Approved v&Vi

8/9/2019 Approved v&Vi

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KUMARAGURU COLLEGE OF TECHNOLOGY

CURRICULUM 2007B.E., AERONAUTICAL ENGINEERING

SEMESTER V

Course Title L T P MU07AR501 Aircraft Structures II 3 1 0 100U07AR502 Mechanics of Machines 3 1 0 100U07AR503 Aerodynamics II 3 1 0 100U07AR504 Aircraft Performance 3 0 0 100U07AR505 Aircraft Electronics and Microprocessors 3 0 0 100U07EE503 Control Systems 3 1 0 100PRACTICALU07AR506 Aircraft Structures Lab II 0 0 3 100U07AR507 Aircraft Design Lab I 0 0 3 100U07GM402 Communication Skills Laboratory 2 0 2 100

U07GM404 Mini Project # 0 0 - 100U07GM501 Technical Seminar II 0 0 3 **

SEMESTER VICourse Title L T P M

U07GM601 Professional Ethics and Human Values 3 0 0 100

U07AR601Aircraft General Engineering and MaintenancePractices

3 0 0 100

U07AR602 Propulsion-II 3 1 0 100U07AR603 Experimental Stress Analysis 3 0 0 100U07AR604 Aircraft Stability And Control 3 0 0 100

Elective I 3 0 0 100PRACTICALU07AR605 Aircraft Design Lab II 0 0 3 100U07AR606 Aircraft Structures Repair Lab 0 0 3 100U07AR607 Propulsion Lab 0 0 3 100

Industrial training @ 0 0 - **

** Internal Evaluation Only.

# Students should do the mini-project work during the 2nd year summer vacation period.

@ Students should undergo training during the 3rd year summer vacation period.


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LIST OF ELECTIVES -VI SEMESTER

Course Title L T P MU07ARE01 Theory of Elasticity 3 0 0 100U07ARE02 Space Mechanics 3 0 0 100

U07ARE03 Wind Tunnel Techniques 3 0 0 100U07ARE04 Heat Transfer 3 0 0 100U07GEE01 Intellectual Property Rights (IPR) 3 0 0 100


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U07AR501 AIRCRAFT STRUCTURES II 3 1 0 100

1. UNSYMMETRICAL BENDING 8

Bending stresses in beams of unsymmetrical sections Bending of symmetric sections with skewloads.

2. SHEAR FLOW IN OPEN SECTIONS 10

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.

3. SHEAR FLOW IN CLOSED SECTIONS 10

Bredt Batho formula - Single and Multi cell structures - approximate methods. Shear flow insingle & multi-cell structures under torsion. Shear flow in single and multi-cell under bending withwalls effective and ineffective.

4. BUCKLING OF PLATES 10

Rectangular sheets under compression, Local buckling stress of thin walled sections, Cripplingstresses by Needhams and Gerards methods, Thin walled column strength. Sheet stiffenerpanels. Effective width, inter rivet and sheet wrinkling failures.

5. STRESS ANALYSIS IN WING AND FUSELAGE 7

Shear and bending moment distribution for semi cantilever and other types of wings andfuselage, thin web beam. With parallel and tapered flanges, Shear resistant web beams, Tensionfield web beams (Wagners).

TUTORIALS 15

TOTAL: 60

TEXT BOOK

1. Megson, T.H.G., Aircraft Structures for Engineering Students, 4th

edition ButterworthHeinemann, 2002.

REFEENCES

1. Peery, D.J., and Azar, J.J., Aircraft Structures, 2nd

edition, McGrawHill, N.Y., 1993.2. Bruhn. E.H. Analysis and Design of Flight vehicles Structures, Tri state off set

company, USA, 1985.3. Rivello, R.M., Theory and Analysis of Flight Structures, McGraw-Hill, 1993.


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U07AR502 MECHANICS OF MACHINES 3 1 0 100

1. MECHANISMS 9

Machine Structure Kinematic link, pair and chain Constrained motion Degrees of freedom -Slider crank mechanism Inversions Applications Kinematic analysis of simple mechanisms

Determination of velocity and acceleration, Gyroscope Principle and application.

2. FRICTION 9

Friction in screw and nut Pivot and collar Thrust bearing Plate and disc clutches Belt - flatand V belt drives. Ratio of tensions Effect of centrifugal and initial tension Condition formaximum power transmission Open and crossed belt drive.

3. GEARING AND CAMS 9

Gear profile and geometry Nomenclature of spur and helical gears Gear trains: Simple,compound gear trains and epicylic gear trains - Determination of speed and torque, Cams Types of cams Design of profiles Knife edged followers with and without offsets for varioustypes of follower motions.

4. VIBRATION 9

Free, forced and damped vibrations of single degree of freedom systems Force transmitted tosupports Vibration isolation Vibration absorption Torsional vibration of shaft Single rotorsystem Critical speed of shaft.

5. BALANCING 9

Static and dynamic balancing Single and several masses in different planes Balancing ofreciprocating masses- primary balancing and concepts of secondary balancing Single and multicylinder engines (Inline).

TUTORIALS 15

TOTAL: 60TEXT BOOKS

1. Rattan.S.S, Theory of Machines, Tata McGrawHill Publishing Co, New Delhi, 2004.2. Ballaney.P.L, Theory of Machines, Khanna Publishers, New Delhi, 2002.

REFERENCES

1. Rao, J.S and Dukkipati, R.V, Mechanism and Machine Theory, Second Edition, WileyEastern Ltd., 1992.

2. Malhotra, D.R and Gupta, H.C., The Theory of Machines, Satya Prakasam, Tech. IndiaPublications, 1989.

3. Gosh, A. and Mallick, A.K., Theory of Machines and Mechanisms, Affiliated East WestPress, 1989.

4. Shigley, J.E. and Uicker, J.J., Theory of Machines and Mechanisms, McGraw-Hill,1980.


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U07AR503 AERODYNAMICS II 3 1 0 100

1. ONE DIMENSIONAL COMPRESSIBLE FLOW 7

Energy, Momentum, continuity and state equations, velocity of sound, adiabatic steady state flowequations, Flow through converging, diverging passages, Performance under various back

pressures.

2. NORMAL, OBLIQUE SHOCKS AND EXPANSION WAVES 15

Prandtl equation and Rankine Hugonoit relation, Normal shock equations, Pitot static tube,corrections for subsonic and supersonic flows, Oblique shocks and corresponding equations,Hodograph and pressure turning angle, shock polars, flow past wedges and concave corners,strong, weak and detached shocks, Raleigh and Fanno Flow. Flow past convex corners,Expansion hodograph, Reflection and interaction of shocks and expansion, waves, Families ofshocks, Methods of Characteristics, Two dimensional supersonic nozzle contours.

3. DIFFERENTIAL EQUATIONS OF MOTION FOR STEADY COMPRESSIBLE FLOWS9

Small perturbation potential theory, solutions for supersonic flows, Mach waves and Mach angles,Prandtl-Glauert affine transformation relations for subsonic flows, Linearised two dimensionalsupersonic flow theory, Lift, drag pitching moment and center of pressure of supersonic profiles.

4. AIRFOIL IN HIGH SPEED FLOWS 6

Lower and upper critical Mach numbers, Lift and drag divergence, shock induced separation,Characteristics of swept wings, Effects of thickness, camber and aspect ratio of wings, Transonicarea rule, Tip effects.

5. HIGH SPEED WIND TUNNELS 8

Blow down, indraft and induction tunnel layouts and their design features, Transonic, supersonicand hypersonic tunnels and their peculiarities, Helium and gun tunnels, Shock tubes, Opticalmethods of flow visualization.

TUTORIALS 15

TOTAL: 60TEXT BOOK

1. John D. Anderson., Modern compressible flows, 3rd

edition, McGraw-Hill Book Co., NewYork 1999.

REFERENCES

1. S.M.Yahya, Fundamentals of Compressible Flow, 3rd

edition, New Age International,2003.

2. Shapiro, A.H., Dynamics and Thermodynamics of Compressible Fluid Flow, RonoldPress, 1982.

3. Zucrow, M.J. and Anderson, J.D., Elements of gas dynamics, McGraw-Hill Book Co.,New York, 1989.

4. Mc Comick. W., Aerodynamics, Aeronautics and Flight Mechanics, 2nd

edition JohnWiley, New York.

5. Rathakrishnan, E., Gas Dynamics, Prentice Hall of India, 2003.

6. Kuethe, A.M., and Chow, C.Y., Foundations of Aerodynamics, John Wiley & Sons, 1982.


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U07AR504 AIRCRAFT PERFORMANCE 3 0 0 100

1. POWER EFFECTS ON LIFT AND DRAG PERFORMANCE 12

Thrust , Power, SFC, Effects of temperature, altitude, speed and humidity on power, Powerrequired vs Power available curves for IC engines, Turbojet, Turboprop and Turbofan engines,Thrust augmentation and direct lift control.

2. STEADY FLIGHT: 8

Steady level flight, Thrust/power, available and required with altitude Estimation of maximum levelflight speed, conditions for minimum drag and minimum power required.

3. GLIDING, CLIMBING AND TURNING PERFORMANCE 12

Maximum range, Minimum rate of sink and glide, Shallow angle of climb, Rate of climb, time toclimb and ceiling, Glide hodograph. Bank angle and load factor, Limitations on turn, Pull up andpush over, the V-n diagram.

4. SPECIAL PERFORMANCE: 6

Range and endurance of jet and propeller type of airplanes, estimation of take-off and landingdistance. Use of thrust augmentation and reverse thrust.

5. PROPELLERS: 7

Froude momentum and blade element theories, Propeller coefficients, Use of propeller charts,performance of fixed and variable pitch propeller.

TOTAL: 45

TEXT BOOK:1. John David Anderson, Jr., Aircraft performance and design, McGraw Hill, 1998.

2. B.W.McCormick, Aerodynamics, Aeronautics, and Flight Mechanics, 2nd

edition, 1994.

REFERENCE:1. L.J.Clancy, Aerodynamics, Pitman, 1986.2. Houghton,E.L., and Carpenter, N.B., Aerodynamics for engineering students, 3

rdEdition

Edward Arnold Publishers,1988.3. J.J. Bertin, Aerodynamics for engineers, Pearson Education, 2002.4. John D. Anderson, Fundamentals of Aerodynamics, 4

THedition, McGraw Hill, 2006.


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U07AR505 AIRCRAFT ELECTRONICS & MICROPROCESSORS 3 0 0 100

1. AIRCRAFT BATTERIES 7

Aircraft Storage Batteries: Dry Cells and Batteries; Lead Acid Storage Batteries & theirmaintenance procedures, Installation of Aircraft Batteries

2. MICROPROCESSORS AND DIGITAL ELECTRONICS 12

Block Diagram of Microprocessors Architecture of Intel 8085, Instruction set, Classification,Data format and storage, Bus Structure of 8085,Addressing modes, Overview of the 8085Instruction Set, Development of Simple Assembly Language Program. Internal architecture andfunctioning of Intel 8086 -Digital electronics, Trouble Shooting, Digital Circuits.

3. AIRCRAFT LIGHTS, COMMUNICATION, NAVIGATION & WARNING SYSTEMS10

Aircraft Lights, Radio Theory: Radio waves, Amplifiers, Functions of a Transmitter & Receivers.Communication & Navigation Systems: VHF Communication Systems, Automatic DirectionFinder Systems.Weather Warning Systems: Radar, Digital Airborne Weather Radar Systems.

4. MICROPROCESSOR MEMORY, INTERFACING PHERIPERALS 9

RAM, ROM, EPROM, Memory Interfacing, Interfacing Input Devices, Memory Mapped I/O, BasicConcepts in Serial I/O, Interfacing a matrix keyboard, 8255,8259,DMA Data transfer 8237 busarchitecture.

5. APPLICATIONS 7

Electronic Flight Instrument Systems, Automatic Flight Control System, Automatic Flight &Landing Systems, Flight Management System, Navigation/Guidance System.

TOTAL: 45

TEXT BOOKS

1. Aircraft Electricity & Electronics Thomas K.Eismin Sixth Edition, McGraw-HillInternational Editions, 2007.

2. Goankar R.S., Microprocessors Architecture. Programming and Applications

REFERENCES

1. Introduction to Microprocessors-Aditya P Mathur, Third Edition, Tata McGraw Hill.

2. Aircraft Instruments & Integrated Systems EHJ Pallet, Indian Reprint 1996-LongmanScientific & Technical.

3. Aircraft Electrical Systems 3rd

edition by EHJ Pallet, Longman Scientific & Technical.


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U07EE503 CONTROL SYSTEMS 3 1 0 100

1. SYSTEMS AND THEIR REPRESENTATION 9

Basic elements in control systems Open and closed loop systems Electrical analogy of

mechanical and thermal systems Transfer function Synchros AC and DC servomotors Block diagram reduction techniques Signal flow graphs.

2. TIME RESPONSE 9

Time response Time domain specifications Types of test input I and II order systemresponse Error coefficients Generalized error series Steady state error P, PI, PID modesof feed back control.

3. FREQUENCY RESPONSE 9

Frequency response Bode plot Polar plot Constant M an N circles Nichols chart Determination of closed loop response from open loop response Correlation between frequencydomain and time domain specifications.

4. STABILITY OF CONTROL SYSTEM 9

Characteristics equation Location of roots in S-plane for stability Routh Hurwitz criterion Root locus construction effect of poles, zero addition Gain margin and phase margin Nyquist stability criterion.

5. COMPENSATOR DESIGN 9

Performance criteria Lag, lead and lag-lead networks Cascade Compensator design usingBode plots.

TUTORIALS 15

Total: 60

TEXT BOOKS

1. K. Ogata, Modern Control Engineering, 4th edition, Pearson Education, New Delhi,2003.

2. I.J. Nagrath & M. Gopal, Control Systems Engineering, New Age InternationalPublishers, 2003.

REFERENCE BOOKS

1. B.C. Kuo, Automatic Control Systems, Prentice Hall of India Ltd., New Delhi, 1995.

2. M. Gopal, Control Systems, Principles & Design, Tata McGraw Hill, New Delhi, 2002.3. M.N. Bandyopadhyay, Control Engineering Theory and Practice, Prentice Hall of India,

2003.


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U07AR506 AIRCRAFT STRUCTURES LAB II 0 0 3 100

LIST OF EXPERIMENTS

1. Unsymmetrical bending of beams

2. Shear centre location for open sections

3. Shear centre location for closed sections

4. Constant strength beam

5. Flexibility matrix for cantilever beam

6. Beam with combined loading

7. Calibration of Photo- elastic materials

8. Stresses in circular discs and beams using photo elastic techniques

9. Vibrations of beams

10. Wagner beam Tension field beam

TOTAL : 45


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U07AR507 AIRCRAFT DESIGN LAB I 0 0 3 100

LIST OF EXPERIMENTS

1. Comparative configuration study of different types of airplanes.

2. Comparative study on specification and performance details of aircraft.

3. Preparation of comparative data sheets.

4. Work sheet layout procedures.

5. Comparative graphs preparation and selection of main parameters for the design.

6. Preliminary weight estimations, selection of main parameters.

7. Power plant selection, Aerofoil selection, Wing tail and control surfaces.

8. Preparation of layouts of balance diagram and three view drawings.

9. Drag estimation.

10. Detailed performance calculations and stability estimates.

TOTAL: 45


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U07GM402 COMMUNICATION SKILLS LABORATORY 2 0 2 100

(COMMON TO ALL BRANCHES)

Globalization has brought in numerous opportunities for the teeming millions, with morefocus on the students overall capability apart from academic competence. Many students,particularly those non- English medium schools, find that they are not preferred due to theirinadequacy of communication skills and soft skills, despite possessing sound knowledge in theirsubject area along with technical capability. Keeping in view their pre- employment needs andcareer requirements, this course on Communication Skills Laboratory will prepare students toadapt themselves with ease to the Industry environment, thus rendering them as prospectiveassets to Industries. The course will equip the student with the necessary communication skillsthat would go a long way in helping them in their profession.

OBJECTIVES:

* To equip students of engineering and technology with effective speakingand listening skills in English.

* To help them develop their soft skills and people skills, which will make thetransition from college to workplace smoother and help them to excel in

their jobs.* To enhance students performance at Placement Interviews, Group

discussions and other recruitment exercises.

1. PC based session (Weightage - 40%) 24 periods

A. English Language Lab (18 Periods)

1. Listening Comprehension (6)

Listening Listening and sequencing of sentences Filling in theBlanks Listening and answering the question

2. Reading Comprehension and Vocabulary (6)

Filling in the blanks Cloze Exercises Vocabulary building Reading andAnswering questions

3. Speaking: (6)

Phonetics: Intonation Ear Training Correct Pronunciation SoundRecognition exercises Common Errors in English

Conversations: Face to face Conversation Telephone conversation - Role playActivities (Students take on roles and engage in conversation)

B. Career Lab (6 Periods)

(Samples are available to learn and practice in the class room session)

1. Resume / Report Preparation / Letter Writing (1)

Structuring the resume / report Letter writing / E-mail communication Samples


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2. Presentation Skills (1)

Elements of an effective presentation Structure of a presentation PresentationTools Voice Modulation Audience analysis Body Language

3. Soft Skills (2)

Time Management Articulateness Assertiveness Innovation and Creativity Stress Management & Poise

4. Group Discussion (1)

Why is GD part of selection process? Structure of a GD- Moderator-led andOther GDs Strategies in GD team work Body Language Mock GD

5. Interview Skills

Kinds of Interviews Required Key Skills Corporate culture- Mock Interviews

II. Class Room Session (welghtage-60%) 24 periods

1. Resume / Report Preparation /Letter writing: Students prepare theirown resume and report. (2)

2. Presentation Skills: Students make presentations on given topics. (8)

3. Group Discussion: Students participate in group discussions (8)

4. Interview Skills: Students participate in Mock Interviews. (8)

Note: Classroom sessions are practice sessions

References:

Books:1.Meenakshi Raman and Sangeetha Sharma, Technical Communication-

Principles and Practice, Oxford University Press. New Delhi (2004).2. Barker. A Improve your communication skills Kogan page India Pvt Ltd.

New Delhi (2006).3. Adrian Doff and Christopher Jones- Language in Use (Upper- Intermediate).

Cambridge University Press. First South Asian Edition (2004).4. John Seely, the Oxford Guide to writing and speaking, Oxford University

Press, New Delhi (2004).5. Customize yourself to corporate life Dr. K. Devadoss & P. Malathy Inder

Publications, Coimbatore (2007).

CDs

1. Train2sucess series 1.Telephone Skills.2. Interviewing Skills 3. NegotiationSkills by Zenith Global Consultants Ltd. Mumbai.

2. BEC Series.

3. Look Ahead by Cambridge University Press.


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U07GM404 Mini Project 0 0 - 100

The objective of this project is to provide opportunity for the students to implement their

skills acquired in the previous semesters to practical problems. Students have to do a mini-projectwork during the summer holidays at the end of 2

ndyear for a period of 2 weeks; a report should

be submitted at the beginning of 5th

semester.

Guidelines

1. Selection of a topic or project title in consultation with a staff member.

2. Develop a project planning strategy.

3. If it is an industry sponsored project, a concurrent letter from industry is required.

4. A maximum of 3 students per group will do the project.

5. The project may be done in one of the labs under the supervision of a guide or in the selected

industry.

6. At the end of the project, a report will be written and a technical presentation along with

demonstration will be made by the students.

7. The report, project demonstration and technical presentation will be evaluated by the internal

and external examiners.


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U07GM501 Technical Seminar II

Content Methodology

Topic Sub-topics Teachers Part Students PartEva

Speaking skills One minute speechTheory to behandled withexamples.

Exercise 1: Eachstudent has to introducethemselves creativity in aminute.

The writtenthe way in presented

Exercise 2: Each studentwill be given a topic onwhich they have to speakinstantly for a minute.

The speec(After speato be writterecord pur

TechnicalPresentation

skills

(for presenting atechnical paper)

Selecting a topic forpresentation

Structuring a technicalpresentation

Resources for gatheringinformation for the presentation

Aids for effective presentation

Theory to behandled withexamples for

preparing atechnicalpaper.

Exercise 3 & 4:Students have to selecttwo technical topics onwhich they will prepare

two papers and twopower point presentationsand present the same.

For both topower pointhe way in

to be evalueach prese

Exercise 5: Student hasto prepare resume andpresent it.

The resumcreative pr

Writing skills Resume writing

Cover letter (for job)

Theory to behandled withexamples. Exercise 6: Student has

to prepare a cover letterfor applying for a job.

The cover for creativi

Report to be maintained by each studenta. Cover page.b. Bona-fide certificate.c. Content with marks awarded for each exercise.d. Evaluated exercises


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U07GM601 PROFESSIONAL ETHICS AND HUMAN VALUES 3 0 0 100

1. HUMAN VALUES 10

Morals, Values and Ethics Integrity Work Ethic Service Learning Civic Virtue Respect for

Others Living Peacefully caring Sharing Honesty Courage Valuing Time Co-operation Commitment Empathy Self-Confidence-Character-Spirituality, Religious tolerance.

2. ENGINEERING ETHICS AND THEORIES 9

Definition, Moral issues, Types of inquiry, Morality and issues of morality, Kohlberg and Gilliganstheories, consensus and controversy, Profession and professionalism, moral reasoning andethical theories, virtues, professional responsibility, integrity, self respect, duty ethics, ethicalrights, self interest, egos, moral obligations etc.

3. SOCIAL ETHICS AND ENGINEERING AS SOCIAL EXPERIMENTATION9

Engineering as social experimentation, codes of ethics, Legal aspects of social ethics, thechallenger case study, Engineers duty to society and environment, Gandhian Principles ofcorporate trusteeship.

4. SAFETY, RESPONSIBILITIES AND RIGHTS OF ENGINEERS 9

Safety and risk assessment of safety and risk risk benefit analysis and reducing risk theThree Mile Island and Chernobyl case studies. Bhopal gas tragedy - Collegiality and loyalty respect for authority collective bargaining confidentiality conflicts of interest occupationalcrime professional rights employee rights Intellectual Property Rights (IPR) discrimination.

5. GLOBAL ISSUES AND ENGINEERS AS MANAGERS, CONSULATANTSAND LEADERS 8

Multinational corporations Environmental ethics computer ethics - weapons development

engineers as managers-consulting engineers-engineers as expert witnesses and advisors-moralleadership Engineers as trend setters for global values, IT Industry (cultural aggression).

Total : 45

Text Books:1. Mike Martin and Roland Schinzinger, Ethics in Engineering, McGraw-Hill, New York, 1996.2. John R.Boatright, Ethics and the Conduct of Business, Pearson Education, New Delhi,

2003.

References:

1. Charles D.Fleddermann, Engineering Ethics, Pearson Education / Prentice Hall, New

Jersey, 2004 (Indian Reprint).2. Charles E.Harris, Michael S.Protchard and Michael J.Rabins, Engineering Ethics-Concepts

and Cases, Wadsworth Thompson Learning, United States, 2000. (Indian Reprint nowavailable)

3. Sadasivam S., Icons of Tamilnadu Inder Publications, Coimbatore, 2008.


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U07AR601 AIRCRAFT GENERAL ENGINEERING AND MAINTENANCE PRACTICES

3 0 0 100

1. AIRCRAFT GROUND HANDLING AND SUPPORT EQUIPMENT 10

Mooring, jacking, levelling and towing operations Preparation Equipment - precautions

Engine starting procedures Piston engine, turboprops and turbojets Engine fire extinguishing Ground power units.

2. GROUND SERVICING OF VARIOUS SUB SYSTEMS 8

Air conditioning and pressurization Oxygen and oil systems Ground units and theirmaintenance.

3. MAINTENANCE OF SAFETY 5

Shop safety Environmental cleanliness Precautions.

4. INSPECTION 10

Process Purpose Types Inspection intervals Techniques Checklist Special inspection Publications, bulletins, various manuals FAR Air worthiness directives Type certificate DataSheets ATA specifications.

5. AIRCRAFT HARDWARE, MATERIALS, SYSTEMS PROCESSES 12

Hand tools Precision instruments Special tools and equipments in an airplane maintenanceshop Identification terminology Specification and correct use of various aircraft hardware (i.e.nuts, bolts, rivets, screws etc.) American and British systems of specifications Threads, gears,bearings, etc. Drills, tapes & reamers. identification of all types of fluid line fittings. Materials,metallic and non-metallic - Plumbing Connectors - Cables Swaging procedures, tests,Advantages of swaging over splicing.

TOTAL : 45

TEXT BOOK

1. KROES WATKINS DELP, Aircraft Maintenance and Repair McGraw-Hill, New York 1993.

REFERENCES

1. A & P MECHANICS, Aircraft hand Book F. A. A. Himalayan Book House, New Delhi,1996.

2. A & P MECHANICS, General hand Book F. A. A. Himalayan Book House, New Delhi,1996.

3. Civil Aviation Publication, CAP 459 and CAP 562, UK Civil Aviation Authority.


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U07AR602 PROPULSION II 3 1 0 100

1. AIRCRAFT GAS TURBINES 12

Impulse and reaction blading of gas turbines Velocity triangles and power output Elementarytheory Vortex theory Choice of blade profile, pitch and chord Estimation of stage

performance Limiting factors in gas turbine design- Overall turbine performance Methods ofblade cooling Matching of turbine and compressor Numerical problems.

2. RAMJET PROPULSION: 10

Operating principle Sub critical, critical and supercritical operation Combustion in ramjetengine Ramjet performance Sample ramjet design calculations Introduction to scramjet Preliminary concepts in supersonic combustion Integral ram- rocket- Numerical problems.

3. FUNDAMENTALS OF ROCKET PROPULSION 8

Operating principle Specific impulse of a rocket internal ballistics- Rocket nozzle classification Rocket performance considerations Numerical Problems.

4. CHEMICAL ROCKETS 10Solid propellant rockets Selection criteria of solid propellants Important hardware componentsof solid rockets Propellant grain design considerations Liquid propellant rockets Selection ofliquid propellants Thrust control in liquid rockets Cooling in liquid rockets Limitations ofhybrid rockets Relative advantages of liquid rockets over solid rockets- Numerical Problems.

5. ADVANTAGES OF PROPULSION TECHNIQUES 5

Electric rocket propulsion Ion propulsion techniques Nuclear rocket Types Solar sail-Preliminary Concepts in nozzle less propulsion.

TUTORIALS 15

TOTAL: 60TEXT BOOKS

1. Sutton, G.P., Rocket Propulsion Elements, John Wiley & Sons Inc., New York, 7th

edition.2. Cohen, H., Rogers, G.F.C. and Saravanamuttoo, H.I.H., Gas Turbine Theory, 4

th

edition, Pearson Education, 1989.

REFERENCES

1. Hill, P.G. & Peterson, C.R. Mechanics & Thermodynamics of Propulsion 2nd

editionPearson Education, 1999.

2. Gordon Oates, Aero thermodynamics of Gas Turbine and Rocket Propulsion, AIAA

Education Series, New York, 1989.3. Mathur, M., and Sharma, R.P., Gas Turbines and Jet and Rocket Propulsion, Standard

Publishers, New Delhi, 1988.


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U07AR603 EXPERIMENTAL STRESS ANALYSIS 3 0 0 100

1. MEASUREMENTS 7

Principles of measurements, Accuracy, Sensitivity and range of measurements.

2. EXTENSOMETERS 7

Mechanical, Optical Acoustical and Electrical extensometers and their uses, Advantages anddisadvantages.

3. ELECTRICAL RESISTANCE STRAIN GAUGES 10

Principle of operation and requirements, Types and their uses, Materials for strain gauge.Calibration and temperature compensation, cross sensitivity, Rosette analysis, Wheatstonebridge and potentiometer circuits for static and dynamic strain measurements, strain indicators.

4. PHOTOELASTICITY 10

Two dimensional photo elasticity, Concept of light photo elastic effects, stress optic law,

Interpretation of fringe pattern, Compensation and separation techniques, Photo elastic materials.Introduction to three dimensional photo elasticity.

5. NON DESTRUCTIVE TESTING 11

Fundamentals of NDT, Radiography, ultrasonic, magnetic particle inspection, Fluorescentpenetrant technique, Eddy current testing, Acoustic Emission Technique, Fundamentals of brittlecoating methods, Introduction to Moir techniques, Holography, ultrasonic C-Scan, Thermograph,Fiber optic Sensors.

TOTAL: 45TEXT BOOKS

1. Srinath, L.S., Raghava, M.R., Lingaiah, K., Garagesha, G., Pant B., and Ramachandra,

K., Experimental Stress Analysis, Tata McGraw-Hill, New Delhi, 1984.

REFERENCES

1. Dally, J.W., and Riley, W.F., Experimental Stress Analysis, McGraw-Hill Inc., New York,1998.

2. Hetyenyi, M., Hand book of Experimental Stress Analysis, John Wiley and Sons Inc.,New York, 1972.

3. Pollock A.A., Acoustic Emission in Acoustics and Vibration Progress, Ed. StephensR.W.B., Chapman and Hall, 1993.


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U07AR604 AIRCRAFT STABILITY AND CONTROL 3 0 0 100

1. GENERAL: 7

Degrees of freedom of a system, Static and dynamic stability Need for stability in an airplane,purpose of controls, inherently and marginally stable airplanes.

2. STATIC LONGITUDINAL STABILITY: 14

Stick fixed: Basic equations of equilibrium, Stability criterion, Wing and tail moments, Effect offuselage and nacelles, Effect of c.g. location, Power effects, Stabiliser setting and c.g. location,Elevator effects, stick fixed neutral point.Stick free: Hinge moment coefficients, Stick free neutral point symmetric maneuvers, stick forcegradients and stick force per cg. Aerodynamic balancing of control surfaces.

3. STATIC LATERAL STABILITY: 7Dihedral effect, coupling between rolling moment and yawing moment, Adverse yaw, Aileronpower, Aileron reversal.

4. STATIC DIRECTIONAL STABILITY: 7

Weather cock effect, rudder requirements. One engine inoperative conditions, rudder lock.

5. DYNAMIC STABILITY: 10

Dynamic Longitudinal Stability - Equation of motion, Stability derivatives, Rouths discriminant,solving the stability quadratic, Phugoid motion, factors affecting the period anddamping.DYNAMIC Lateral And Direction Stability-Dutch roll and spiral instability Auto rotationand spin, Two control airplane.

TOTAL: 45

TEXT BOOK:

1. Nelson, R.C. Flight stability & Automatics Control, McGraw Hill, 1989.2. Eitkin, B., Reid, L.D.: Dynamics of Flight Stability and Control, 3

rdedition, Wiley, New York

1996.

REFERENCES:

1. Babister, A.W. Aircraft stability and response, Pergamon Press, 1980.2. McCormick, B.W., Aerodynamics, Aeronautics & Flight Mechanics John Wiley, 1995.3. C. D. Perkins and R. E. Hage, Airplane Performance, Stability and Control, John Wiley &

Sons, 1949.


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U07AR605 AIRCRAFT DESIGN LAB II 0 0 3 100

LIST OF EXPERIMENTS

1. V-n diagram for the design study.

2. Gust and maneuverability envelopes.3. Critical loading performance and final V-n graph calculation.

4. Structural design study Theoretical approach.

5. Load estimation of wings.

6. Load estimation of fuselage.

7. Balancing and maneuvering loads on tail plane, Aileron and Rudder loads.

8. Detailed structural layouts.

9. Design of some components of wings, fuselage.

10. Preparation of a detailed design report with CAD drawings.

TOTAL : 45


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U07AR606 AIRCRAFT STRUCTURES REPAIR LAB 0 0 3 100

LIST OF EXPERIMENTS

1. Aircraft wood gluing.

2. Welded patch repair by TIG.

3. Welded patch repair by MIG.

4. Welded patch repair by Plasma Arc.

5. Fabric Patch repair.

6. Riveted patch repairs.

7. Repair of composites.

8. Repair of Sandwich panels.

9. Sheet metal forming.

10. Control cable inspection and repair.

TOTAL : 45


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U07AR607 PROPULSION LAB 0 0 3 100

LIST OF EXPERIMENTS

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. Study of forced convective heat transfer over a flat plate.

4. Study of free convective heat transfer over a flat plate

5. Cascade testing of a model of axial compressor blade row.

6. Study of performance of a propeller.

7. Determination of heat of combustion of aviation fuel.

8. Combustion performance studies in a jet engine combustion chamber.

9. Study of free jet.

10. Study of wall jet.

TOTAL : 45


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Assessment Guidelines for Industrial training

At the end of 6th

semester, all UG students undergo industrial training for at least two

weeks. They will work in industry under the guidance of a professional. Their work will be

monitored by the KCT staff at least 2 times during the training period. The students shall keep a

log book and write a weekly report on their work describing the assignment, acquired knowledge,

activities performed, contribution to industry and other relevant matters. An introduction to the

company with an organization chart shall be included in the log book. At the end of the training

period, a detailed report on the project with accomplishments shall be written and submitted by

the students for the joint review and assessment of KCT staff and industry guide. A training

certificate signed by KCT staff, industry guide and KCT Principal will be given to the students on

the basis of their contribution as satisfactory, good, very good and excellent.

First visit of KCT staff to industry will be in the middle of the training period and a review

of the log book maintained by the student will be done.

First assessment

RatingS.No Activity

Satisfactory Good V. Good Excellent Comments

1. Assignment

2. Attitude and Motivation

3. Contribution to industry4. Progress of the assignment

The above assessment will be signed by both industry guide and KCT staff.

At the end of the training period, both the log book and the report will be reviewed by

KCT staff and industry guide.


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Second assessment (End of training)

RatingS.No Activity

Satisfactory Good V. Good Excellent

I.1.

2.

3.

4.

Log book and interviewAssignment

Work accomplishment

Behaviour

Contribution to industry

II.

1.

2.

3.

4.

Report

Presentation

Technical content

Results analysis, discussion and

recommendationBenefit to industry

The ranking for the issuance of the industrial training certificate will be determined by the

KCT staff on the basis of the above assessments. A certificate will then be issued to the student

in the presence of the class advisor and respective HOD. The student report in the form of a CD

and hard copy shall be kept in the respective department library for inspection by the University

Committee.


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U07ARE01 THEORY OF ELASTICITY 3 0 0 100

1. ASSUMPTIONS IN ELASTICITY 4

Definitions- notations and sign conventions for stress and strain, Equations of equilibrium.

2. BASIC EQUATIONS OF ELASTICITY 15

Strain displacement relations, Stress strain relations, Lames constant cubical dilation,Compressibility of material, bulk modulus, Shear modulus, Compatibility equations for stressesand strains, Principal stresses and principal strains, Mohrs circle, Saint Venants principle.

3. PLANE STRESS AND PLANE STRAIN PROBLEMS 8

Airys stress function, Bi-harmonic equations, Polynomial solutions, Simple two-dimensionalproblems in Cartesian coordinates like bending of cantilever and simply supported beams, etc.

4. POLAR COORDINATES 10

Equations of equilibrium, Strain displacement relations, Stress strain relations, Axi symmetric

problems, Kirsch, Michells and Boussinesque problems.

5. TORSION 8

Naviers theory, St. Venants theory, Prandtls theory on torsion, The semi- inverse method andapplications to shafts of circular, elliptical, equilateral triangular and rectangular sections.

TOTAL : 45

TEXT BOOK

1. Timoshenko, S., and Goodier, T.N., Theory of Elasticity, McGrawHill Ltd., Tokyo, 1990.

REFERENCES

1. Enrico Volterra & J.H. Caines, Advanced Strength of Materials, Prentice Hall New Jersey,1991.

2. Wng, C.T., Applied Elasticity, McGrawHill Co., New York, 1993.3. Sokolnikoff, I.S., Mathematical Theory of Elasticity, McGrawHill New York, 1978.


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U07ARE02 SPACE MECHANICS 3 0 0 100

1. BASIC CONCEPTS 7

The Solar System References Frames and Coordinate Systems The Celestial Sphere TheEcliptic Motion of Vernal Equinox Sidereal Time Solar Time Standard Time The Earths

Atmosphere.

2. THE GENERAL N-BODY PROBLEM 10

The many body Problem Lagrange Jacobian Identity The Circular Restricted Three BodyProblem Libration Points- Relative Motion in the N-body Problem Two Body Problem Satellite Orbits Relations Between Position and Time Orbital Elements.

3. SATELLITE INJECTION AND SATELLITE ORBIT PERTURBATIONS 10

General Aspects of satellite Injections Satellite Orbit Transfer Various Cases OrbitDeviations Due to Injection Errors Special and General Perturbations Cowells Method Enckes Method Method of vibrations of Orbital Elements General Perturbations Approach.

4. INTERPLANETARY TRAJECTORIES 8Two Dimensional Interplanetary Trajectories Fast Interplanetary Trajectories ThreeDimensional Interplanetary Trajectories Launch if Interplanetary Spacecraft Trajectory aboutthe Target Planet.

5. BALLISTIC MISSILE TRAJECTORIES AND MATERIALS 10

The Boost Phase The Ballistic Phase Trajectory Geometry- Optimal Flights Time of Flight Re entry Phase The Position of the Impact Point Influence Coefficients. Space Environment Peculiarities Effect of Space Environment on the Selection of Spacecraft Material.

TOTAL : 45

TEXT BOOK1. Cornelisse, J.W., Rocket Propulsion and Space Dynamic, W.H. Freeman & Co., 1984.

REFERENCES

1. Sutton, G.P., Rocket Propulsion Elements, 7th

edition, John Wiley, 1993.2. Van de Kamp, P., Elements of Astromechanics, Pitman, 1979.3. Parker E.R., Materials for Missiles and Spacecraft, McGraw-Hill Book Co. Inc., 1982.


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U07ARE03 WIND TUNNEL TECHNIQUES 3 0 0 100

1. PRINCIPLES OF MODEL TESTING 6

Buckingham Theorem Non-Dimensional Numbers Scale Effect Types of Similarities.

2. WIND TUNNELS 8

Classification Special problems of Testing in Subsonic, Transonic, supersonic and hypersonicspeed regions Layouts sizing and design parameters.

3. CALIBRATION OF WIND TUNNELS 11

Test section speed Horizontal buoyancy Flow angularities Turbulence measurements Associated instrumentation Calibration of supersonic tunnels.

4. WIND TUNNEL MEASUREMENTS 12

Pressure and velocity measurements Force measurements Three component and sixcomponent balances Internal balances.

5. FLOW VISUALIZATION 8

Smoke and Tuft grid techniques Dye injection special techniques Optical methods of flowvisualization.

TOTAL : 45TEXT BOOK

1. Rae, W.H. and Pope, A. Low Speed Wind Tunnel Testing, John Wiley Publication, 1984.

REFERENCE

1. Pope, A., and Goin, L., High Speed wind Tunnel Testing, John Wiley, 1985.


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U07ARE04 HEAT TRANSFER 3 0 0 100

1. HEAT CONDUCTION 11

Basic Modes of Heat Transfer One dimensional steady state heat conduction: CompositeMedium Critical thickness Effect of variation of thermal Conductivity Extended Surfaces

Unsteady state Heat Conduction: Lumped System Analysis Heat Transfer in Semi infinite andinfinite solids Use of Transient Temperature charts Application of numerical techniques.

2. CONVECTIVE HEAT TRANSFER 10

Introduction Free convection in atmosphere free convection on a vertical flat plate Empiricalrelation in free convection Forced convection Laminar and turbulent convective heat transferanalysis in flows between parallel plates, over a flat plate and in a circular pipe. Empiricalrelations, application of numerical techniques in problem solving.

3. RADIATIVE HEAT TRANSFER 8

Introduction to Physical mechanism Radiation properties Radiation shape factors Heatexchange between non black bodies Radiation shields.

4. HEAT EXCHANGERS 8

Classification Temperature Distribution Overall heat transfer coefficient, Heat ExchangeAnalysis LMTD Method and E-NTU Method.

5. HEAT TRANSFER PROBLEMS IN AEROSPACE ENGINEERING 8

High-Speed flow Heat Transfer, Heat Transfer problems in gas turbine combustion chambers Rocket thrust chambers Aerodynamic heating Ablative heat transfer.

TOTAL : 45TEXT BOOKS

1. Yunus A. Cengel., Heat Transfer A practical approach, Second Edition, Tata McGraw-Hill, 2002.

2. Incropera. F.P.and Dewitt.D.P. Introduction to Heat Transfer, John Wiley and Sons 2002.

REFERENCES

1. Lienhard, J.H., A Heat Transfer Text Book, Prentice Hall Inc., 1981.2. Holman, J.P. Heat Transfer, McGraw-Hill Book Co., Inc., New York, 6

thEdn., 1991.

3. Sachdeva, S.C., Fundamentals of Engineering Heat & Mass Transfer, Wiley EasternLtd., New Delhi, 1981.

4. Mathur, M. and Sharma, R.P. Gas Turbine and Jet and Rocket Propulsion, StandardPublishers, New Delhi 1988.


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U07GEE01 INTELLECTUAL PROPERTY RIGHTS (IPR) 3 0 0 1001. Introduction 5

Introduction Invention and Creativity Intellectual Property (IP) Importance Protection of

IPR Basic types of property-Movable Property, Immovable Property and Intellectual Property.

2. Patents 10

IP Patents Copyrights and related rights Trade Marks and rights arising from Trademarkregistration Definitions Industrial Designs and Integrated circuits Protection of GeographicalIndications at national and International levels Application Procedures.

3. International Scenario 10

International convention relating to Intellectual Property Establishment of WIPO Mission andActivities History General Agreement on Trade and Tariff (GATT).

4. WTO 10

Indian Position Vs WTO and Strategies Indian IPR legislations commitments to WTO-PatentOrdinance and the Bill Draft of a national Intellectual Property Policy Present against unfaircompetition.

5. Copyrights 10

Case Studies on Patents (Basmati rice, turmeric, Neem, etc.) Copyright and related rights Trade Marks Industrial design and Integrated circuits Geographic indications Protectionagainst unfair competition.

TOTAL : 45

TEXT BOOK

1. Subbaram N.R. Handbook of Indian Patent Law and Practice , S. Viswanathan (Printersand Publishers) Pvt. Ltd., 1998.

REFERENCES

1. Eli Whitney, United States Patent Number: 72X, Cotton Gin, March 14, 1794.2. Intellectual Property Today: Volume 8, No. 5, May 2001, [www.iptoday.com].

3. Using the Internet for non-patent prior art searches, Derwent IP Matters, July 2000.[www.ipmatters.net/features/000707_gibbs.html.

Documents

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