical Engineering, Longman,19952. E.O.Doebelin, Measurement Systems, Applications and Design, McGraw Hill, 4th edition, 20003. S.Bhasker, Basic Principles – Measurements and Control Systems,Anuradha Publications,Chennai,20074. S.Ramachandran, Mechatronics Anuradha Pubclications, Chennai


Max. Marks: 80 Exam Duration: 3 hrsPART A : 2 Questions from each unit, each carrying 2 marks 20 marksPART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks



SAEX 4001 AERO CAD LAB – IL T P Credits Total Marks

0 0 4 2 100

Using any Softwares like PRO/E, CATIA, Solid Works, ANSYS, MSC / Nastran

1. Modeling of various components using any modeling software

2. Static analysis on cantilever beam

3. Static analysis of forces in a simply supported beam

4. Static analysis- Plane truss

5. 2-D static stress analysis

6. 3-D static stress analysis

7. Stress distribution in a shrink fit

8. Natural frequencies of a spring mass system

9. Stress and modal analysis of a cylinder under pressure

10. Stress distribution and natural frequencies in indeterminate structure

11. Analysis of a model airplane wing

SPRX4003 STRENGTH OF MATERIALS LABORATORYL T P Credits Total Marks

0 0 2 1 50

1. Evaluation of Engineering Stress/ strain diagram on steel rod, Thin Wire and Twisted bars under tension.

2. Compression Test on bricks, Concrete blocks

3. Deflection Test- Verification of Maxwell theorem

4. Comparison of hardness values of Steel, Copper and aluminum using Brinell and Rockwell hardness measuringmachines.

5. Estimation of spring constant under tension and Compression.

6. Estimation of notch toughness of Steel using Charpy / Izod impact testing machine.

7. Double shear Test in U.T.M

8. Fatigue Test on Steel

9. Load Measurement using Proving Ring.

SPRX4004 FLUID MECHANICS & MACHINERY LABORATORYL T P Credits Total Marks

0 0 2 1 50

1. Determinations of flow throw pipes, Losses in pipes. 2. Calibration of Orifice meter and Venturi meter. 3. Flow through notches and weir 4. Flow through open Orifice -Cd, Cc and Cv

5. Buoyancy experiment -Meta Centric height 6. Performance characteristics of Centrifugal Pump 7. Performance characteristics of Multistage Pump 8. Performance characteristics of Gear Pump 9. Performance characteristics of Jet Pump10. Performance characteristics of Reciprocating Pump11. Characteristics of Impulse turbine- Pelton wheel turbine12. Characteristics of reaction turbine - Francis turbine



SMTX 1010ENGINEERING MATHEMATICS IV

(Common to all branches except Bio Informatics)


3 1 0 4 100

UNIT I PARTIAL DIFFERENTIAL EQUATION 10 hrs.

Formulation of equations by elimination of arbitrary constants and arbitrary functions-solutions byequations-general, particular and complete integrals-Lagrange’s linear equation-standard type of first orderequation-second and higher order equations with constant coefficients-homogenous equations.

UNIT II FOURIER SERIES 10 hrs.

Euler’s formula-Dirichlets conditions-convergence statement only-change of interval-odd and even functions-halfrange series-RMS value-Parseval’s formula-complex form of Fourier series-harmonic analysis.

UNIT III WAVE AND HEAT EQUATION 10 hrs.

One dimensional wave equation-Transverse vibration of finite elastic string with fixed ends-boundary and initialvalue problems-Fourier series solution-Derivation of one dimensional heat equation-steady and unsteady state-boundaryand initial value problems-Fourier series solutions. Two dimensional heat equation-steady state heat flow in twodimensions-Laplace equation in Cartesian coordinates - Fourier series solution.

UNIT IV FOURIER TRANSFORM 10 hrs.

The infinite Fourier transform-sine and cosine transform-Properties-Inversion theorem-Finite Fourier transform-sineand cosine transform-Convolution theorem-Parseval’s identity.

UNIT V Z – TRANSFORM AND DIFFERENCE EQUATIONS 10 hrs.

Z – Transforms – Elementary Properties – Inverse Z – transforms – Convolution theorem – Formation of differenceequations – Solution of difference equations using Z – transforms.

TEXT / REFERENCE BOOKS: 1. Kandasamy, P., Thilagavathy, K., and Gunavathy, K., “Engineering Mathematics”, Volumes II & III (4th Revised Edition), S. Chand

& Co., New Delhi, 2001. 2. Venkataraman, M.K. “Engineering Mathematics” Volumes III - A & B, 13th Edition National Publishing Company, Chennai. Engineering

Mathematics – Dr. T.Veerarajan, Tata McGrawhill Company, 1998. 3. Veerarajan, T., “Engineering Mathematics”, Tata McGraw Hill Publishing Co., New Delhi, 1999. 4. Grewal, B.S., “Higher Engineering Mathematics” (35th Edition), Khanna Publishers, Delhi, 2000. 5. Kreyszig, E., “Advanced Engineering Mathematics” (8th Edition), John Wiley and Sons (Asia) Pvt Ltd., Singapore, 2001.







SAEX 1005 MODERN AVIONICSL T P Credits Total Marks

3 0 0 3 100

UNIT I DESIGN CONSIDERATIONS & DISPLAY SYSTEMS 10 hrs.Importance and role of avionics, avionic environment, Regulatory and advisory agencies -Displays and

man-machine interaction: Head -glass cockpit- Cathode Ray Tube (CRT), Active Matrix Liquid Crystal Display (AMLCD),Head Down Display (HDD), Head Up Display (HUD),Helmet Mounted Display (HMD), OLEDS, Night Vision Goggles,LASERS, Integrated Standby Instrument System (ISIS), data fusion, intelligent displays management,Displays technology, control and data entry, instrument placements

UNIT II AIRCRAFT INSTRUMENTS 10 hrs.Inertial reference systems, attitude derivation. RMI, HSI, ADI Magnetic Heading Reference System (MHRS.);

Outside world sensor systems: Radar systems - Radar Sensing - Radar Altimeter (RADALT), Doppler Radar, WeatherRadar, RADOME, Infrared systems, AWACS, Aircraft Lighting, Runway Lighting Systems

UNIT III NAVIGATION SYSTEMS 10 hrs.Principles of navigation, Automatic Direction Finding, Very High Frequency Omni-Range (VOR), Distance

Measuring Equipment (DME), landing aids ( ILS & MLS ), Inertial Navigation, GPS-global positioning system, terrainreference navigation, RNAV, FMS,GPWS,TCAS,GNSS

UNIT IV SURVEILLANCE & COMMUNICATIONS SYTEMS 10 hrs.HF, VHF, UHF, Microwaves Signals and Noise, Modulation and demodulation, Antennas, propagation, data links,

Telemetry, Transponders, Typical Systems in Aircrafts, Basic Radar Systems and types, ATC Electronic Warfare Basics

UNIT V DATA BUSES: 10 hrs.Evolution of avionics architecture, integrated modular avionics, tornado serial, ARINC

429,629,MIL-STD-1553B,STAGNAG 3910,JWIAG,hi speed data bus, PI Bus, TM Bus, COTS Data buses, Fibre Channeloptions, IEEE 1394 firewire, TTE, commercial off-the shelf (COTS) TTE Bus, modern data buses, Gigabit Ethernet

TEXT BOOKS: 1. Cary R.Spitzer, The Avionics Handbook, 2nd Edition, CRC Press LLC, 2006 2. Ian Moir, Allan G.Seabridge, Military Avionics Systems, John Wiley & Sons, Ltd,2009

REFERENCES: 1. Ian Moir, Allan G.Seabridge, Aircraft Systems : Mechanical, Electrical, Avionics Subsystems Integration, 3 rdEdition, ohn Wiley &

Sons, Ltd 2008 2. Cary R.Spitzer., Digital Avionics Systems Principles and Practices, 2nd ed,McGraw-Hill,Inc,1993. 3. Brain Kendal, “Manual of Avionics”, The English Book House, 3rd Edition, New Delhi, 1993. 4. Collinson RPG, Introduction to Avionics, Second Edition, Kluwer Academic Publishers, Chapman & Hall, 2003. 5. Don Middleton., Avionic Systems (Longman Aviation Technology Series), Longman, 1989


Max. Marks: 80 Exam Duration: 3 hrs.PART A : 2 Questions from each unit, each carrying 2 marks 20 marksPART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks



SPRX1005MECHANICS OF MACHINES

(Common to Mech & Prod and Aero)


3 1 0 4 100

UNIT I BASIC CONCEPTS 10 hrs.Links, pairs, chains, mechanisms and machines, inversions, four bar chains, single and double slider crank

chains.

Velocity and acceleration diagrams Four bar and Single slider mechanism.

UNIT II INERTIA & BALANCING 10 hrs.D’Alembert’s Principle – Inertia forces in mechanism – Calculation of crankshaft torque – Fluctuation of energy

and speed of flywheel.

Balancing of rotating and reciprocating masses in one plane and in several planes – Primary and secondaryforces and couples in single cylinder and multi cylinder in line engines.

UNIT III CAMS & GEAR TRAINS 10 hrs.Cams – Types and followers – Drawing of profile cams with roller, knife edge and flat followers – all displacement.

Gear trains – simple, compound, reverted and epi-cyclic gear trains.

UNIT IV FRICTION DEVICES 10 hrs.Friction – Friction in square threaded, V-thread, Screw jack, Clutches. Belt and rope drives –Power transmitted

through collar and journal bearings.

UNIT V VIBRATION 10 hrs.Vibrations – Free, damped and forced vibrations of single degree of freedom system. Torsion vibration of 2

rotor systems – Critical speed of loaded shafts.

TEXT / REFERENCE BOOKS:1. Thomas Beven, Theory of Machines - CBS publishers and Distributor, 19842. Amitabha Ghosh and Ashok Kumar Malick, Theory of Mechanisms and Machines, Affiliated East - West Press Private Limited, 19883. R.S.Khurmi & J.K.Gupta, Theory of Machines - S.Chand and company Pvt. Ltd 19864. Shifley J.D & Vicker J.J, Theory of Machines and Mechanics, McGraw Hill, 1980


Max.Marks: 80 Exam Duration: 3 hrs.PART A : 2 Questions from each unit, each carrying 2 marks 20 marksPART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks



SAEX1006 AERODYNAMICSL T P Credits Total Marks

3 0 0 3 100

UNIT I REVIEW OF BASIC FLUID MECHANICS 10 hrs.Continuity, Momentum and Energy Equations. Applications of Bernouli’s theorem

UNIT II TWO DIMENSIONAL FLOWS 10 hrs.Complex Potential, Point Source and Sink, Potential Vortex, Uniform Parallel flow and their Combinations, Pressure

and Velocity Distributions on Bodies with and Without Circulation in Ideal and Real fluid Flows. Kutta Joukowski’sTheorem.

UNIT III CONFORMAL TRANSFORMATION 10 hrs.Complex potential function, Blasius theorem, principles of conformal transformation, Kutta - Juokowaski

transformation of a circle into flat plate, airfoils & ellipses.

UNIT IV AIRFOILS 10 hrs.Joukowski, Karman Trefftz Profiles, Von Mises airfoils -Glauert’s thin airfoil theory, symmetrical airfoil, cambered

airfoil, flapped airfoil, determination of mean camber line shapes for uniform & linear distribution of circulation. elementsof panel method

UNIT V SUBSONIC WING THEORY 10 hrs.Downwash & induced drag, Vortex line, Horse Shoe Vortex, Biot and Savart Law, Flow past finite wings - vortex

model of the wing - induced drag – Prandtl’s lifting line theory - elliptic wing –influence of taper and twist applied towings – effect of sweep back – delta wings.

(Computational problems must be given as assignments for each unit)

TEXT BOOK:1. Anderson, J.D., “Fundamentals Of Aerodynamics”, McGraw Hill Book Co., New York 2005.

REFERENCES:1. Houghton, E.L., and Carruthers, N.B., “Aerodynamics for Engineering students”, Edward Arnold Publishers Ltd., London, 1989.2. Milne Thomson, L.H., “Theoretical Aerodynamics”, Dover Publication, 20083. Clancy, L.J., “Aerodynamics”, Pitman, 1986.


Max. Marks: 80 Exam Duration: 3 hrs.PART A : 2 Questions from each unit, each carrying 2 marks 20 marksPART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks (20% problems and 80 % theory may be asked)



SAEX1007 AIRCRAFT STRUCTURES – IL T P Credits Total Marks

2 1 0 3 100

UNIT I STATICALLY DETERMINATE STRUCTURES 10 hrs.Analysis of plane truss – Method of joints – 3 D Truss - Plane frames.

UNIT II STATICALLY INDETERMINATE STRUCTURES 10 hrs.Composite beam - Clapeyron’s Three Moment Equation - Moment Distribution Method.

UNIT III ENERGY METHODS 10 hrs.Strain Energy due to axial, bending and Torsional loads - Castigliano’s theorem - Maxwell’s Reciprocal theorem,

Unit load method - application to beams, trusses, frames, rings, etc.

UNIT IV COLUMNS 10 hrs.Columns with various end conditions – Euler’s Column curve – Rankine’s formula Column with initial curvature

- Eccentric loading – South well plot – Beam column.

UNIT V FAILURE THEORY 10 hrs.Maximum Stress theory – Maximum Strain Theory – Maximum Shear Stress Theory – Distortion Theory –

Maximum Strain energy theory – Application to aircraft Structural problems.


TEXT BOOK:1. E F Bruhn, “Analysis and Design of Flight Vehicles Structures”, 1st Tristate offset co, USA, 1985

REFERENCES:1. Timoshenko, S., “Strength of Materials”, Vol. I and II, Princeton D. Von Nostrand Co, 1990.





SAEX1008 AIRCRAFT SYSTEMS AND INSTRUMENTSL T P Credits Total Marks

3 0 3 3 100

UNIT I AIRCRAFT INSTRUMENTS 10 hrs.Flight Instrument and Navigation Instruments – Accelerometers, Air data instruments-airspeed, altitude, Vertical

speed indicators. Static Air temperature, Angle of attack, Air Speed Indicators – Mach Meters – Altimeters – GyroscopicInstruments – principles and Operation and types– Study of Various Types of Engine Instruments – Tachometers –Temperature Gauges – Pressure Gauges – Operation and Principles.

UNIT II AIRPLANE CONTROL SYSTEMS 10 hrs.Conventional Systems –Modern Flight Control Systems Control Actuation Digital Fly By Wire systems – Auto

pilot System -Active Control Technology – CCV, The Control Problem, Principles of actuation systems, Types ofactuation systems. Actuators, Valves, Servo amplifiers pick-offs, Synchronous data transmission system

UNIT III FUEL AND ENVIRONMENTALCONTROLSYSTEM 10 hrs.Fuel system – Layout, Types of fuel tanks, locations, control pressure, sequence of fuel consumption, venting

Basic Air Cycle Systems – Vapour Cycle Systems,– Evaporative Vapour Cycle systems – Evaporative air Cycle systems–Pressurization system – Principle-components-limitation- Oxygen systems – Fire Protection Systems, Deicing and AntiIcing Systems

UNIT IV AIRCRAFT SYSTEMS 10 hrs.Hydraulic Systems – Types of Hydraulic oil -and its properties. Study of Typical Workable System – Components

– Hydraulic System Components – Modes of Operation – Pneumatic Systems – Advantages – Working Principles –Components, case studies in modern aircrafts

UNIT V LANDING GEAR SYSTEMS 10 hrs.Landing Gear Systems – Classification – Purpose and types of Shock Absorbers. construction and its operation

– LG -Retraction/extension Mechanism. Brake System types, components and advantages, anti-skid system.conventional and tubeless tires construction, advantages and common defects, modern advancements in tyretechnologies

REFERENCES: 1. Mekinly, J.L. and Bent, R.D., “Aircraft Power Plants”, McGraw Hill, 1993. 2. Pallet, E.H.J., “Aircraft Instruments & Principles”, Pitman & Co., 1993. 3. Treager, S., “Gas Turbine Technology”, McGraw Hill, 1997. 4. Mckinley, K.L., and Bent, R.D., “Aircraft Maintenance & Repair”, McGraw Hill1993 5. “General Hand Books of Airframe and Power plant Mechanics”, U.S. Dept. of Transportation, Federal Aviation Administration, the

English Book Store, New Delhi, 1995. 6. James Ephraim Johnson, Electro hydraulic Servo Systems, Published by Editors of Hydraulics & pneumatics magazine, 1977. 7. Neal E.Wood et al, ‘Electro-mechanical actuation development AFFDL-TR-150’ DEC 1978.





SAEX4002 AERODYNAMICS LABL T P Credits Total Marks

0 0 4 2 100

1. Flow visualization studies using Hele shaw apparatus2. Flow visualization technique by using water flow channel3. Flow visualization studies in low speed flows over cylinders and Airfoils using wind tunnel.4. Calibration of subsonic wind tunnel.5. Pressure distribution over smooth and rough cylinder.6. Pressure distribution over symmetric airfoils.7. Pressure distribution over cambered airfoils & thin airfoils8. Study of lift drag characteristics of airfoils using wind tunnel.9. Measurement of boundary layer thickness.10. Force measurements using wind tunnel balances

SAEX 4003 AVIONICS LABL T P Credits Total Marks

0 0 2 1 50

DIGITAL SYSTEMS1. Verification of logic gates2. Verification of Boolean theorems3. Study of Half adder/Full adder4. Study of Multiplexer / De-multiplexer Circuits.5. Study of Encoder/Decoder Circuits.6. Shift Registers, Binary Comparator Circuits.DIGITAL EXPERIMENTS ON AIRCRAFT SYSTEMS1. Aircraft engine starting system by logic gates2. Aircraft landing gear position indignation and warning system3. Case study of logic trouble shooting TechniquesMICROPROCESSORS1. Addition and Subtraction of 8-bit and 16-bit numbers.2. Sorting of Data in Ascending & Descending order.3. Sum of a given series with and without carry.4. Greatest in a given series & Multi-byte addition in BCD mode.5. Interface programming with 4 digit 7 segment Display & Switches & LED’s.6. 16 Channel Analog to Digital Converter & Generation of Ramp, Square, Triangular wave by Digital to Analog Converter.AVIONICS DATA BUSES1. Study of Different Avionics Data Buses.2. MIL-Std - 1553 Data Buses Configuration with Message transfer.3. MIL-Std - 1553 Remote Terminal Configuration.

SAEX4004 AERO MODELLING LABL T P Credits Total Marks

0 0 2 1 50

1. Study about historical background of airplanes 2. Component of airplanes and its functions3. Construction of glider 4. Construction of fuselage5. Construction of wing 6. Construction of tail plane7. Assembly of a plane 8. Mounting of engine and controls9. Training in flight maneuvering through computer simulation 10. Testing of trainer flight model



SMTX1011APPLIED NUMERICAL METHODS

(Common to All Branches Except Bio Med and Bio Info)


3 1 0 4 100

UNIT I 10 hrs.

Curve Fitting-Method of group averages-Principle of least squares-Method of moments-Finite Differences-OperatorsE & D-Relationship between operators.

UNIT II 10 hrs.

Interpolation-Newton’s method-Lagrange’s method-Numerical Differentiation and Integration-Trapezoidal andSimpson’s Rule-Finite Difference Equations.

UNIT III 10 hrs.

Numerical solution of Algebraic and Transcendental Equations-Regula Falsi method-Newton Raphsonmethod-Graffe’s Root Squaring method-Simultaneous linear algebraic equations- Gauss Jordan method-Crout’smethod-Gauss Seidel method-Relaxation method.

UNIT IV 10 hrs.

Numerical solution of Ordinary Differential Equations-Taylor’s series-Modified Euler’s method-Runge Kutta methodof fourth order-Predictor-Corrector methods-Milne’s method-Adam’s Bashforth method.

UNIT V 10 hrs.

Numerical solution to Partial Differential Equations-Classification-Elliptic equations-Poisson’s equations-Leibmann’siteration procedure-Parabolic equation-Bender Schmidt Scheme-Crank Nicholson’s Scheme-Hyperbolic equations.

TEXT / REFERENCE BOOKS:1. Kandasamy P & Co., Numerical Methods, S.Chand & Co., New Delhi, 2003.2. Venkataraman M.K., Engineering Mathematics – First Year (2nd edition), National Publishing Co., 2000.3. Grewal, B.S., “Higher Engineering Mathematics” (35th Edition), Khanna Publishers, Delhi, 2000.4. Balgurusamy .E, Numerical Methods, Tata McGraw Hill, New Delhi, 2006.5. Steven C.Chapra, Raymond P. Canale, Numerical Methods for Engineers, Tata McGraw Hill, New Delhi, 2003.







SAEX1009 SUPERSONIC AERODYNAMICSL T P Credits Total Marks

3 0 0 3 100

UNIT I CONCEPTS OF COMPRESSIBLE FLOW 10 hrs.Introduction to isentropic flow-Scope of compressible flow-Review of continuity, momentum and steady flow energy

equations and entropy considerations- Energy and momentum equations for compressible fluid flow referencevelocities-stagnation states-velocity of sound-critical states-mach number-critical Mach number. Types of waves- machcones mach angle-effect of Mach number on compressibility flow regimes.

UNIT II SHOCKS AND EXPANSION WAVES 10 hrs.Development of normal shocks-governing equations-Stationery and moving normal shock waves-applications,

applications to supersonic wind tunnel. Shock tubes, Shock polars, supersonic pitot probes. Oblique shock - Reflectionof flow- Prantl- Meyer expansion flow. Under and over expanded nozzles, shock expansion method for flow overairfoils

UNIT III FLOW IN CONSTANT AREA DUCT WITH FRICTION AND HEAT TRANSFER 10 hrs.Fanno flow and Rayleigh flow - flow equations and solutions- variation of flow properties-variation of Mach

number with duct length-tables and charts for Fanno flow and Rayleigh flow

UNIT IV BRIEF INTRODUCTION TO THE METHODS OF CHARACTERISTICS 10 hrs.Method of characteristics – Prandtl - Glauert and Goethert rules - Ackeret’s supersonic airfoil theory. Small

perturbation equations for subsonic, transonic, supersonic and hypersonic flow. Experimental characteristics of Airfoilsin compressible flow.

UNIT V EXPERIMENTAL METHODS 10 hrs.Transonic, Supersonic and hypersonic wind tunnels and characteristic features, their operation and performance-

Flow visualization methods of supersonic flows.


TEXT BOOK 1. Radhakrishnan, Ethirajan., Gas Dynamics, John Wiley & Sons,2010 2. Yahya, S. M., Fundamentals of Compressible flow with Aircraft and Rocket Propulsion, 3rd edition, New Age International

Ltd.Publishers,2003

REFERENCE BOOKS: 1. Shapiro, Ascher. H., The Dynamics and Thermodynamics of Compressible Fluid Flow (Vol I and II ),Ronald Press,1953. 2. Anderson J. D., Jr., Modern Compressible Flow with Historical Perspective, McGraw Hill Publishing Co.,2004 3. Edward.R.C. Miles, Supersonic Aerodynamics, Dover, New York, 1950. 4. Clancy, L,J., Aerodynamics, Pitman, 1986 5. Anderson J. D., Jr., Fundamentals to Aerodynamics, McGraw Hill Publishing Co., 3rd edition, 2001


Max. Marks: 80 Exam Duration: 3 hrs.PART A : 2 Questions from each unit, each carrying 2 marks 20 marksPART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks (30% problems and 70% theory may be asked)



SAEX1010 AIRCRAFT STRUCTURES – IIL T P Credits Total Marks

3 1 0 4 100

UNIT I UNSYMMETRICAL BENDING 10 hrs.Bending stresses in beams of unsymmetrical sections – Bending of symmetric sections with skew loads.

UNIT II SHEAR FLOW IN OPEN SECTIONS 10 hrs.Thin walled beams, Concept of shear flow, shear centre, Elastic axis. With one axis of symmetry, with wall

effective and ineffective in bending, unsymmetrical beam sections.

UNIT III SHEAR FLOW IN CLOSED SECTIONS 10 hrs.Bredt – Batho formula, Single and multi – cell structures. Approximate methods. Shear flow in single & multi-cell

structures under torsion. Shear flow in single and multi-cell under bending with walls effective and ineffective.

UNIT IV BUCKLING OF PLATES 10 hrs.Thin Plate theory-Pure bending of thin plates, plates subjected to bending and twisting. Rectangular sheets

under compression, Local buckling stress of thin walled sections, Crippling stresses by Needham’s and Gerard’smethods, Thin walled column strength. Sheet stiffener panels. Effective width, inter rivet and sheet wrinkling failures.

UNIT V STRESS ANALYSIS IN WING AND FUSELAGE 10 hrs.Procedure – Shear and bending moment distribution for semi cantilever and other types of wings and fuselage,

cut- outs in fuselages. Thin webbed beam. With parallel and non parallel flanges, Shear resistant web beams, Tensionfield web beams (Wagner’s). Airframe loads-Inertia, Maneuver, Gust load


Text Book:1. Peery, D.J., and Azar, J.J., “Aircraft Structures”, 2nd edition, McGraw–Hill, N.Y., 1993.

REFERENCE BOOKS:1. Megson, T.M.G., “Aircraft Structures for Engineering Students”, Butterworth-Heinemann,2007.2. Elmer Franklin Bruhn. “Analysis and Design of Flight vehicles Structures”, Jacobs Publication,19733. Rivello, R.M., “Theory and Analysis of Flight Structures”, McGraw-Hill, 1993.4. C. T. Sun, Mechanics of Aircraft Structures, Wiley-Inter Science Publication,2006





SAEX1011 EXPERIMENTAL STRESS ANALYSISL T P Credits Total Marks

3 0 0 3 100

UNIT 1 MEASUREMENTS 10 hrs.Principles of measurements-Accuracy, Sensitivity and range of measurements. Measurement of force or load,

Measurement of torque., Strain measurement of rotating shaft, Measurement of pressure or vacuum.

UNIT II EXTENSOMETERS 10 hrs.Mechanical, Optical, Acoustical and Electrical extensometers and their uses, Advantages and disadvantages.

Review of bridge circuits

UNIT III ELECTRICAL RESISTANCE STRAIN GAUGES 10 hrs.Principle of operation and requirements-Types and their uses-Materials for strain gauge. Calibration and

temperature compensation-cross sensitivity, Rosette analysis –Delta, Tee, rectangular Rosette -- Wheatstone bridgeand potentiometer circuits for static and dynamic strain measurements- strain indicators. Charecteristics of straingauges-Trasverse sensity of gauge, Temperature effect.

UNIT IV THEORY OF PHOTOELASTICITY 10 hrs.Electromagnetic wave representation of light, ,polarization, refraction, stress and birefringence, Isoclinic and

Isochromatic fringe analysis. Stress analysis by two and three dimensional photoelasticity-interpolation of stresspatterns-Typical applications-Description and uses of reflection polariscope

UNIT V NON-DESTRUCTIVE TESTING 10 hrs.Fundamentals of NDT-Radiography-ultrasonics -Magnetic particle inspection- Fluorescent penetrant technique-

Eddy current testing- Acoustic Emission Technique-Fundamentals of brittle coating methods- Introduction to Moiretechniques- Holography- Ultrasonic C-Scan- Thermography, Fibre-optic Sensors.


TEXT BOOKS 1. Dally, J. W., and Riley, W. F., Experimental Stress Analysis, McGraw Hill Inc., New York, 1978. 2. Hetyenyi, M., Hand Book of Experimental Stress Analysis, John Wiley and Sons Inc., New York, 1972. 3. Experimental stress analysis – Dr. Sadhu Singh., Khanna Publications. 4. James Doyle, Modern Experimental Stress Analysis: completing the solution of partially specified problems. John Wiley & Sons,

Ltd, 2004

REFERENCE BOOKS 1. Srinath, L. S., Raghava, M.R., Lingaiah, K.Gargesha, G.Pant B., and Ramachandra, K., Experimental Stress Analysis, Tata McGraw

Hill, New Delhi, 1984. 2. Pollock, A. A., Acoustic Emission in Acoustics and Vibrations Progress, ed. by Stephens R.W.B.,Chapman and Hall, 1983.


Max. Marks: 80 Exam Duration: 3 hrs.PART A : 2 Questions from each unit, each carrying 2 marks 20 marksPART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks (90% Theory and 10% Problems may be asked)



SAEX1012 AIRCRAFT PERFORMANCEL T P Credits Total Marks

3 0 0 3 100

UNIT I FORCE AND DRAG 10 hrs.International Standard Atmosphere, Forces and moments acting on a vehicle in flight. Equations of motion of a

rigid flight vehicle Various types of drags. Drag polar of vehicles from low speeds to hypersonic speeds.

UNIT II AIR BREATHING ENGINES AND ROCKETS 10 hrs.Review of the variation of thrust/power and SFC with altitude and velocity, for various air breathing engines and

rockets.

UNIT III UNACCELERATED FLIGHT 10 hrs.Performance of airplane in level flight, range, endurance. glide, climb, Maximum speed in level flight - Conditions

for minimum drag and power required

UNIT IV ACCELERATED FLIGHT 10 hrs.Accelerated flight, turn, maneuvers, take-off and landing. Flight limitations of pull up and push over - V-n diagram

and load factor

UNIT V FLIGHT TESTING 10 hrs.Flight - testing: Altitude definitions, Speed definitions, Air speed, altitude and temperature measurements. Errors

and calibration. Measurement of engine power, charts and corrections. Flight determination of drag polar.


TEXT BOOKS1. Edward Lewis Houghton, N. B. Carruthers, Aerodynamics for Engineering Students, Butterworth-Heineman,20032. Anderson J. D., Jr., Airplane Performance and Design, McGraw Hill Publishing Co., 1999

REFERENCE BOOKS1. Jan Roskam, chuan- Tau Edward Lan, Airplane Aerodynamics and Performance, DAR Corporation, 2007.2. Warren. F. Phillips, Mechanics of Flight, John Wiley and Sons, 2004.3. Bandu N.Pamadi, Performance, Stability, Dynamics and Control of Airplane, AIAA,20044. Donald Layton, Aircraft Performance, Matrix Publications, 19885. W. Austyn Mair, David L. Birdsall, Aircraft Performance, Cambridge Aerospace series, 1996


Max. Marks: 80 Exam Duration: 3 hrs.PART A : 2 Questions from each unit, each carrying 2 marks 20 marksPART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks (40 % problems and 60 % theory may be asked)



SAEX1013 AIRFRAME MAINTENANCE & REPAIR PRACTICESL T P Credits Total Marks

3 0 0 3 100

UNIT I WELDING IN AIRCRAFT STRUCTURAL COMPONENTS 10 hrs.Equipments used in welding shop and their maintenance – Ensuring quality welds – Soldering and Brazing.

UNIT II SHEET METAL REPAIRS AND MAINTENANCE 10 hrs.Inspection of damage – Classification – Repair or replacement – Sheet metal inspection – N.D.T Testing –

Riveted repair design, Damage investigation, Types of plastics, Maintenance and repair of plastic components, Reversetechnology. Repair of cracks, holes etc., and various repairs schemes – Scopes. Inspection – Repair of compositecomponents – Special precautions – Autoclaves.

UNIT III AIRCRAFT JACKING, ASSEMBLY AND RIGGING 10 hrs.Airplane, Jacking and Weighing and C.G. Location. Rigging of control surfaces – Inspection, maintenance.

Helicopter flight controls, Tracking and balancing of main rotor.

UNIT IV REVIEW OF HYDRAULIC AND PNEUMATIC SYSTEM 10 hrs.Trouble shooting theory and Procedure, Inspection and maintenance of Hydraulic, Pneumatic, Fuel, Landing

gear, Inspection and maintenance of Air conditioning, Pressurization systems Oxygen, De-icing, Fire ProtectionInstallation and maintenance of instruments – Handling - Testing – Inspection, Position and warning system AuxiliaryPower Units (APUs)

UNIT V SAFETY PRACTICES 10 hrs.Safety – Importance of Flight Safety, Maintenance of Ground Support Equipments, refueling, de-refueling, fire

equipments, Hazardous materials storage and handling, Environmental and shop cleanliness – precautions, Aircraftfurnishing -practices, Equipments, Hazard zones.


TEXT BOOK1. Micheal J. Kroes, Alfred Watkins, Frank Delp, Aircraft Maintenance and Repair, 6th edition, McGraw Hill, New York, 1993

REFERENCE BOOKS1. Larry Reithmeir, Aircraft Repair Manual – Palamar Books, Marquette, 1992.2. Brimm D.J.Bogges H.E., Aircraft Maintenance – Pitman Publishing Corp. New York, 1940.3. Howard Curtis, Antonio Fillippone, Aerospace Engineering Reference, Butterworth – Heinmann, 20094. Micheal .J. Kroes, James .R. Rardon, Aircraft : Basic Science with Student Study Guide, McGraw Hill, 20075. Douglas. S. Carmody, Airplane Maintenance & Repair : A Manual for Owners, Builders, Technicians & Pilots, McGraw,1997





SAEX1014 CONTROL SYSTEMS FOR AIRCRAFTL T P Credits Total Marks

3 0 0 3 100

UNIT I INTRODUCTION TO AFCS 10 hrs.Historical review - control systems applications in aircrafts, missiles, spacecrafts – aircraft flight control

systems-models representations – open loop and closed loop -effects of feedback – Transfer function-- Block diagramrepresentation of control systems, Reduction of block diagrams, Signal flow graph representations with applicationsand problems in aircraft control, systems

UNIT II MODEL REPRESENTATIONS 10 hrs.mathematical models of physical systems - Simple pneumatic, hydraulic and thermal systems-–

Mechanical-Electrical systems – Analogies introduction to state space –concept of state variables and state modelsand derivation of state models from block diagram with reference to aircraft models

UNIT III TIME RESPONSE AND STEADY STATE ERRORS 10 hrs.Response of systems to different inputs viz., Step input, impulse, ramp, parabolic and sinusoidal inputs, Time

response of first and second order systems, steady state errors and error constants of unity feedback circuit. Automaticcontrols systems – Controllers - P, PI, PID controllers in aircraft FCS

UNIT IV CONCEPT OF STABILITY & ROOT LOCUS TECHNIQUES 10 hrs.Characteristic equation, location of roots in S-plane, Concept of stability -Routh - Hurwitz criteria of stability -

relative stability, Nyquist stability Criterion, Root locus Techniques – construction of root loci, problems in AFCS domain

UNIT V FREQUENCY RESPONSE & APPLICATIONS 10 hrs.Frequency response of the systems – correlation between time and frequency response – gain and phase

margins – bode plot method, Applications & problems in Aircrafts Flight control systems


TEXT BOOK:1. Katsuhiko Ogata, “Modern Control Engineering”, Pearson, New Delhi. 20102. Pallet, E.H.J. “Automatic Flight Control”, Shroff Publishers, India, 2004

REFERENCES:1. Gene F. Franklin, J. D. Powell, Abbas E, Feedback Control of Dynamic Systems, 6th edition, Pearson, 20092. Benjamin C. Kuo, Farid Golnaraghi, Automatic control systems, Volume 1, 8th Ed, John Wiley & Sons, 20033. Norman S. Nise, Control Systems Engineering,4th edition, John Wiley, New Delhi,20044. Richard C. Dorf, Robert H. Bishop, Modern control systems, 11th edition, Prentice Hall India, 20085. Rao V. Dukkipati., Analysis and design of control systems using MATLAB, New Age International Publishers,India,2006.6. Brian D.H, D. T. Valentine, Essential MATLAB for engineers and scientists, 4th ed, Butterworth Heinemann, 20097. Roger Pratt, Flight control systems, Institution of Electrical Engineers, United Kingdom, UK, 2000.





SAEX4005 AEROSPACE STRUCTURES LABL T P Credits Total Marks

0 0 4 2 100

1. Bending tests, Stress and deflections of beams for various end conditions,

2. verification of Maxwell’s theorem

3. Castiglianos theorems, Influence coefficients.

4. Compression tests on long and short columns, Critical buckling loads, South well plot.

5. Tests on riveted and bolted joints.

6. Unsymmetrical Bending of a Cantilever Beam

7. Combined bending and Torsion of a Hollow Circular Tube

8. Material Fringe Constant of a Photoelastic Model

9. Shear Centre of a Channel Section (open section)

10. Free Vibration of a Cantilever Beam-

11. Wagner beam – Tension field beam

12. Determination of Stresses in the Pressure Vessels

13. Computational Methods involving Aerospace Structures

14. Shear Centre of a Channel Section- closed section

SAEX 4006 COMPUTATION LABL T P Credits Total Marks

0 0 2 1 50

Using MATLAB / Maples / X-plane / Flight-Gear & Aerosim or any equivalent software

1. programs to perform Calculus 2. programs to perform Vectors and Matrices

3. Plotting Graphs 4. Solving Linear Systems

5. M Files – Variables, Loops, 6. MATLAB Graphics

7. Partial – Fraction expansion 8. Transformation of Mathematical Equations

9. Transient Response Analysis 10. Root-Locus Plots

11. Frequency Response Analysis – bode plots 12. Simulink Models – AFCS

13. Problems in Aerodynamics, Solid Mechanics, thermodynamics, Fluid Dynamics may be given as experiments

SAEX4007 AIRCRAFT SYSTEMS LABL T P Credits Total Marks

0 0 2 1 50

1. Aircraft “Jacking Up” procedure 2. Aircraft “Leveling” procedure

3. Control System “Rigging check” procedure 4. Aircraft “Symmetry Check” procedure

5. Flow test” to assess of filter element clogging 6. Aircraft rudder control

7. Hydraulically operated landing Gear 8. Electrically operated Flap Control

9. Aircraft fuel system, oil systems. 10. “Brake Torque Load Test” on wheel brake units

11. “Pressure Test” To assess hydraulic External/Internal Leakage

12. “Functional Test” to adjust operating pressure of hydraulic systems.

13. “Pressure Test” procedure on fuel system components

14. Maintenance and rectification of snags in hydraulic and fuel systems.

15. Removal stroke installation of wheels and brakes and overhauling of brake units.

(Modern Computational methods may be used)



SMEX1017RESOURCE MANAGEMENT TECHNIQUES

(Common to All Branches)


3 0 0 3 100

UNIT I INTRODUCTION AND LINEAR PROGRAMMING 10 hrs.

Operations Research(OR)-Nature-Characteristics-Phases.-Role of OR in Decision making- Outline of OR ModelsLinear Programming – Formulation of L.P.problems –Solution by graphical method, simplex method, and big M methods– Applications of O.R. in production management

UNIT II TRANSPORTATION AND ASSIGNMENT MODEL 10 hrs.

Transportation problem – Initial feasible solution- Northwest corner method, Least Cost method, Vogel’sapproximation method – Test for optimality-MODI method

Assignment problems- Hungarian assignment models- Travelling salesman problems

UNIT III RESOURCE SCHEDULING AND NETWORK ANALYSIS 10 hrs.

Problem of Sequencing – Problem with N jobs and 2 machines, 3 jobs and M machines. Project Management– Basic concepts – Case studies – Network construction and scheduling, Program evaluation and resource levelingby network techniques, time – Cost trade off.

UNIT IV INVENTORY CONTROL AND SIMULATION 10 hrs.

Inventory Control – Various Types of inventory models – deterministic inventory models – Production model,Purchase model– with and without shortage- EOQ – Buffer stock – Shortage quantity, Probabilistic inventory models– Quantity Discount and Price Breaks Simulation – Use, advantages & limitations, Monte –Carlo simulation, applicationto queuing, inventory & other problems

UNIT V QUEUEING THEORY, GAME THEORY AND REPLACEMENT MODELS 10 hrs.

Queuing theory – Poisson arrivals and exponential service times, Single channel models only. Game theory-Payoff matrix, competitive games with pure strategy, minimax criterion, principles of dominance &mixed strategiesReplacement policy for items whose maintenance cost increases with time- Consideration of money value- Replacementpolicy- Individual, Group replacement of items that fail completely

TEXT BOOK:1. Kanti Swarup, P.K.Gupta, & Manmohan., Operations Research – S. Chand & Sons.

REFERENCE BOOKS:1. K.V.Mital and C.Mohan,” Optimization Methods in O.R and System Analysis “, New Age International Publishers.2. S.D.Sharma,”Operations Research”, Kedarnath Ramnath& Co, 2002.3. Hamdy A. Taha,” Operations Research”, 5th Edn., PHI, 19954. Hiller & Liberman,”Introduction to operation research”, 5th Edn., McGraw Hill, 2001.5. Ravindran,Phillips&Solberg, “Operations Research: principles and practice”, 2nd Edn., Wiley India Lts, 2007







SAEX1015 AIRCRAFT STABILITY AND CONTROLL T P Credits Total Marks

3 0 0 3 100

UNIT I BASIC CONCEPTS 10 hrs.Aircraft Axis System, Coordinate Transformation, Aircraft Force Equations, Moment Equations, Basic Concept Of

Stability And Control, Longitudinal And Lateral- Directional Equations, Kinematic Equation

UNIT II LONGITUDINAL DYNAMIC STABILITY AND CONTROL 10 hrs.Stick - fixed stability, control effectiveness, hinge moment, tabs, aerodynamic balancing, effects of freeing the

stick. Control forces and force gradients. Critical conditions for stability and control.

UNIT III MANEUVERABILITY 10 hrs.Effect of maneuvers. Longitudinal dynamic stability, equations of motion of a disturbed aircraft, stability derivatives,

characteristic equation for stick fixed case, modes and stability criterion, effect of freeing the stick.

UNIT IV DYNAMIC STABILITY 10 hrs.Brief description of lateral and directional dynamic stability- spiral, divergence and Dutch roll. Response, automatic

control, autorotation and spin. Determination Of Neutral Points And Maneuver Points In Flight Tests

UNIT V MODERN CONTROL THEORY 10 hrs.Classical Vs modern control theory, introduction – state-space modeling, canonical transformation, controllability

and observability, state-feedback design, application of modern control theory to aircraft autopilot design- stabilityaugmentation, autopilot design, state observer, optimal control, problems . Introduction to aircraft autopilot design usingclassic control theory. Introduction to nonlinear problems in aircraft flight dynamics - Inertia coupling. - High angle ofattack phenomena - Flexibility effects -Divergence.


TEXT BOOKS1. Perkins, C, D.,and Hage, R,E., Airplane Performance, Stability and Control, Wiley Toppan, 1974.2. Babister, A, W., Aircraft Stability and Response, Pergamon Press,1980.

REFERENCE BOOKS1. Thomas R. Yechout, ‘An introduction to Aircraft Flight Mechanics’, AIAA educational Series; 2003.2. Bernard Etkin, Lloyd Duff Reid, Dynamics of Flight, Stability & Control, 3rd ed, John Wiley & Sons, 19953. Bandu N. Pamadi, ‘Performance, Stability, Dynamics and Control of Airplanes’, AIAA 2nd Ed, 2004.4. Malcom J Abzug, E E. Larrabee, Airplane Stability & Control , 2nd ed, Cambridge University Press,, 20025. Nelson. R.C., Flight Stability and Automatic Control, McGraw Hill, 1989.6. Louis. V. Schmidt, Introduction To Aircraft Flight Dynamics,AIAA,2002





SAEX1016 PROPULSION – IL T P Credits Total Marks

3 0 0 3 100

UNIT I FUNDAMENTALS OF GAS TURBINE ENGINES 10 hrs.Basic concepts of air standard cycles .Illustration of working of gas turbine engine - Air-standard Brayton cycle,

actual gas turbine engine cycle The thrust equation - Factors affecting thrust - Effect of pressure, velocity andtemperature changes of air entering compressor - Methods of thrust augmentation – Characteristics of turboprop,turbofan and turbojet - Performance characteristics.

UNIT II SUBSONIC AND SUPERSONIC INLETS FOR JET ENGINES 10 hrs.Internal flow and Stall in Subsonic inlets - Boundary layer separation - Major features of external flow near a

subsonic inlet - Relation between minimum area ratio and external deceleration ratio - Diffuser performance -Supersonicinlets - Starting problem in supersonic inlets - Shock swallowing by area variation – External deceleration - Modes ofinlet operation.

UNIT III COMBUSTION CHAMBERS 10 hrs.Classification of combustion chambers - various arrangements, simplex and duplex burners. line design Important

factors affecting combustion chamber design – Combustion process - Combustion chamber performance - effect of operatingvariables on performance - Flame tube cooling- Flame stabilization - Use of flame holders - Numerical problems.

UNIT IV NOZZLES 10 hrs.Theory of flow in isentropic nozzles – design, Convergent nozzles and nozzle choking - Nozzle throat conditions

Nozzle efficiency - nozzle operating characteristics for isentropic flow, nozzle flow and shock waves Losses in nozzles- Over expanded and under-expanded nozzles - Ejector and variable area nozzles - Interaction of nozzle flow withadjacent surfaces - Thrust reversal.

UNIT V PROPELLERS 10 hrs.Ideal momentum theory and blade element theory and their relative merits, numerical problems on the

performance of propellers using propeller charts, selection of propellers, fixed, variable and constant speed propellers,prop-fan, material for propellers, shrouded propellers helicopter, rotor in hovering.


TEXT BOOKS 1. Philip Hill and Carl Peterson, Mechanics and Thermodynamics of Propulsion, 2nd Edition, Addison -Wesley Publishing Company,

Singapore, 1992

REFERENCE BOOKS1. Rolls-Royce, Jet Engine, 3rd edition, 1983.2. Oates, G,C., Aerothermodynamics of Aircraft Engine Components, AIAA Education Series, New York,1985.3. Cohen, H, Rogers., G.F.C. and Saravanamuttoo, H.I.H., Gas Turbine Theory, Longman, 1989.4. Mattingly, J.D., Heiser, W.H., and Pratt, D.T., Aircraft Engine Design, AiAA Education Series, New York, 2002.5. Thomas. A. Ward, Aerospace Propulsion Systems, John Wiley & Sons,20106. Aircraft Gas Turbine Engine- operations, Components & Systems, (Jet Propulsion), Wexford, 2008.7. Ahmed F. El-Sayed, Aircraft propulsion and gas turbine engines, CRC Press, 20088. Tony Giampaolo, Gas turbine handbook: principles and practice, The Fairmont Press, Inc., 2009

UNIVERSITY EXAM QUESTION PAPER PATTERNMax. Marks: 80 Exam Duration: 3 hrs.PART A : 2 Questions from each unit, each carrying 2 marks 20 marksPART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks (50% problems and 50 % theory may be asked)



SAEX1017 FINITE ELEMENT METHODL T P Credits Total Marks

3 1 0 4 100

UNIT I INTRODUCTION 10 hrs.FEM- Examples Areas of Application- General Steps in Finite Element Analysis- Examples of Finite Element

Modeling

UNIT II ONE DIMENSIONAL PROBLEMS 10 hrs.Direct stiffness method – spring element- Derivation of the stiffness matrix- Example of a spring

assemblage-Assembly of global stiffness matrix-Types of boundary conditions- The Potential energy approach –ExamplesPrismatic bar under axial loading- bending of beams Introduction- Finite Element Modeling – Element Division-Numbering Scheme- Coordinate and Shape Functions- The Potential Energy Approach- Assembly of Global StiffnessMatrix and Load Vector- Treatment of Boundary Conditions- Temperature Effects- Shear Force and Bending Moment-Examples.

UNIT III TWO DIMENSIONAL PROBLEMS 10 hrs.Plane truss structure-Introduction- Plane Trusses-Coordinate Transformation – Local & Global Coordinate- The

Element Stiffness Matrix- Stress Calculations- Temperature Effects -Examples plane stress & strain – cst element–Introduction- Finite Element Modeling-Constant Strain Triangle (CST)- Isoparametric Representation- Potential EnergyApproach - Element Stiffness; Force Terms Stress Calculations- Temperature Effects- Examples

UNIT IV SCALAR FIELD PROBLEMS 10 hrs.One-dimensional steady-state heat transfer- Introduction- One-Dimensional Heat Conduction- The Governing

Equation-Boundary Conditions- The One-Dimensional Element- Functional Approach – The Element Conductivity Matrixand Heat Rate Vector- Heat Flux Boundary Conditions; Examples one-dimensional heat transfer in thin fins –Introduction- The Governing Equation - The Boundary Conditions- The Convection Matrix and Heat Rate Vector; GlobalSystem of Liner Equations; Example

UNIT V FINITE ELEMENT MODELING & SOFTWARE 10 hrs.Finite element modeling- Rectangular Plate- Plane Stress & Plane Strain Condition-Pipe Under Internal Pressure-

Axisymmetric Condition- Symmetry Consideration MSC nastran software – Introduction- Analysis steps in Nastran-Laboratory sessions (depending on availability of laboratory facilities.)


REFERENCE BOOKS 1. T. R. Chandrupatla and A. D. Belegundu, “Introduction to Finite Elements in Engineering”, 2nd Edition, Prentice Hall, New Jersey,

1997. 2. Daryl L. Logan, “A First Course in the Finite Element Method”, 2nd Edition, PWS Publishing Company, Boston, 1993. 3. Dr. S. S. Rao, ”The Finite Element Method In Engineering”, Pergamon Press, 1989 4. K. H. Huebner, D. L. Dewhirst, D. E. Smith and T. G. Byron, “The Finite Element Method for Engineers”, 4th Edition, John Wiley

& Sons Inc., New York, 2001. 5. J. N. Reddy, “An Introduction to the Finite Element Method”, 2nd Edition, McGraw-Hill,Inc., New York, 1993. 6. Concepts and Applications of Finite Element Analysis: COOK. D. Robert. Malus. S.David, Plesha E.Michel, John wilely & sons 3rd

Ed. New York, 2000

UNIVERSITY EXAM QUESTION PAPER PATTERN:Max.Marks: 80 Exam Duration: 3 hrs.PART A : 2 Questions from each unit, each carrying 2 marks 20 marksPART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks (80% Problems and 20% Theory may be asked)



SAEX4008 AIRCRAFT STRUCTURAL REPAIR & PRACTICE LABL T P Credits Total Marks

0 0 4 2 100

1. Introduction to aircraft structural repairs and preparation of repair scheme

2. Flaring of aluminum tubes

3. Patch repair on transparent plastics

4. Repair of panels by insertion patch repair.

5. Repair by splicing on wooden spares

6. Tube bending

7. Make channel section by hand forming Riveting practices : Lap joint, Butt Joint

8. Gas Welding, Arc Welding, TIG Welding, MIG Welding, Spot Welding

9. Introduction to Modern methods in aircraft structural repair practices

SAEX 4009 PROPULSION LABL T P Credits Total Marks

0 0 4 2 100

1. Study of an aircraft piston engine. (Includes study of assembly of sub systems, various components, their functions and operating principles)

2. Study of an aircraft jet engine (Includes study of assembly of sub systems, various components, their functions and operating principles)

3. Modeling of Hybrid Rockets 4. Modeling of Supersonic ramjet

5. Heat Transfer by forced Convection 6. Heat Transfer by natural Convection

7. Saybolt Viscometer 8. Redwood Viscometer

9. Cleveland flash and Fire Point apparatus (Open cup)

10. Pensky martin flash and Fire Point apparatus (Closed cup)

11. Junker’s Gas Calorimeter 12. Bomb Calorimeter

13. Modeling of Pulse jet Engine 14. Cascade Testing

15. Computational Methods in Propulsion 16. Characteristic study of free jet

17. Characteristic study of wall jet

SAEX 4010 AIRCRAFT DESIGN PROJECTL T P Credits Total Marks

0 0 4 2 100

1. Comparative studies of different types of airplanes and their specifications and performance details.

2. Preliminary weight estimations, selection of main parameters, Power plant selection, Aerofoil selection, Wing, tailand control surfaces.

3. Preparation of lay outs of balance diagram and three view drawings.

4. Drag estimation, Detailed performance, Calculations and stability estimates. V-n diagram.

5. Preliminary design of an Aircraft wing – Shrenck’s curve, structural load distribution, shear force, bending momentand torque diagrams

6. Detailed design of an aircraft wing – design of spars and stringers, bending stress and shear flow calculations– buckling analysis of wing panels.

7. Preliminary design of an aircraft fuselage – load distribution on an aircraft fuselage.

8. Detailed design of an aircraft fuselage – design of bulkheads and longerons – bending stress and shear flowcalculations – buckling analysis of fuselage panels.

9. Preparation of a detailed design report with CAD drawings

(Modern Computation Design methods can be used)



SBAX1001PRINCIPLES OF MANAGEMENT AND

PROFESSIONAL ETHICSL T P Credits Total Marks

3 0 0 3 100

UNIT I MANAGEMENT FUNCTIONS & STRUCTURE 10 hrs.

Management – Definition – Basic Function – Contribution of Taylor & Fayol. Types of structure – Line, staff,Functional, Committee, Project & Matrix – Structures.

Departmentalization – Centralization – Decentralization – span of control. Management By Objectives –Management By Exception.

UNIT II MANAGEMENT OF ORGINASATION 10 hrs.

Forms of Business / Industrial Ownership – Sole Trader, Partnership, Company, Performance Appraisal – BasicPrinciples – Pitfalls – Methods to Overcome. Industrial Safety – Causes of Accidents – Cost of Accident – How tominimize Accidents. Plant Layout & Maintenance – Need, Types & Managerial Aspects.

UNIT III ORGANISATIONAL BEHAVIOUR 10 hrs.

OB – Definition – Nature & Scope – Contributing Disciplines – Importance of OB to Managers. Personality –Definition – Theories – Factors Influencing Personality. Motivation – Definition – Theories. Theory X & Y – TransactionalAnalysis. Morale & Job Satisfaction – Factors Influencing Job Satisfaction.

UNIT IV GROUP DYNAMICS 10 hrs.

Group – Definition – Types – Determinants of Group Cohesiveness – Communication – Process – Barriers –Effective Communication. Leadership Theories – Factors Contributing to Effective Leadership – Role of Trade Unionin Organizations – Functions of Trade Union – Why Trade Union is required? – Types of Trade Union.

UNIT V PROFESSIONAL ETHICS 10 hrs.

Ethics in Workplace – Formulation of Ethics – Managerial Ethics – Managing Ethical Behaviour – Codes ofEthics – Encouraging Ethical Behaviour – Social Responsibility – Spirituality.

TEXT / REFERENCE BOOKS1. Gupta C.B., Management Theory and Practice, 14th Edition, Sultan Chand & Sons, 2009.2. Dr. Prasad L.M., Principle & Practice of Management, 7th Edition, Sultan Chand & Sons, 2008.3. Aswathappa, Organisational Behaviour, 8th Edition, Himalaya Publishing House, 2010.4. Dr. Prasad L.M., Organisational Behaviour, 4th Edition, Sultan Chand & Sons, 2008.5. Harold Koontz, Principles of Management, 1st Edition, Tata McGraw Hill, 2004.







MEX1018 HEAT AND MASS TRANSFERL T P Credits Total Marks

3 1 0 4 100

(Use of Heat transfer data book, steam table are permitted)UNIT I CONDUCTION 10 hrs.

Basic Concepts – Mechanism of Heat Transfer – Conduction, Convection and Radiation – General Differentialequation of Heat Conduction – Fourier Law of Conduction – Cartesian and Cylindrical Coordinates – One DimensionalSteady State Heat Conduction – Conduction through Plane Wall, Cylinders and Spherical systems – CompositeSystems-critical thickness of insulation – Conduction with Internal Heat Generation – Extended Surfaces – UnsteadyHeat Conduction – Lumped Analysis – Infinite and Semi Infinite Solids

UNIT II CONVECTION 10 hrs.

Basic Concepts – Convective Heat Transfer Coefficients – Boundary Layer Concept – Forced Convection –External Flow – Flow over Plates, Cylinders Spheres and Bank of tubes – Internal Flow – Free Convection – Flowover Vertical Plate, Horizontal Plate, Inclined Plate, Cylinders and Spheres.

UNIT III PHASE CHANGE HEAT TRANSFER AND HEAT EXCHANGERS 10 hrs.

Nusselt’s theory of condensation- Regimes of pool boiling and flow boiling, correlations in boiling andcondensation. Heat Exchanger Types – Overall Heat Transfer Coefficient – Fouling Factors – Analysis – LMTD method,– NTU method.

UNIT IV RADIATION 10 hrs.

Basic Concepts, Laws of Radiation – Wiens Displacement Law – Stefan Boltzman Law, Kirchoff Law – BlackBody Radiation – Grey body radiation – Shape Factor – Electrical Analogy – Radiation Shields.

UNIT V MASS TRANSFER 10 hrs.

Basic Concepts – Diffusion Mass Transfer – Fick’s Law of Diffusion – Steady state Molecular Diffusion –Convective Mass Transfer – Momentum, Heat and Mass Transfer Analogy – Convective Mass Transfer Correlations.

TEXT BOOK:1. Yunus A. Cengel, “Heat Transfer A Practical Approach”, Tata Mc Graw Hill, 20042. R.K.RAJPUT,” Heat and Mass transfer”, S.Chand & Co

REFERENCES:1. Frank P. Incropera and David P. Dewitt, “Fundamentals of Heat and Mass Transfer”, John Wiley & Sons, 1998.2. C.P.KOTHANDARAMAN” Fundamentals of Heat and Mass Transfer”, New Age International (P) Ltd., 19983. R.C.SACHDEVA, “Fundamentals of Heat and Mass Transfer”, New Age Internationals (P) Ltd.4. N.M.OZISIK,” Heat Transfe”, McGraw Hill Book Company, 1988.5. J.P.HOLMAN “Heat Transfer “, McGraw Hill Book Company, 19896. R.Yadav,” Heat and Mass Transfer”, Central Publishing House, 1995.







SAEX 1018 PROPULSION IIL T P Credits Total Marks

3 0 0 3 100

UNIT I TURBINES 10 hrs.Introduction to turbine analysis, mean radius stage calculations, stage parameters, stage loading and flow

coefficients degree of reaction, stage temperature ratio and pressure ratio, blade spacing, radial variation, velocity ratio.Axial flow turbine, stage flow path, Dimensional stage analysis.; Steps of turbine design: single stage and two stages.Turbine performance. Blade cooling

UNIT II COMPRESSOR 10 hrs.Principal of operation of centrifugal compressor - Work done and pressure rise Euler’s Turbo machinery equations.

Axial flow compressor analysis, cascade action, flow field. Euler’s equation, velocity diagrams, flow annulus area stageparameters. Degree of reaction, cascade airfoil nomenclature and loss coefficient, diffusion factor, stage loading andflow coefficient, stage pressure ratio, Blade Mach No., repeating stage, repeating row

UNIT III RAMJET PROPULSION 10 hrs.Operating principle – Subcritical, critical and supercritical operation - Combustion in ramjet engine – Ramjet

performance - Sample ramjet design calculations - Introduction to scramjet - Preliminary concepts in supersoniccombustion - Integral ram rocket - Numerical problems.

UNIT IV FUNDAMENTALS OF ROCKET PROPULSION 10 hrs.Operating principle - Specific impulse of a rocket - Internal ballistics - Rocket nozzle classifications – Rocket

performance considerations - Numerical problems. Electric, ion, Nuclear rocket propulsion -Principles

UNIT V CHEMICAL ROCKETS 10 hrs.Solid propellant rockets - Selection criteria of solid propellants - Important hardware components of solid rockets

- Propellant grain design considerations - Liquid propellant rockets - Selection of liquid propellants Thrust control inliquid rockets - Cooling in liquid rockets - Limitations of hybrid rockets - Relative advantages of liquid rockets oversolid rockets –Numerical Problems


TEXT BOOKS1. Philip Hill, and Carl Peterson, Mechanics and Thermodynamics of Propulsion, 2nd edition, Pearson Education Ltd, 2009.2. Mathur, M., and Sharma, R. P., Gas Turbines and Jet and Rocket Propulsion, Standard Publishers, New Delhi, 1988.3. Gorden, C. V., Aerothermodynamics of Gas Turbine & Rocket Propulsion, AIAA Education Series, New York, 1997

REFERENCE BOOKS1. George .P .Sutton, Oscar Biblarz, Rocket Propulsion Elements, John Wiley & Sons Inc., New York, 5th Ed., 20102. Cohen, H., Rogers, G. F. C. and Saravanamuttoo, H.I.H., Gas Turbine Theory, Prentice Hall India Ltd, 20013. Mattingly, J.D., Heiser, W. H., and Pratt, D. T., Aircraft Engine Design, AIAA Education Series, New York, 2002.4. Saced Farokhi, Aircraft Propulsion, Volume 10,John Wiley & sons, 20085. Ahmed F.El-Sayed, Aircarft Propulsion & Gas Turbine Engine, CRC Press, 2008


Max. Marks: 80 Exam Duration: 3 hrs.PART A : 2 Questions from each unit, each carrying 2 marks 20 marksPART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks (30% Problems and 70% Theory may be asked)



SAEX 1019 THEORY OF VIBRATIONSL T P Credits Total Marks

3 1 0 4 100

UNIT I INTRODUCTION 10 hrs.Simple harmonic motion, definition of terminologies, Review of Newton’s, Laws, D’Alembert’s principle, Energy

methods

UNIT II SINGLE DEGREE OF FREEDOM SYSTEM 10 hrs.Free vibrations free damped vibrations, forced excitations with and without damping, support excitation, vibration

measuring instruments

UNIT III TWO-DEGREE OF FREEDOM SYSTEMS 10 hrs.Two degrees of freedom systems, Static and dynamic couplings, vibration absorber, Principal coordinates, Principal

modes, orthogonality conditions. Hamilton’s Principle, Lagrangean equation and applications.

UNIT IV THREE DEGREES OF FREEDOM 10 hrs.Three degrees of freedom systems, Static and dynamic couplings Principal modes, orthogonality conditions,- For

coupled systems – Dunkerley’s method, Rayleigh Ritz method- Applications.

UNIT V VIBRATIONS OF ELASTIC BODIES 10 hrs.Vibrations of elastic bodies, String or stretched cord, Longitudinal vibration, Lateral vibration, Torsional vibration.

Approximate methods for calculating natural frequencies. Eigen value extraction methods – Subspace hydration method,Lanczos method – Eigen value reduction method – Dynamic response of large systems – Implicit and explicit methods

(Computational problems must be given as assignments for each unit)Total No hours: 50

TEXT BOOKS1. William T Thomson, “Theory Of Vibration With Applications, Taylor & Francis, 1993

REFFERENCES1. S.Singiresu Rao, Mechanical Vibrations, 5th edition, Pearson Education, Canada, 20102. Ramamurti, V., Mechanical Vibration Practice with Basic Theory, 1st edition, Narosa Publishing House, Chennai, 20003. Meirovitch, L., “Elements of Vibration Analysis”, McGraw-Hill Inc., 1986.4. Francis Sing Tse, Ivan .E. Morse and Rolland Theodore Hinkle, “Mechanical Vibrations”, Prentice Hall of India, 1984.5. Fung, Y.C., “An Introduction to the Theory of Aeroelasticity”, John Wiley & Sons Inc., New York, 1985.6. Rao.J.S. and Gupta K., “Theory and practice of Mechanical Vibrations” Wiley Eastern Ltd., New Delhi.,1999.7. Timoshenko,S., “Vibration Problems in Engineering”, John Wiley & Sons Inc., 19878. Jan R Wright, Jonathan E Copper, Introduction to Aircraft Aeroelasticity & Loads, John n Wiley & Sons, 20079. Robert . C.Sapri, Mechanical Vibrations : Measurements, Effects & Control, Nova Science Publishers, 200910. S.Graham Kelly, Mechanical Vibrations, Schuam’s Outlines, Tata Mc GRaw Hill, 2007





SAEX 1020 AIRCRAFT COMPOSITE MATERIALSL T P Credits Total Marks

3 0 0 3 100

UNIT I INTRODUCTION AND COMPOSITE FUNDAMENTALS 10 hrs.Types of Composites; Why composites; History of applications, Nano, Micro and Macro behavior of composites

Anisotropic and tailored-made properties Fundamental reinforcing mechanisms Key differences between compositesand metals-Properties and functions of fibers and Matrix. Advantages and application of composite materials–Generalized Hooke’s Law – Elastic constants for anisotropic, orthotropic and isotropic materials

UNIT II METHODS OF ANALYSIS 10 hrs.Micro mechanics – Mechanics of materials approach, elasticity approach to determine material properties – Macro

Mechanics – Stress-strain relations with respect to natural axis, arbitrary axis – Determination of material properties.Experimental characterization of lamina - Problems

UNIT III CLASSICAL LAMINATION THEORY AND FAILURE ANALYSIS 10 hrs.In-plane forces, bending and twisting moments, Derivation of classical lamination theory, Shear coupling in

unbalanced laminates Bending and stretching of unsymmetric laminates Failure criteria for composites- Maximumstress/strain criteria, Tsai- Hill criterion, Tsai-Wu criterion–Example problems

UNIT IV HYGROTHERMAL BEHAVIOR OF COMPOSITES AND SANDWICH CONSTRUCTION 10 hrs.Hygrothermal stress-strain relations for a lamina General CLT with hygrothermal effects Hygrothermal effects on

material properties -Skill check problems .Basic concepts of sandwich construction -Materials used for sandwichconstruction - Failure modes of sandwich panels.

UNIT V FABRICATION PROCESS 10 hrs.Various Open and closed mould processes. Manufacture of fibers – Types of resins and properties and

applications – Netting analysis.


TEXT BOOKS1. Autar K.Kaw Mechanics of Composite Materials, CRC Press 19972. Jones, R. M., Mechanics of Composite Materials, 2nd Edition, Taylor & Francis, Philadelphia, PA, 1999

REFERENCES1. Agarwal, B.D., and Broutman, L.J., “Analysis and Performance of Fibre Composites”, John Wiley and sons. Inc., New York, 1995.2. Lubin, G., “Handbook on Advanced Plastics and Fibre Glass”, Von Nostrand Reinhold Co., New York, 1989.3. Niu, Michael, Composite Airframe Structures, Conmilit Press, 19924. Alan.A.Baker,Stuart Dutton, Donald Kelly, Donald W.Kelly Composite Materials for Aircraft Structures,AIAA,20045. Calcote, L R. “The Analysis of laminated Composite Structures”, Von – Noastrand Reinhold Company, New York 1998.





SAEX 1021 ROCKETS AND MISSILESL T P Credits Total Marks

3 0 0 3 100

UNIT I ROCKETS SYSTEM 10 hrs.Ignition System in rockets - types of Igniters - Igniter Design Considerations - Design Consideration of liquid

Rocket Combustion Chamber, Injector Propellant Feed Lines, Valves, Propellant Tanks Outlet and Helium Pressurizedand Turbine feed Systems - Propellant Slash and Propellant Hammer - Elimination of Geysering Effect in Missiles -Combustion System of Solid Rockets.

UNIT II AERODYNAMICS OF ROCKETS AND MISSILES 10 hrs.Airframe Components of Rockets and Missiles - Forces Acting on a Missile While Passing Through Atmosphere

- Classification of Missiles - methods of Describing Aerodynamic Forces and Moments - Lateral Aerodynamic Moment- Lateral Damping Moment and Longitudinal Moment of a Rocket - lift and Drag Forces - Drag Estimation - BodyUpwash and Downwash in Missiles - Rocket Dispersion - Numerical Problems.

UNIT III ROCKET MOTION IN FREE SPACE AND GRAVITATIONAL FIELD 10 hrs.One Dimensional and Two Dimensional rocket Motions in Free Space and Homogeneous Gravitational Fields -

description of Vertical, Inclined and Gravity Turn Trajectories - Determination of range and Altitude SimpleApproximations to Burnout Velocity.

UNIT IV STAGING AND CONTROL OF ROCKETS AND MISSILES 10 hrs.Rocket Vector Control – Methods, SITVC termination, Thrust determination, Multi staging of rockets - Vehicle

Optimization - Stage Separation Dynamics - Separation Techniques, Types of aerodynamics control in missiles

UNIT V MATERIALS FOR ROCKETS AND MISSILES 10 hrs.Selection of Materials - Special Requirements of Materials to Perform under Adverse Conditions.


TEXT BOOK:1. Sutton, G.P., et al., “Rocket Propulsion Elements”, John Wiley & Sons Inc., New York, 1993.

REFERENCE BOOKS:1. Mathur, M., and Sharma, R.P., “ Gas Turbines and Jet and Rocket Propulsion”, Standard Publishers, New Delhi 1998.2. Cornelisse, J.W., “ Rocket Propulsion and Space Dynamics”, J.W., Freeman & Co. Ltd., London, 1982.3. Parket, E.R., “ Materials for Missiles and Spacecraft”, McGraw-Hill Book Co. Inc., 1982.


Max. Marks: 80 Exam Duration: 3 hrs.PART A : 2 Questions from each unit, each carrying 2 marks 20 marksPART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks (30% Problems and 70% Theory may be asked)



SAEX 1022AIRCRAFT ENGINE MAINTENANCE & REPAIR

PRACTICESL T P Credits Total Marks

3 0 0 3 100

(A) INSPECTION, MAINTENANCE, OPERATION AND TROUBLE SHOOTING OF PISTON ENGINESUNIT I PISTON ENGINE 10 hrs.

Types of piston engines – Principles of operation – Function of components – Materials used – Details ofstarting the engines – Details of carburetion and injection systems for small and large engines – Ignition systemcomponents – Spark plug details – Engine operating conditions at various altitudes –Lubrication system, Maintenanceand inspection checks to be carried out.

Inspection and maintenance and troubleshooting – Inspection of all engine components – Daily and routinechecks – Overhaul procedures – Compression testing of cylinders – Special inspection schedules – Engine fuel, controland exhaust systems – Engine mount and super charger.UNIT II PROPELLER 6 hrs.

General Inspection procedures – checks on constant speed propellers – Pitch setting – Engine starting procedure,Installation and maintenance checks.UNIT III FAILURE & FAULT DIAGNOSIS 10 hrs.

Symptoms of failure – Fault diagnostics – Case studies of different engine systems – Rectification during testingequipments for overhaul: Tools and equipment requirements for various checks and alignment during overhauling –visualinspection – methods and instruments for non destructive testing techniques. Engine testing: Engine testing proceduresand schedule preparation – on line maintenance.(B) INSPECTION, MAINTENANCE, OPERATION AND TROUBLE SHOOTING OF JET ENGINES:UNIT IV 14 hrs.

Types of jet engines – Principles of operation – Function of components – Details of starting and operating procedures– gas turbine engine inspection and check ups. – use of instruments for on line maintenance – special inspection procedures:foreign object damage and blade damage, lubrication, fuel and pneumatic systems, engine surge and stall

Gas turbine engine Schedule & Non schedule maintenance procedures of gas turbine – trouble shooting andrectification procedures – system maintenance procedures.

Engine Testing and storage: gas turbine testing procedures – test schedule procedure – storage of engine –preservation and de-preservation procedures.UNIT V 10 hrs.

Engine overhaul – Overhaul procedures- inspection and cleaning of the components – repair schedules foroverhaul- balancing of gas turbine components

Trouble shooting: procedures for trouble shooting – condition monitoring of the engine on ground and at flight– engine health monitoring and corrective methods.

TEXT BOOK: 1. Michael J. Kroes, Aircraft power plants - Aviation technology series, 7th Edition, McGraw-Hill, 1990 2. Dale Crane, Aviation Maintenance Technician: Powerplants, 2nd edition, Aviation Supplies & Academics Inc,2005REFERENCE BOOKS: 1. Turbomeca, “Gas turbine engines”, The English Book Store, New Delhi, 1993. 2. Ujited Technologies Pratt & Whitney, “Aircraft Gas turbine engine and its operation, The English Book Store, New Delhi, 1993 3. Treager, Aircraft: Gas Turbine Engine Technology, Tata McGraw-Hill, 2002 4. Ralph .D. Bent, James .L. McKinsley, Aircraft & Powerplants, Gregg Division, McGraw Hill, 1985 5. Larry Reithmaier, Lawrence .W. Reithmaier, Standard Aircraft Handbook for Mechanics and Technicians, McGraw Hill Professional, 6th Edition, 1999 6. Douglas .S.Carmody, Airplane Maintenance & repair : Manual for owner, builders, technicians & pilots, McGraw Hill Publishing,1997 7. Jeppesen Sanderson, Standard Aviation Maintenance Handbook, Jeppesen & Company, 2003 8. Dale Crane, Aviation Maintenance Handbook, Aviation Supplies & Academics Inc,2006 9. R .P. Chatteerjee, Airforce Maintenance & Planning, Pentagon Press, 2010

UNIVERSITY EXAM QUESTION PAPER PATTERNMax. Marks: 80 Exam Duration: 3 hrs.PART A : 2 Questions from each unit, each carrying 2 marks 20 marksPART B : 2 Questions from each unit with internal choice, each carrying 12 marks 60 marks



SAEX 4011 COMPOSITE STRUCTURES LABL T P Credits Total Marks

0 0 2 1 50

1. Fabrication of glass epoxy laminates using vacuum bag method2. Fabrication of Carbon polyster laminate using compression moulding3. Fabrication of glass fiber filament wound pipes using filament winding machine4. Calculation of material properties of bi directional composite laminate5. Determination of material properties of cross ply laminate6. Determination of shear modulus of composite laminate7. Fabrication of sandwich beam8. Determination interlaminar strength of a composite laminate9. Failure analysis of composite laminate using matlab10. Determination of material properties using plate theory.

SAEX 4012AIRCRAFT ENGINE MAINTENANCE AND REPAIR

PRACTICES LABL T P Credits Total Marks

0 0 2 1 50

1. Stripping of a piston engine2. Engine (Piston Engine) - cleaning, visual inspection, NDT checks.3. Piston Engine Components - dimensional checks.4. Piston – Engine reassembly.5. Propeller Pitch Setting, Propeller Blade, Vertical, horizontal Balancing6. Stripping of a jet engine7. Jet Engine – identification of components and defects.8. Jet Engine – NDT checks and dimensional checks9. Jet Engine – reassembly.10. Engine starting procedures.

S26XPROJ PROJECT WORK & VIVA VOCEL T P Credits Total Marks

0 0 30 15 100

The objective of the project work is to make use of the knowledge gained by the student at various stages ofthe degree course. Students, will also be permitted to undertake industrial/consultancy project Work, outside thedepartment, in industries/Research labs.

There shall be three assessments during the semester by a review committee. The student shall make threepresentations on the progress made before the committee at various stages of the Project work. The Head of theDepartment shall constitute the review committee for each branch of study. The total marks obtained in the threereviews, shall be taken in to account. There will be a viva-voce examination at the end of the Project work, conductedby one internal examiner and one external examiner. The total marks secured will be the sum of marks secured inthe Project reviews and Viva Voce Examination.

Each student is required to submit a Project report on the project assigned to him by the department. Thereport should be based on the information available in the literature or data obtained by the student by way ofexperiments conducted in the laboratory/industry.



SAEX 1023 COMPUTATIONAL FLUID DYNAMICSL T P Credits Total Marks

3 0 0 3 100

UNIT I GOVERNING EQUATIONS 10 hrs.Introduction — Various applications, Governing equations — continuity, momentum, energy equations, Boundary

conditions

UNIT II MATHEMATICAL BEHAVIOUR OF PARTIAL DIFFERENTIAL EQUATIONS 10 hrs.Mathematical Behavior of Partial differential equations- Hyperbolic, Parabolic, Elliptic equations, Well posed

problems, Difference equations, Explicit and Implicit approach, Errors and analysis of stability

UNIT III GRID GENERATION 10 hrs.Grid generation: general transformation of the equations, Matrices and Jacobians, Stretched and compressed

grids, Boundary fitted coordinate systems, Modern developments in grid generation — Finite volume mesh generation,unstructured meshes and Cartesian meshes

UNIT IV SOLUTION TECHNIQUES 10 hrs.Simple CFD Techniques: The Lax — Wendroff Technique, MacCornmack’s Technique, The relaxation Technique

and its use with low speed invicid flow, Artificial viscosity, Alternating Direction Implicit (ADI) Technique, Pressurecorrection Techniques, courant

UNIT V EXAMPLES WITH DIFFERENT METHODS 10 hrs.Solved Problems, Finite Volume Techniques, first order upwind, second order upwind


TEXT BOOK 1. J. D.Anderson, Computational Fluid Dynamics, McGraw Hill International, 1995.

REFERENCE BOOKS 1. Versteeg, H. K., and Malalasekera W., An Introduction to Computational Fluid Dynamics the Finite Volume Method, Addison Wes ley

Longman Limited, 1995. 2. Patankar, S.V., Numerical Heat Transfer and Fluid Flow, Hemispher Publishing Corporation, 1980.





SAEX 1024 WIND TUNNEL TECHNIQUESL T P Credits Total Marks

3 0 0 3 100

UNIT I PRINCIPLES OF MODEL TESTING 10 hrs.Buckingham Theorem – Non Dimensional Numbers – Scale Effect of Similarites.

UNIT II WIND TUNNELS 10 hrs.Classification – Special Problems of Testing in Subsonic, Transonic, Supersonic and Hypersonic Speed Regions

– Layouts – Sizing and Design Parameters.

UNIT III CALIBRATION OF WIND TUNNELS 10 hrs.Test Section Speed – Horizontal Buoyancy – Flow Angularities – Turbulence Measurements – Associated

Instrumentation – Calibration of Supersonic Tunnels.

UNIT IV WIND TUNNEL MEASUREMENTS 10 hrs.Pressure and Velocity Measurements - Force Measurements – Three Component and Six Component Balances

– Internal Balances.

UNIT V FLOW VISUALIZATION 10 hrs.Smoke and Tuft Grid Techniques – Dye Injection Special Techniques – Optical Methods of Flow Visualization.


REFERENCE BOOKS:1. Pope, A., and Goin, L., “High Speed Wind Tunnel Testing”, John Wiley, 1985.2. Rae, W.H., and Pope, A., “Low Speed Wind Tunnel Testing”, John Wiley Publication, 1984.





SAEX 1025 AIRCRAFT DESIGNL T P Credits Total Marks

3 0 0 3 100

UNIT I REVIEW OF DEVELOPMENTS IN AVIATION 10 hrs.Categories and types of aircrafts – various configurations – Layouts and their relative merits – strength, stiffness,

fail safe and fatigue requirements – Manoeuvering load factors – Gust and manoeuverability envelopes – Balancingand maneuvering loads on tail planes.

UNIT II POWER PLANT TYPES AND CHARACTERISTICS 10 hrs.Characteristics of different types of power plants – Propeller characteristics and selection – Relative merits of

location of power plant.

UNIT III PRELIMINARY DESIGN 10 hrs.Selection of geometric and aerodynamic parameters – Weight estimation and balance diagram – Drag estimation

of complete aircraft – Level flight, climb, take – off and landing calculations – range and endurance – static anddynamic stability estimates – control requirements.

UNIT IV SPECIAL PROBLEMS 10 hrs.Layout peculiarities of subsonic and supersonic aircraft – optimisation – of wing loading to achieve desired

performance – loads on undercarriages and design requirements.

UNIT V STRUCTURAL DESIGN 10 hrs.Estimation of loads on complete aircraft and components – Structural design of fuselage, wings and

undercarriages, controls, connections and joints. Materials for modern aircraft – Methods of analysis, testing andfabrication.


TEXT BOOKS1. D.P. Raymer, “Aircraft Conceptual design”, AIAA Series, 1988.2. G. Corning, “Supersonic & Subsonic Airplane Design”, II Edition, Edwards Brothers Inc., Michigan, 1953.3. E.F. Bruhn, “Analysis and Design of Flight Vehicle Structures”, Tristate Offset Co., U.S.A., 1980.

REFERENCES1. E. Torenbeek, “Synthesis of Subsonic Airplane Design”, Delft University Press, London, 1976.2. H.N.Kota, Integrated design approach to Design fly by wire” Lecture notes Interline Pub. Bangalore, 1992.3. A.A. Lebedenski, “Notes on airplane design”, Part-I, I.I.Sc., Bangalore





SAEX 1026 HELICOPTER AERODYNAMICSL T P Credits Total Marks

3 0 0 3 100

UNIT I ELEMENTS OF HELICOPTER AERODYNAMICS 10 hrs.Configuration based on Torque Reaction – Jet Rotors and Compound Helicopters – Method of Control – Collective

and Cyclic Pitch Changes – Lead – Lag and Flapping Hinges.

UNIT II IDEAL ROTOR THEORY 10 hrs.Hovering performance – Momentum and Simple Blade Element Theories – Figure of Merit – Profile and Induced

Power Estimation - Constant Chord and Ideal Twist Rotors.

UNIT III POWER ESTIMATES 10 hrs.Induced, Profile and Parasite Power requirements in Forward Flight – Performance Curves with Effects of Altitude

– Preliminary Ideas on Helicopter Stability.

UNIT IV LIFT, PROPULSION AND CONTROL OF V/STOL AIRCRAFT 10 hrs.Various Configuration – Propeller, Rotor, Ducted Fan and Jet Lift – Tilt Wing and Vectored Thrust – Performance

of VTOL and STOL Aircraft in Hover, Transition and Forward Motion.

UNIT V GROUND EFFECT MACHINES 10 hrs.Types – Hover Height, Lift Augmentation and Power Calculation for Plenum Chamber and Peripheral Jet Machine

– Drag of Hovercraft on Land and Water. Applications of Hovercraft.


REFERENCE BOOKS:1. Gessow,A., Aerodynamics of Helicopter, MacMillan & CO ., N.Y., 19872. McCormick. B.W., Aerodynamics of V/STOL Flight, Academic Press, 19873. Johnson. W., Helicopter Theory, Princeton University Press, 19804. Seddon. J. ., Sion Newton, Basic Helicopter Aerodynamics, Blackwell Science, 20025. Gordon. J. Leishman, Principles of Helicopter Dynamics, Cambridge University press, 20066. Raymon W. Prouty, Helicopter Aerodynamics, PJS Publications, 19857. Gupta, L., “Helicopter Engineering”, Himalayan Books, 1996.





SAEX 1027 ADVANCED FLIGHT DYNAMICSL T P Credits Total Marks

3 0 0 3 100

UNIT I 10 hrs.Atmospheric and space flight –modeling and simulation-attitude and kinematics of of ordinate frames – basic

definitions and vector operations-coordinate systems and rotation matrix-Euler axis and principal angle-Euler angles-Eulersymmetric parameters ( quaternion)-Rodrigues parameters –Gibbs vectors-attitude kinematics

UNIT II 10 hrs.Newton’s law of gravitation –gravity of an asymmetric planet-gravitational anomalies-Particle kinematics in moving

plane-Newton’s law of motion –energy, movements and angular movements –two body problem

UNIT III 10 hrs.Celestial frame and orbital elements –planet fixed frame –lamberts problem- perturbation acceleration-effects of

planetary oblateness - effects of atmospheric drag-numerical solution to perturbed problem-three body problem-equationsof motion langrage solution-restricted three body problem

UNIT IV 10 hrs.Atmospheric and trajectory trajectories – equations of motion –airplane flight paths- long range cruising flight

–steady wind on airplane-take off maneuver-rocket ascent trajectories

UNIT V 10 hrs.Euler equation for a rotational motion-rotational kinematic energy-principal body frame –torque free rotation of

spacecraft – attitude motion in atmospheric flight –implementation of control systems elements-single axis closed loopattitude control-multi axis closed loop attitude control-Six-degrees of freedom simulation-wing rock motion of a aircraftsimulation


REFERENCE BOOKS 1. Ashish tewari, atmospheric and space flight dynamics: modeling and simulation with Matlab and Simulink, Birkhauser, spinger

international edition,2007. 2. Pamadi, B. “Performance, stability, dynamics and control of airplanes”, AIAA 2004. 3. Etkin, B. and Reid L.D. “Dynamics of Flight-Stability and Control” 3rd edition, John Wiley, 1996. 4. Stengel, R.F. “Flight dynamics” Princeton University Press, Princeton, N.J., USA, 2004. 5. Kaplan, Marshall H., Modern Spacecraft Dynamics and Control, John Wiely & Sons, New York. 1976 6. Wiesel, William E., Spaceflight Dynamics, Tata McGraw Hill Publishing Company Limited, New Delhi. 1997 7. Thomson, William T., Introduction to Space Dynamics, Dover Publication, Inc. New York. 1986 8. Sidi, Marcel J., Spacecraft Dynamics and Control, Cambridge University Press, U.K. 2000





SAEX 1028 HELICOPTER MAINTENANCEL T P Credits Total Marks

3 0 0 3 100

UNIT I HELICOPTER FUNDAMENTALS 10 hrs.Basic directions – Ground handling, bearings – Gears, construction of fuselage and tail boom.

UNIT II MAIN ROTOR SYSTEM 10 hrs.Head maintenance – blade alignment – Static main rotor balance – Vibration – Tracking-– Span wise dynamic

balance – Blade sweeping –Electronic balancing – Dampener-maintenance – Counter weight adjustment – Auto rotationadjustments – Mast & Flight-Control Rotor - Mast – Stabilizer, dampeners – Swash plate flight control systems Collective– Cyclic – Push pull tubes – Torque tubes – Bell cranks – Mixer box –Gradient unit control boosts – Maintenance& Inspection control rigging.

UNIT III MAIN ROTOR TRANSMISSIONS 10 hrs.Engine transmission coupling – Drive shaft – Maintenance clutch – Free wheeling units –Spray clutch – Roller

unit – Torque meter – Rotor brake – Maintenance of components – vibrations and monitoring systems- Mountingsystems – Transmissions.

UNIT IV POWER PLANTS & TAIL ROTORS 10 hrs.Fixed wing power plant modifications – Installation – Different type of power plant maintenance. Tail rotor system

– Servicing tail rotor track – System rigging.

UNIT V AIRFRAMES AND RELATED SYSTEMS 10 hrs.Fuselage maintenance – Airframe Systems – Special equipment, types of undercarriages and their operations.

TEXT BOOK 1. Jeppesen, “Helicopter Maintenance”, Jeppesen and Sons Inc., 2000.,

REFERENCES 1. “Civil Aircraft Inspection Procedures”, Part I and II, CAA, English Book House, New Delhi, 1986. 2. Larry Reithmier, “Aircraft Repair Manual”, Palamar Books Marquette, 1992.





SAEX 1029 AIR TRANSPORT AND AIRCRAFT MAINTENANCEL T P Credits Total Marks

3 0 0 3 100

UNIT I INTRODUCTION 10 hrs.Development of air transportation, comparison with other modes of transport – Role of IATA, ICAO – The

general aviation industry, airline – Factors affecting general aviation, use of aircraft, airport: airline management andorganisation – levels of management, functions of management, Principles of organizations, planning the organisation– chart, support departments & line departments.

UNIT II AIRLINE ECONOMICS 10 hrs.Forecasting – Fleet size, Fleet planning, fleet commonality, factors affecting choice of fuels, aircraft evaluation,

the aircraft selection process, operating cost, passenger capacity, load factor etc. – Passenger fare and tariffs –Influence of geographical, economic & political factors on routes, route selection and capital acquisition.

Valuation & Depreciation – Budgeting, Cost planning – Aircrew evaluation – Route analysis

UNIT III PRINCIPLES OF AIRLINES SCHEDULING 10 hrs.Equipment maintenance, Flight operations and crew scheduling, Ground operations and facility limitations,

equipments and types of schedule – hub & spoke scheduling, advantages / disadvantages & preparing flight plans –Aircraft scheduling in line with aircraft maintenance practices.

UNIT IV AIRCRAFT RELIABILITY 10 hrs.Aircraft reliability and alert level determination – The maintenance schedule & its determinations – hardtime, On

condition, Condition monitoring maintenance– Extended range operations (EROPS) & ETOPS – Ageing aircraftmaintenance production.

UNIT V TECHNOLOGY IN AIRCRAFT MAINTENANCE 10 hrs.Airlines scheduling (with reference to engineering) – Product support and spares – Maintenance sharing –

Equipments and tools for aircraft maintenance – Aircraft weight control – Budgetary control. On board maintenancesystems – Engine monitoring – Turbine engine oil maintenance –Turbine engine vibration monitoring in aircraft – Lifeusage monitoring – Current capabilities of NDT – Helicopter maintenance – Future of aircraft maintenance.

TEXT BOOKS1. Fedric J.H., “Airport Management”, 2000. 2. C.H. Friend, “Aircraft Maintenance Management”, 2000.

REFERENCES 1. Gene Kropf, “Airline Procedures”. Himalayan Book house 19492. Wilson & Bryon, “Air Transportation”. 20063. Philip Locklin D, “Economics of Transportation”. Richard D. Irwing 19724. “Indian Aircraft manual” – DGCA Pub. 19755. Alexander T Wells, “Air Transportation”, Wadsworth Publishing Company, California, 1993.





SAEX 1030 AIRCRAFT RULES AND REGULATIONSL T P Credits Total Marks

3 0 0 3 100

UNIT I C.A.R. SERIES ‘A’ & SERIES ‘B’ 10 hrs.Responsibilities of operators / owners – Procedure of CAR issue, amendments etc., – Objectives and targets

of airworthiness directorate – Airworthiness regulations and safety oversight of engineering activities of operators.

C.A.R. Series ‘B’ – Issue Approval of Cockpit Check List, MEL, CDL - Deficiency list (MEL and CDL) – Preparationand use of cockpit checklist and emergency list.

UNIT II C.A.R. SERIES ‘C & SERIES ‘D’ 10 hrs.Defect recording, reporting, investigation, rectification and analysis – Flight report – Reporting and rectification

of defects observed on aircraft – Analytical study of in-flight readings and recordings – Maintenance control by reliabilityMethod.C.A.R. Series ‘D’ – Aircraft Maintenance Programme - Reliability Programmes (Engines) – Aircraft maintenanceprogramme and their approval – On condition maintenance of reciprocating engines – TBO – Revision programme –Maintenance of fuel and oil uplift and consumption records – Light aircraft engines – Fixing routine maintenanceperiods and component TBOs – Initial and revisions.

UNIT III C.A.R. SERIES ‘E’ & SERIES ‘F’ 10 hrs.Approval of organizations in categories A, B, C, D, E, F, and G – Requirements of infrastructure at stations

other than parent base. C.A.R. Series ‘F’ – Air Worthiness and Continued Air Worthiness - Procedure relating toregistration of aircraft – Procedure for issue / revalidation of Type Certificate of aircraft and its engines / propeller;Issue / revalidation of certificate of airworthiness – Requirements for renewal of certificate of airworthiness.

UNIT IV C.A.R. SERIES ‘I’,‘L’, ’M’ ,’ S’ AND SERIES ’R’ 10 hrs.Issue of AME License – Classification and experience requirements – Mandatory modifications/inspections.

UNIT V C.A.R. Series ‘T’ & Series ’X’ 10 hrs.Flight testing of (Series) aircraft for issue of C of A – Flight testing of aircraft for which C of A had been

previously issued –Registration Markings of aircraft – Weight and balance control of an aircraft – Provision of first aidkits and physician’s kit in an aircraft – Use furnishing materials in an aircraft – Concessions – Aircraft log books–Document to be carried on board on Indian registered aircraft – Procedure for issue of tax permit – Procedure forissue of type approval of aircraft components and equipment including instruments, CAR’M’- CAR-145.

TEXT BOOKS1. Anonymous, “Civil Aviation Requirements with Latest Amendment (Section 2Airworthiness)”, DGCA Publications, 2000.2. Aeronautical Information Circulars (relating to Airworthiness), DGCA Publications, 2000.

REFERENCES1. Anonymous, “Aircraft Manual (India) Volume-II”, Latest Edition, The English Book Store, 17-1, Connaught Circus, 20032. Advisory Circulars from DGCA 2008.





SAEX 1031 AIRLINE OPERATIONS AND MANAGEMENTL T P Credits Total Marks

3 0 0 3 100

UNIT I INTRODUCTION 10 hrs.Introduction to Transportation – Modes – Modal Competition – The Economic Importance – Transportation and

Economic Development – Transport as a Factor of Production – International Transportation– Importance of InternationalTransportation – Logistics Management – Concepts and Types of Aviation –History of Civil Aviation Industry – AviationTechnology Transformation (1930 – 2003) – Scope of Aviation

UNIT II INDUSTRY 10 hrs.Aircraft Manufacturers – Introduction - Airbus Industries, Civilian Products, Competition with Boeing –New

Generation Aircraft – About the Airbus A-380 – The Boeing Company – Airline Market Projection (2000-2020 &2004-2024) – Economy and Aviation - Air Transport and the Economy – Benefits of Air Transports

UNIT III MANAGEMENT 10 hrs.Aviation Management Structure – Introduction – Operational Management – Era of Open Skies Policies –

Overview of Airline Industry – International and Domestic Air Traffic – Financial Performance of Airlines – NewEconomic Model for Airline Business – Outlook Muted for Legacy Carriers – Infrastructure Management – AirportPlanning Management

UNIT IV AIRSPACE MANAGEMENT 10 hrs.Aircraft Characteristics – Airport Capacity Management – Terminal Management – Apron Management– Size

of Airport Infrastructure – Airports and their Economics in National Economic Growth and Development –IndianScenario – Global Emerging Trends of Airport Infrastructure Industry – Global Study on Airport Performance – ModernAviation Infrastructure Business Trend – Airspace Management – Airports and Airspace Congestion Issues –Regulatory Management

UNIT V GROWTH & DEVELOPMENT 10 hrs.International Civil Aviation Organization (ICOA) - Introduction – Objectives – Strategic Planning – Annexes –

International Air Transport Association (IATA) – Aims – Two Tier Systems – Growth and Development – World TradeOrganization – World Tourism Organization – Federal Aviation Administration (FAA) – Civil Aviation Authority (CAA)-EASA (European Aviation Security Agency) – Director General of Civil Aviation (DGCA) – Functions -Concepts ofBilateral, Multilateral and Plurilateral in Air Trade Agreements – Major Factors that Converge Private Sector Initiatives– Modern Airline Trends – Liberalization in Air Transport – Potential Paths to Further Liberalization – Privatization inIndian Civil Aviation Industry – Deregulation in Indian Air Pocket – Airport Internalization – Basic Principle behindPrivatization – Airport Privatization – Forms of Airport Privatization – Airport Privatization Models – Causes – Objectives– Airport Ownership and Governance Models – Airport Privatization in India – Road Map for the Civil Aviation Sector

(Computational problems must be given as assignments for each unit)TEXT BOOKS1. P.S. Senguttuvan, “Fundamentals of Air Transport Management”, Excel Books, First Edition 2006

REFERENCE1. Allan Rossmore, Airline Operations :An Inside View 2000, 2, illustrated, Kellmark Aeronautics, Incorporated, 2000.2. Massoud Bazargan, Airline operations and scheduling, Ashgate Publishing Limited, Hampshire, England, 2008.3. Alexander T. Wells, Seth B. Young, Airport planning & management, McGraw-Hill, 2004.





SAEX 1032 AIRCRAFT MAINTENANCE MANAGEMENTL T P Credits Total Marks

3 0 0 3 100

UNIT I AIRLINE ECONOMICS AND MAINTENANCE COST 10 hrs.

Airline economics and the aircraft – Principles of airlines economics – Cost of aircraft maintenance.

UNIT II SCHEDULES AND CONSTRAINTS 10 hrs.

Aircraft reliability –The maintenance schedules and its determinations–hardtime, on condition, conditions monitoredmaintenance – Extended range operations (EROPS) & ETOPS – Ageing aircraft. Maintenance, corrosion preventionprogramme

UNIT III MAINTENANCE PRODUCTION 10 hrs.

Airline scheduling (with reference to engineering) – Product support and spares – Maintenance sharing –Equipments and tools for aircraft maintenance – Aircraft weight control – Budgetary control, man power allocation.

UNIT IV COMPUTER IN AIRCRAFT MAINTENANCE 10 hrs.

Computer in aircraft maintenance – Artificial intelligence – Aircraft maintenance software’s.

UNIT V TECHNOLOGY IN AIRCRAFT MAINTENANCE 10 hrs.

On board maintenance system – engine monitoring – Turbine engine oil maintenance – Turbine engine vibrationmonitoring in aircraft – life usage monitoring – current capabilities of NDT – Helicoper maintenance – Future of aircraftmaintenance, aircraft loadable softwares- navigation data system, TCAS, EGPWS, EICAS.

TEXT BOOKS1. C.H. Friend, Aircraft Maintenance Management, Longman, 19932. K.C.Batra,Production Managemen, Stringer, UK, 20053. Richordson J.D., Essential of Airlines Management Kendral Hunt, 19954. Banfe Charles F., Airline Management, Englewood Cliffs, N J – Prentice Hall 1992

REFERENCES1. D.Philip Locklin, Economics of Transportation2. Taneja Nawal K, Airlines in Transition Lexington, Mass, D.C.Health 1981.


Max. Marks: 80 Exam Duration: 3 hrs.





SAEX 1033 COMPUTER AIDED DESIGN AND ANALYSISL T P Credits Total Marks

3 0 0 3 100

UNIT I INTRODUCTION TO CAD 10 hrs.Introduction to Design process - CAD. Geometric Modeling: Types - Wireframe, surface and solid modeling.

Solid modeling techniques: CSG and B-rep - Operations: Boolean - Extrude - Sweep - Revolve. Entities - Line -Circle - Ellipse - Parabola - Cubic Spline, Bezier and B-spline.

UNIT II GRAPHICS TRANSFORMATIONS AND DISPLAY FUNCTIONS 10 hrs.Coordinate systems - Transformations: translation, scaling, reflection, rotation - Concatenated transformation -

Inverse transformation. Hidden line removal - Shading - Colouring - Rendering - Animation (Basic treatment only).

UNIT III SOFTWARE PACKAGES AND TECHNOLOGY 10 hrs.Commercial solid modeling packages: Important features - Technical comparison - Modules and tools - Format

of data exchange standards. Brief outline of feature technology: Classification of features - Design by features -Applications of features - Advantages and limitations - Brief outline of Parametric technology.

UNIT IV FEM INTRODUCTION 10 hrs.Introduction - Steps involved in FEA: Nodes - Elements and their types, shape function, constraints, forces and

nodal displacements - Stiffness matrix - Solution techniques. Analysis of spring element. Simple problems involvingstepped bar subject to axial loading and simple structural members with triangular element.

UNIT V ANALYSIS FEA in CAD Environment: 10 hrs.Stages of FEA in CAD environment - Preprocessor - Solver and postprocessor. Demonstration of the above

using any one commercial packages. Brief outline of kinematic analysis - Manufacturability analysis and simulation(Basic treatment only).


TEXT BOOKS1. Ibrahim Zeid, CAD/CAM - Theory and Practice, Tata Mc Graw-Hill, New Delhi, 20012. Radhakrishnan. P., CAD / CAM / CIM - New age international, 20003. Chairs McMahon and Jimmie Browne, CAD/CAM, Addision Wesly, New York, 2000

REFERENCE BOOKS1. Chandupatla and Belagundu, Introduction to Finite Element Methods in Engineering, Prentice Hall of India Private Limited, New Delhi 19972. Newman and Sproull R. F., Principles of interactive computer graphics, Tata Mc Graw-Hill, New Delhi, 19973. Mikell P. Groover, CAD/CAM, Prentice Hall of India Private Limited, New Delhi, 1997





SAEX 1034 AIRCRAFT MATERIALSL T P Credits Total Marks

3 0 0 3 100

UNIT I ELEMENTS OF MATERIAL SCIENCE 10 hrs.Structure of Solid Materials – Atomic structure Crystal Structure – Imperfections In Crystals.

UNIT II MECHANICAL BEHAVIOUR OF ENGINEERING MATERIALS 10 hrs.Linear and Non-linear Elastic Properties – Mechanism of Elastic and Inelastic Action – Yielding, Strain Hardening,

Fracture, Elastic After Effect Bauchinger’s Effect, Testing and Flaw Detection of Material and Components by mechanicaland NDT checks

UNIT III HEAT TREATMENT & CORROSION 10 hrs.Heat Treatment of Carbon Steel, Aluminum Alloy, Magnesium Alloy and Titanium Alloy used in Aircraft. Types

of Corrosions – Effect of Corrosion on Mechanical Properties – Protection against Corrosion – Corrosion ResistantMaterials used in Aircraft.

UNIT IV ALUMINIUM ALLOYS AND COMPOSITES 10 hrs.Introduction – Physical Metallurgy – Wrought Aluminum Alloys – Cast Aluminum Alloy - Production of Semi

Abrogated Forms – Aerospace Application – Plastics and Rubber – Introduction to FRP, Glass and Carbon Composites– Fibers and Resins – Characteristics and Application.

UNIT V SELECTION OF MATERIALS FOR AIRCRAFT AND ROCKETS 10 hrs.Classification of Aircraft Materials used for Aircraft Components – Application of Composite Materials – Super

Alloys, Indigenes Alloys. Emerging Trends in Aerospace Materials.

REFERENCE BOOKS:1. Martin, J.W., “Engineering Materials, Their Properties, and Application”, Wykendhan Publication. (London) Ltd., 1987.2. Titterton, G., “ Aircraft Materials and Processes”, Vedition, Pitman Publication Co., 1995.3. Krishnadas Nair, C.G., “ Handbook of Aircraft Materials”, Interline Publishing, 1993.4. Balaram Gupta, “ Aerospace Materials”, Vol.I, II and III, Chand & Company Ltd., New Delhi – 1996.





SAEX 1035 AEROELASTICITYL T P Credits Total Marks

3 0 0 3 100

UNIT I AEROELASTIC PHENOMENA 10 hrs.Stability versus response problems - The aero-elastic triangle of forces Aero elasticity in Aircraft Design

-Prevention of Aero elastic instabilities.

UNIT II DIVERGENCE OF A LIFTING SURFACE 10 hrs.Simple two dimensional idealizations - Strip theory - Fredholm integral equation of the second kind – Exact

solutions for simple rectangular wings –Semi rigid assumption and approximate solutions – Generalized coordinates-Successive approximations - Numerical approximations using matrix equations

UNIT III STEADY STATE AEROELASTIC PROBLEMS 10 hrs.Loss and reversal of aileron control - Critical aileron reversal speed - Aileron efficiency – Semi rigid theory and

successive approximations - Lift distribution -Rigid and elastic wings.

UNIT IV FLUTTER PHENOMENON 10 hrs.Non-dimensional parameters - Stiffness criteria Dynamic mass balancing -Model experiments – Dimensional

similarity - Flutter analysis - Two dimensional thin airfoils in steady incompressible flow – Quasi steady aerodynamicderivatives - Galerkin method for critical speed - Stability of distributed motion - Torsion flexure flutter - Solution ofthe flutter determinant - Methods of determining the critical flutter speeds – Flutter prevention and control.

UNIT V EXAMPLES OF AEROELASTIC PROBLEMS IN CIVIL AND MECHANICAL ENGINEERING10 hrs.

Galloping of transmission lines and flow induced vibrations of tall slender structures and suspension bridges.


TEXT BOOKS1. Bisplinghoff., R.L., Ashley, H., and Halfmann, R.L., “Aeroelasticity”, Addison Wesley Publishing Co., Inc., II ed, 1987.2. Fung, Y.C., “An Introduction to the Theory of Aeroelasticity”, John Wiley & Sons Inc., New York 1985.

REFERENCE BOOKS:1. Broadbent, E.G., “Elementary Theory of Aeroelasticity” BunHill Publications Ltd., 1986.2. Scanlan, R.H. and Rosenbaum, R., “Intrioduction to the Study of Aircraft Vibration and Flutter”, MacMillan Co., N.Y., 1991.





SAEX 1036ADVANCED CONTROL SYSTEM DESIGN FOR

AEROSPACE VEHICLESL T P Credits Total Marks

3 0 0 3 100

UNIT I INTRODUCTION 10 hrs.Introduction and Motivation for Modern Control Design- Review of Classical Control Systems-Introduction to Basic

Flight Mechanics and Flight Control Systems.-State Space Representation of Dynamical Systems.

UNIT II NON LINEAR SYSTEMS 10 hrs.Linearization of Nonlinear Systems, Linearized Flight Mechanics-Review of Matrix Theory-time Response of

Dynamical Systems in State Space form-Stability of Linear Systems-Controllability and Observability of Linear Systems.

UNIT III CONTROL SYSTEM DESIGN 10 hrs.Pole Placement Control Design.-Pole Placement Observer Design - Static Optimization -Optimal Control

Formulation; Linear Quadratic Regulator (LQR) Design- Application of Linear Control Theory to Autopilot Design ofAircrafts and Missiles-Gain Scheduling and Dynamic Inversion Design.

UNIT IV STABILITY ANALYSIS & LYAPUNOV THEORY 10 hrs.Stability Analysis of Nonlinear Systems Using Lyapunov Theory-Neuro-Adaptive Design for Nonlinear

Systems-Advanced Nonlinear Control of Aerospace Vehicles Using Dynamic Inversion and Neuro-Adaptive Design.

UNIT V NONLINEAR CONTROL DESIGN 10 hrs.Nonlinear Control Design Using Back-stepping-An Overview of LQ Observer and Kalman Filtering- Nonlinear

Observer Design.


REFERENCES1. N. S. Nise: Control Systems Engineering, 4th Ed., Wiley, 2004.2. K. Ogata: Modern Control Engineering, 3rd Ed., Prentice Hall, 1999.3. B. Friedland: Control System Design, McGraw Hill, 1986.4. E. Bryson and Y-C Ho: Applied Optimal Control, Taylor and Francis, 19755. Mathukumalli Vidyasagar, Nonlinear systems analysis, 2nd Edition,SIAM, 20026. Hassan K. Khalil, Nonlinear systems, Macmillan Pub. Co., 19927. Shankar Sastry, Nonlinear systems: analysis, stability, and control, Springer, 1999





SAEX 1029AIRCRAFT NAVIGATION, GUIDANCE AND

CONTROLL T P Credits Total Marks

3 0 0 3 100

UNIT I INERTIAL SENSORS 10 hrs.Gyroscopes-Mechanical-electromechanical-Ring Laser gyro- Fiber optic gyro, Accelerometers

UNIT II INERTIAL NAVIGATION SYSTEMS 10 hrs.INS components: transfer function and errors-The earth in inertial space, the coriolis effect-Mechanisation. Platform

and Strap down, INS system block diagram, Different co-ordinate systems, Schuler loop, compensation errors, Gimballock, Alignment.

UNIT III RADIO NAVIGATION 10 hrs.Different types of radio navigation- ADF, VOR/DME- Doppler –LORAN, DECCA and Omega - TACAN

UNIT IV APPROACH AND LANDING AIDS 10 hrs.ILS, MLS, GLS - Ground controlled approach system - surveillance systems-radio altimeter, RNAV, Modern

Navigation Aids

UNIT V SATELLITE NAVIGATION & HYBRID NAVIGATION 10 hrs.Introduction to GPS -system description -basic principles -position and velocity determination-signal

structure-DGPS, Introduction to Kalman filtering-Estimation and mixed mode navigation-Integration of GPS andINS-utilization of navigation systems in aircraft


REFERENCES:1. Myron Kyton, Walfred Fried, ‘Avionics Navigation Systems’, John Wiley & Sons,2nd edition, 19972. Nagaraja, N.S. “Elements of Electronic Navigation”, Tata McGraw-Hill Pub. Co., New Delhi, 2nd edition, 1975.3. George M Siouris, ‘Aerospace Avionics System; A Modern Synthesis’, Academic Press Inc., 1993.4. Albert Helfrick, ‘Practical Aircraft Electronic Systems’, Prentice Hall Education, Career & Technology, 1995.5. Albert D. Helfrick, ‘Modern Aviation Electronics’, Second Edition, Prentice Hall Career & Technology, 1994.6. Sen, A.K. & Bhattacharya, A.B. “Radar System and Radar Aids to Navigation”, Khanna Publishers, 1988.7. Slater, J.M. Donnel, C.F.O and others, “Inertial Navigation Analysis and Design”, McGraw-Hill Book Company, New York, 1964.





SAEX 1038 FLIGHT CONTROL SYSTEM DESIGNL T P Credits Total Marks

3 0 0 3 100

UNIT I INTRODUCTION TO CONTROL SYSTEM DESIGN & FCS 10 hrs.Open vs. Closed Loop Control - Analogue, Digital and Logical Control - Industrial Controllers - Control System

Design Objectives - Control System Design Cycle - Introduction to Flight Control Systems - History of FCS - Guidance,Navigation and Control - Flight Control Channels - Flight Control Methods - SAS vs. Autopilot

UNIT II AERODYNAMIC CONSIDERATIONS OF FLIGHT CONTROL SYSTEMS 10 hrs.Static and Dynamic Stability - Stability and Maneuverability - Static Margin - Variations of the Center of Pressure

- Hinge Moment - Aeroelastic Effects- Control System Performance - Canard Control - Wing Control - Tail Control -Fin Configuration Effects- Side Jet Control-Thrust -Vector Control - Variation of Mass and CG

UNIT III SENSORS & ACTUATORS 10 hrs.Flight Control Sensors – Accelerometers- Gyroscopes-Angle of attack vane - Other sensors - Sensor Selection-

Flight Control Actuators- Servomechanism- Reversible vs. Irreversible –Mechanisms-Hydraulic Actuators-PneumaticActuators- Electric Actuators

UNIT IV CONTROLLER DESIGN 10 hrs.An Overview of Controller Design-Design Using Frequency Response-Design Using Root Locus- Pole Placement

Methods-Linearization and Transfer Functions of Flying Vehicles- Coordinate Systems-Equations of Motion-Roll, Pitchand Yaw Transfer Functions-Design of Aerodynamic Control System for Missiles-STT vs. BTT -Lateral Control SystemDesign for STT-Roll Control-Control System Design for BTT-MIMO Based Design-Design of Single Channel FlightControl Systems

UNIT V AIRCRAFT CONTROL SYSTEM DESIGN 10 hrs.Longitudinal Control-Lateral Control- Attitude Control Systems -Flight Path Control Systems- Active Control

Systems -Thrust Vector Control - Classifications and Applications - Mathematical Modeling -Control Architectures -Controller Design- Miscellaneous Topics - Sensitivity Analysis-Man in the Loop considerations-Parameter Optimization


TEXT BOOKS:1. Garnell, P., “Guided Weapon Control Systems”, 2nd Edition, Pergamon Press, 1980.2. McLean, D., “Automatic Flight Control Systems”, Prentice Hall International (UK) Ltd, 1990.3. Blakelock, J. H.; Automatic Control of Aircraft and Missiles, 2nd Edition, John Wiley & Sons, 1990.

REFERENCE:1. Siouris, G.M. “Missile Guidance and control systems”, Springer, 2003.2. Fleeman, Eugene L.; Tactical Missile Design, First Edition, AIAA Education series, 2001.3. Roskam, Jan; Airplane flight dynamic and Automatic flight control, 3th Printing, Design, Analysis and Research Corporation, 2001.





SAEX 1039 UNMANNED AIRCRAFT SYSTEMSL T P Credits Total Marks

3 0 0 3 100

UNIT I INTRODUCTION TO UAS 10 hrs.History of unmanned aerial vehicles- types- Introduction to Unmanned aircraft systems-Unmanned aerial vehicles

–Micro aerial vehicles definitions, history, classification- applications-recent research and development in civil anddefense applications – autonomous vehicles -future research in autonomous vehicles – design standards and regulatoryaspects introduction to design and selection of systems

UNIT II ASPECTS OF UAS SYSTEMS 10 hrs.Involvement of different aspects in the development of UAV-aerodynamic configurations -Aspects of airframe

design- Stealth design, payload types, communication, navigations & guidance systems, control & stability, launch,recovery and support systems, reliability design

UNIT III MODELING AND CONTROL HELICOPTER MODEL 10 hrs.Modeling and control of small and miniature unmanned helicopters –single rotor helicopter design – coaxial rotor

helicopter design - autonomous control of a mini quadrotor vehicle using LQG controllers – linearization and identificationof helicopter model

UNIT IV UAV DESIGN MODELING & CONTROL 10 hrs.Development of autonomous quad tilt wing – advanced flight control systems for rotorcraft UAV and MAV –

mathematical modeling and non linear control of VTOL aerial vehicles

UNIT V DEPLOYMENT OF UAS/UAV SYSTEMS 10 hrs.Only application point of view of various UAS roles played in civil, defense applications -vision based navigation-

company trails- certification of UAS/UAV/MAV systems


REFERENCES: 1. Reg Austin, Unmanned Aircraft Systems: UAVS Design, Development and Deployment John Wiley, UK,2010 2. Kenzo Nonami, Farid Kendoul, Satoshi Suzuki, Wei Wang, Daisuke Nakazawa, Modeling and Control of Unmanned Small Scale

Rotorcraft Uavs & Mavs, Springer, New York, 2010 3. Laurence R. Newcome, Unmanned aviation: a brief history of unmanned aerial vehicles, American Institute of Aeronautics and

Astronautics, New York, 2004 4. Kimon Valavanis, Advances in unmanned aerial vehicles, Springer, Netherlands, 2007 5. Elizabeth Bone, Christopher Bolkcom, Unmanned aerial vehicles, Novinka Books, United Kingdom 2004 6. Rogelio Lozano, Unmanned Aerial Vehicles Embedded Control, John Wiley & Sons, 2010 7. Pedro Castillo, Rogelio Lozano, Alejandro E. Dzul, Modelling and control of mini-flying machines, Advances in industrial control

(AIC), Springer-Verlag, London,2005 8. Bernard Mettler, Identification modeling and characteristics of miniature rotorcraft, Kluwer Publishers, USA, 2003





SAEX 1040 ROBOTICS ENGINEERINGL T P Credits Total Marks

3 0 0 3 100

UNIT I INTRODUCTION TO ROBOTICS 10 hrs.Basic concepts - Robot anatomy - Manipulators - kinematics: Forward and reverse kinematics - Precision

movement, robot specifications and Work volume, Types of Robot drives - Basic robot motions - Point to point control,continuous path control.

UNIT II END EFFECTORS AND CONTROL SYSTEMS 10 hrs.End effectors - classification - mechanical, magnetic, vacuum and adhesive gripper - gripper force analysis and

design. Robot control - unit control system concept - servo and non-servo control of robot joints, adaptive and optimalcontrol.

UNIT III SENSORS 10 hrs.Sensor devices, Types of sensors - contact, position and displacement sensors, Force and torque sensors -

Proximity and range sensors - acoustic sensors - Robot vision systems - Sensing and digitizing - Image processingand analysis.

UNIT IV ROBOT PROGRAMMING 10 hrs.Robot language classification - programming methods - off and on line programming - Lead through method -

Teach pendent method - VAL systems and language, simple program.

UNIT V APPLICATIONS 10 hrs.Application of robots - Material handling - Machine loading and unloading, Assembly, Inspection, Welding, Spray

painting, Mobile robot - Recent developments in robotics- safety considerations- Application in Aeronautical Engineering.


TEXT BOOKS:1. Deb, S. R., Robotics Technology And Flexible Automation, Tata McGraw Hill Co, New Delhi, 19942. Mikell P. Groover, Industrial Robotics Technology Programming And Applications, McGraw Hill Co., Singapore, 1995

REFERENCE BOOKS: 1. Klafter, R. D, Chmielewski, T. A. and Noggins, Robot Engineering : An Integrated Approach, Prentice Hall of India Pvt. Ltd., New

Delhi, 1994 2. Fu, K. S., Gonzalez, R. C., & Lee, C.S.G., Robotics Control, Sensing, Vision And Intelligence, McGraw Hill Book Co., Singapore,

1987 3. Craig, J. J., Introduction To Robotics Mechanics And Control, Addison-Wesley, London, 1999





SAEX 1041 CRYOGENICSL T P Credits Total Marks

3 0 0 3 100

UNIT I INTRODUCTION 10 hrs.Historical Background - Introduction to cryogenic propellants - Liquid hydrogen, liquid helium, liquid nitrogen and

liquid oxygen and their properties

UNIT II PRODUCTION OF LOW TEMPERATURE 10 hrs.Theory behind the production of low temperature - Expansion engine heat exchangers - Cascade process Joule

Thompson Effect - Magnetic effect - Ortho and H2 - Helium4 and Helium 3

UNIT III EFFICIENCY OF CRYOGENIC SYSTEMS 10 hrs.Types of losses and efficiency of cycles - specific amount of cooling - The fraction liquified – Cooling coefficient

of performance - Thermodynamic efficiency – The energy balance Method

UNIT IV CYCLES OF CRYOGENIC PLANTS 10 hrs.Classification of cryogenic cycles - The structure of cycles - Throttle expansion cycles - Expander cycles -

Thermodynamic analysis - Numerical problems

UNIT V CRYOGENIC IN AEROSPACE APPLICATIONS 10 hrs.Cryogenic liquids in missile launching and space simulation Storage of cryogenic liquids - Effect of cryogenic

liquids on properties of aerospace materials – Cryogenic loading problems - Zero gravity problems associated withcryogenic propellants - Phenomenon of tank collapse - Elimination of Geysering effect in missiles


TEXT BOOKS1. Haseldom, G., Cryogenic Fundamentals, Academic Press, 19712. Barron, R. F., Cryogenic Systems, Oxford University, 1985

REFERENCE BOOK1. Parner, S. F., Propellant Chemistry, Reinhold Publishing Corpn., New York 1985





SAEX 1042 SPACECRAFT TECHNOLOGYL T P Credits Total Marks

3 0 0 3 100

UNIT I BASIC CONCEPTS 10 hrs.The solar system - Reference frames and coordinate systems - The celestial sphere -The ecliptic - Motion of

vernal equinox - Sidireal time - Solar time - Standard time - The earth’s atmosphere.

UNIT II THE GENERAL N-BODY PROBLEM 10 hrs.The Many body problem - Lagrange - Jacobi identity - The circular restricted three body problem – Libration

points - Relative Motion in the N-body problem - The two - body problem - Satellite orbits - Relations between positionand time - Orbital elements.

UNIT III SATELLITE INJECTION AND SATELLITE ORBIT PERTURBATIONS 10 hrs.General aspects of satellite injections - Satellite orbit transfer - Various cases - Orbit deviations due to injection

errors - Special and general perturbations - Cowell’s Method - Encke’s method - Method of variations of orbital elements- General perturbations approach.

UNIT IV INTERPLANETARY TRAJECTORIES BALLISTIC MISSILE - TRAJECTORIES 10 hrs.Two-dimensional interplanetary trajectories - Fast interplanetary trajectories - Three dimensional interplanetary

trajectories - Launch of interplanetary spacecraft - Trajectory about the target planet. The boost phase - Theballistic phase - Trajectory geometry - Optimal flights - Time of flight - Re-entry phase - The position of the impactpoint - Influence coefficients.

UNIT V MATERIALS FOR SPACECRAFT 10 hrs.Space environment - Peculiarities -Effect of space environment on the selection of materials of spacecraft.


TEXT BOOKS1. Brown, C. D., Spacecraft Mission Desing, AIAA Education Series, Washington DC, 1992.2. Sutton, G, P., Rocket Propulsion Elements, John Wiley, 1993.3. Van de Kamp, P., Elements of Astromechanics, Pitman, 1979.

REFERENCE BOOKS1. Cornelisse, J. W., Rocket Propulsion and Space Dynamics, W.H. Freeman & Co., 1984.2. Parker, E. R., Materials for Missiles and Spacecraft, McGraw Hill Book Co., Inc., 1982.





SAEX 1043LAUNCH VEHICLES AND SPACECRAFT

PROPULSIONL T P Credits Total Marks

3 0 0 3 100

UNIT I 10 hrs.Introduction - Historical Note / Basic Propulsion Devices - Architectural description of Launch Vehicles and

Satellites - Rocket Equation / Staging / Payload - Launch weight relation - Propulsion Requirements / Thrust and timerequirements - Types of rockets / propellants / choices.

UNIT II 10 hrs.Nozzle flows / Introduction - Performance parameters - Review of aero thermo chemistry - Propellant and burning

- Internal Ballistics - Grains / Ignition etc.

UNIT III 10 hrs.System Description / Propellants - Combustion / Heat Transfer / Cooling - Feed Systems - R-4 Auxilliary

Components - Monopropellants / Catalytic systems -Ignition / Restart / Environmental problems.

UNIT IV 10 hrs.Cold gas systems - Thruster satellite integration - Propellant management in spacecrafts - Propellant access in

microgravity.

UNIT V 10 hrs.Air breathing options in launch vehicles - Non chemical propulsion options - Nuclear Rockets. Electrostatic and

Electromagnetic propulsion. Special thermal and integration problems


REFERENCES:1. G.P. Sutton : Rocket Propulsion Elements, Wiley, New York, 20062. C.D. Brown: Spacecraft Propulsion, AIAA Education Series, AIAA Inc., Washington DC, 1996 .





SAEX 1044 ORBITAL MECHANICSL T P Credits Total Marks

3 0 0 3 100

UNIT 1 INTRODUCTION 10 hrs.Dynamics of point masses kinematics- time derivatives-relative motion – the two body problem-equations of

motion in inertial frame, relative motion- angular momentum, circular, elliptical, parabolic, hyperbolic trajectories Lagrangecoefficients-three body problem

UNIT II ORBITAL ELEMENTS 10 hrs.Orbits Vs trajectories, universal variables, orbits as function of time, orbits in three dimensions – Gibbs method,

Lambert Problem, sidereal time- top centric coordinate system- gauss method

UNIT III MANEUVERS 10 hrs.Hofmann transfer-bi-elliptic Hofmann-non Hoffman-plane range-relative motion –rendezvous motion- interplanetary

trajectories – gyroscopic instruments-mechanisms- types -operation

UNIT IV RIGID BODY DYNAMICS 10 hrs.Kinematics-equations of motion, rotational motion-moment of inertia-Euler’s equation-kinetic energy-Euler’s

angles-yaw, pitch and roll angles, dual spin the spinning top problem

UNIT V ATTITUDE DYNAMICS 10 hrs.Torque free motion - stability –dual spin-rotation damper-coning maneuver -attitude control thrusters-gyroscopic

attitude control-gravity-gradient stabilization- rocket vehicle dynamics- thrust equation-rocket performance- staging-optimalstaging


TEXT BOOK:1. Howard.D.Curtis, Orbital Mechanics for Engineering Students. 2nd ed, Elsevier, 20092. William.E.Wiesel,Space Flight Dynamics, 2nd ed, Tata McGraw-Hill,SiE,2007

REFERENCES: 1. Tewari, Atmospheric and Space Flight Dynamics - Modeling and Simulation with MATLAB and Simulink. Birkhäuser-Spinger, Special

Indian Edition, New Delhi, 2009 2. M.J. Sidi, Spacecraft Dynamics and Control. Cambridge, 1997, 3. Francis. J. Hale, Introduction to Space Flight. Prentice Hall, 1994 4. D.A. Vallado, Fundamentals of Astrodynamics and Applications. 2nd Edition, Microcosm, 2001, 5. G.A. Gurzadyan, Space Dynamics. CRC, 2002, 6. M.H. Kaplan, Modern Spacecraft Dynamics & Control. 1976, Wiley 7. B. Wie, Space Vehicle Dynamics and Control. AIAA, 1998





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AERO B.E. Final Syllabus