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Laxmi Institute of Technology, Sarigam
Approved by AICTE, New Delhi; Affiliated to Gujarat Technological University, Ahmedabad
Laxmi Institute of Technology, Sarigam
Approved by AICTE, New Delhi; Affiliated to Gujarat Technological University, Ahmedabad
Laxmi Institute of Technology, Sarigam
Approved by AICTE, New Delhi; Affiliated to Gujarat Technological University, Ahmedabad
Laxmi Institute of Technology, Sarigam
Approved by AICTE, New Delhi; Affiliated to Gujarat Technological University, Ahmedabad
ASSIGNMENT: 1
Name of Subject: - Structural Analysis I [S.A.1] Subject Code: - 2140603
Given Date: - 00/00/2019
FUNDAMENTALS
Sr. No. Name of Question
1 States the Maxwell’s Reciprocal theorem
2 Define Statically Determinate Beam Indeterminate Beam
3 Explain degree of static indeterminacy
4 Discuss about Stability of Structure
5 Find Static and Kinematic indeterminacy of the structures shown below.
6 Find Static and Kinematic indeterminacy of the structures shown below. And
also comment about Stability.
7 Find Static and Kinematic indeterminacy of the structures shown below.
8 Distinguish between Plane truss and Space Truss
Laxmi Institute of Technology, Sarigam
Approved by AICTE, New Delhi; Affiliated to Gujarat Technological University, Ahmedabad
9 Draw SF and BM diagram for the frame loaded as shown in fig.
10 Analyze the rigid jointed portal frame shown in fig. Draw Shear Force Diagram,
Bending Moment Diagram Axial Force Diagram.
Submission Date:
Name & Sign of Subject In-charge :
SAQUIB SHAIKH
Laxmi Institute of Technology, Sarigam
Approved by AICTE, New Delhi; Affiliated to Gujarat Technological University, Ahmedabad
ASSIGNMENT: 2
Name of Subject: - Structural Analysis I [S.A.1] Subject Code: - 2140603
Given Date: - 00/00/2019
DISPLACEMENT OF DETERMINATE BEAMS
Sr. No. Name of Question
1 Differentiate between real beam and Conjugate beam. Justify the support
condition in conjugate beam.
2 Determine slope at A & D and Deflection at C & D for overhanging beam loaded as shown in
fig. Take E = 200 GPa & I = 2 x 107 mm4. Using Conjugate beam method.
3 Find slope & Deflection for following structure as shown in fig. by Double Integration Method.
Take E = 200 KN/mm2 & I = 14400 x 104 mm4.
4 Find slope at point A and B using Macaulay’s Method.
Take E = 210GPa & I = 16000 x 104 mm4.
5 Find slope and Deflection at point A and B for beam as shown in Fig. using Conjugate beam
Method. Take EI = 3000 KN.m2
6 A Simply Supported beam of 3m Span carries two point loads of 120 KN and 80
KN at distance of 0.6m and 2m from left support. If for the beam E = 2.1 x 105
N/mm2 & I = 16 x 108mm4, calculate the deflection under load using Macaulay’s method.
7 A cantilever 2m long is loaded as shown in Fig. Find slope and deflection at free
end using Macaulay’s method.
Take E = 200 GPa & I = 160 x 106
mm4.
Laxmi Institute of Technology, Sarigam
Approved by AICTE, New Delhi; Affiliated to Gujarat Technological University, Ahmedabad
8 For beam as shown in fig. calculate the slope at support C and deflection under
point load. Take E = 2 x 105 N/mm2 & I = 5 x 108 mm4.
9 Find the slope and deflection at centre C of Simply supported beam AB as
shown in fig. by moment area method.Take E = 2 x 105 N/mm2 & I = 2 x 108 mm4.
10 Find the slope and deflection at free end of cantilever beam as shown in fig. by
moment area method. Take E = 2 x 105 N/mm2. The cross section of beam is rectangle of
200 x 300mm deep.
11 Find the slope and deflection at free end of cantilever beam as shown in fig. by
moment area method. Take E = 2 x 105 N/mm2 and I = 2 x 108 mm4.
12 Find: 1) Deflection of Cantilever beam with point load at free end.
2) Deflection of Cantilever beam with UDL throughout span
3) Deflection of Cantilever beam with point load not at free end.
4) Deflection of Cantilever beam partially loaded with UDL over
length l1 from the fixed end.
13 Find: 1) Deflection of Simply supported beam with central point load.
2) Deflection of Simply supported beam with UDL throughout span
3) Deflection of Simply supported beam with UDL on half span from
one support.
4) Deflection of Simply supported beam with eccentric point load.
Submission Date: -
Name & Sign of Subject In-charge :
ZEESHAN MUNSHI
Laxmi Institute of Technology, Sarigam
Approved by AICTE, New Delhi; Affiliated to Gujarat Technological University, Ahmedabad
ASSIGNMENT: 3
Name of Subject: - Structural Analysis I [S.A.1] Subject Code: - 2140603
Given Date: - 00/00/2019
COLUMN AND STRUT
Sr. No. Name of Question
1 A cast iron column of hollow circular section having 200mm external diameter and
20mm metal thickness, 5m length has to carry load of 120KN at an eccentricity of
20mm from the geometrical axis. Calculate the maximum and minimum stresses
induced in the section, if the ends are fixed. Also calculate the maximum
permissible eccentricity so that no tension is induced at the base. Take E 120GPa.
2 A 2.5 m long pin ended column of square cross section is made up of timber. Using Euler’s
formula, find out size of the column with a factor of safety 2 for 250KN axial load. Consider E =
12.5GPa, allowable stress in axial compression = 12 Mpa.
3 A steel bar of rectangular cross section 30mm x 40mm, pinned at each end is subjected to an axial
compressive load. The bar is 1.75m long. Determine the buckling load and the corresponding stress
using Euler’s formula. Also find minimum length for which Euler’s formula may be used to
determine buckling load, if the proportional limit of material is 200Mpa. Take = 200GPa.
4 A Circular column loaded by an axial load of 400 KN. The effective length of column is 6.0 m. The
permissible strength of material is 160 N/mm2, and Rankine constant 1/3600. The thickness of
material is to be taken as 10% of external diameter. Calculate external diameter of required section.
5 A steel strut is made up of 5 m long T section. The size of flange 250mm x 50mm and size of web
100mm x 50mm. The strut is hinged at the both ends. Calculate the safe axial load by rankine
formula, using FOS 3. Take Fc = 300N/mm2 and α = 1/7500.
Submission Date: 25-02-2019
Name & Sign of Subject In-charge :
ZEESHAN MUNSHI
Laxmi Institute of Technology, Sarigam
Approved by AICTE, New Delhi; Affiliated to Gujarat Technological University, Ahmedabad
ASSIGNMENT: 4
Name of Subject: - Structural Analysis I [S.A.1] Subject Code: - 2140603
Given Date: - 00/00/2019
DIRECT AND BENDING STRESSES
Sr. No. Name of Question
1 Explain limit of eccentricity and core of section and draw core diagram for
different core section.
2 Define: Axial load, Eccentric load, Eccentricity, core of section., co officient of wind resistance.
3 Explain the formula for maximum and minimum stresses in rectangular column. And also explain
stress distribution in column.
4 Explain stability condition of retaining wall.
5 A rectangular column section ABCD having side AB = BC = 500mm and BC = CD = 250 carries
a compressive load of 300Kn at corner B. Find stress at each corner A, B, C, D, and draw stress
distribution diagram for each side.
6 A column of T Section is subjected to a load of 100 KN at a point on the centroidal axis, 40 mm
below the centroidal x – x axis. Calculate the maximum and minimum stresses induced in the
section. size of flange : 200mm x 20mm and size of web: 100mm x 10mm.
7 A masonry dam 6m height, 3m wide at base and 1.2m wide at top, retain water on vertical face for
full height. Considering density of masonry as 17 KN/m3 and density of water 10 KN/m3, Find out
maximum and minimum pressure intensities at the base.
8 A cylindrical chimney, 25 m high, of uniform circular section is 5m external diameter and 2m
internal diameter. It is subjected to a horizontal wind pressure of 1400N/m2. If the co efficient of
wind pressure is 0.6 and unit weight of masonry is 22KN/m3. Find the maximum and minimum
stresses at the base of the section.
Submission Date: 25-02-2019
Name & Sign of Subject In-charge :
SAQUIB SHAIKH
Laxmi Institute of Technology, Sarigam
Approved by AICTE, New Delhi; Affiliated to Gujarat Technological University, Ahmedabad
ASSIGNMENT: 5
Name of Subject: - Structural Analysis I [S.A.1] Subject Code: - 2140603
Given Date: - 00/00/2019
ARCHES, CABLES, AND SUSPENSION BRIDGE
Sr. No. Name of Question
1 For a three hinged parabolic arch having rise of 6m, span of 40m and loaded by a
point load of 200KN at 10m from left support and an udl of 20Kn/m over right half,
Calculate the maximum bending moment in both halves. Also calculate the bending
moment, shear force and normal thrust at 15m from left support.
2 A symmetrical three hinged circular arch has span 20m and central rise 4m. It is
carrying point load 12KN at 6m from left side hinge.
Calculate : (1) thrust at springing
(2) Magnitude and direction of reactions at support
(3) B.M. at 4m from left
(4) Maximum +ve and –ve B.M.
3 A cable of span 150m and dip 15m carries a load of 6KN per meter run of
horizontal span. Find the maximum tension for the cableand inclinationof the cable
at the support. Also find vertical and horizontal forces in each per under the
following conditions.
(1) If the cable passes over smooth rollers on the top of pier.
(2) If the cable is clamped to a saddle with smooth rollers resting on he top of the
pier.
In each case, the back stay is inclined at 30° to the orizontal. If height of pier is
20m, Find max. B.M. in the pier.
4 A flexible rope weighing 1N per meter run between two point 40mapart and at the same level, 12m
above the ground. It is to carry a concentrated load of 300N at a point P, on the rope at horizontal
distance of 10m from the left hand support .What is the maximum height above the ground to
which the point P may be raised if the maximum tension in the rope is not to exceed 1000N?
5 A three hinged parabolic arch having rise of r, span of L , having two hinges at
same level. It is subjected to total load W, uniformly distributed over entire span.
Shows that there will be no B.M. at any point on the arch. Also calculate horizontal
thrust at support.
Submission Date: 08-03-2019
Name & Sign of Subject In-charge :
ZEESHAN MUNSHI
Laxmi Institute of Technology, Sarigam
Approved by AICTE, New Delhi; Affiliated to Gujarat Technological University, Ahmedabad
ASSIGNMENT: 6
Name of Subject: - Structural Analysis I [S.A.1] Subject Code: - 2140603
Given Date: - 00/00/2019
THIN CYLINDER
Sr. No. Name of Question
1 A thin cylindrical shell of internal diameter d, wall thickness t and length l, is
subjected to internal pressure p. Derive the expression for circumferential stress
produced if the efficiency of longitudinal joint is η?
2 A thin cylindrical shell of internal diameter d, wall thickness t and length l, is
subjected to internal pressure p. Derive the expression for change in volume of the
cylinder.
3 A thin cylindrical shell of internal diameter d, wall thickness t and length l, is
subjected to internal pressure p. prove that volumetric strain is equal to twice the
circumferential strain plus longitudinal strain.
4 A cylindrical shell 3 m long & 1 m internal diameter is subjected to internal pressure of 1 N/mm2. If
the thickness of the shell is 12 mm, find the circumferential & longitudinal stresses. Find also the
maximum shear stress & change in dimensions of the shell.
5 A thin sphere of 1.5m diameter is filled with fluid which exerts internal pressure of 3 N/mm2.
Calculate the thickness required for the sphere if the change in volume is not to exceed 2% of the
original volume.
6 A cylindrical boiler to generate internal steam pressure 2 N/mm2, is to be fabricated using 12mm
thick plate having a limiting tensile stress of 120 N/mm2. If the efficiencies of the longitudinal and
circumferential joints are 75% and 40% respectively, find the safe diameter of the boiler.
7 A cylindrical shell has 3.5m length, 1.2m diameter and 10mm thickness. The shell is subjected to
internal pressure of 2 N/mm2. Calculate the max. Shear stress and change in dimension of the shell.
Submission Date:
Name & Sign of Subject In-charge :
ZEESHAN MUNSHI
Laxmi Institute of Technology, Sarigam
Approved by AICTE, New Delhi; Affiliated to Gujarat Technological University, Ahmedabad
ASSIGNMENT: 7
Name of Subject: - Structural Analysis I [S.A.1] Subject Code: - 2140603
Given Date: - 00/00/2019
STRAIN ENERGY
Sr. No. Name of Question
1 A 35kg collar is released from height h to drop on disk at bottom end C of the bar
ABC. End A of the bar is fixed. Part AB is 2m long and 40mm in diameter. Part
BC is 1.5m long and 30mm in diameter. Calculate the height h for which the
maximum stress in the rod is 250MPa.
2 A steel bar 100 cm long and rectangular in section 40mm X 80mm is subjected to
an axial load of 1KN. Find the maximum stress if,
1) The load is applied gradually
2) The load is applied suddenly
3) The load is applied after falling through a height of 8 cm
What are the strain energies in each of the above cases? Take E = 200GPa.
3 Determine strain energy stored due to bending in the beam for the simply supported
beam subjected load 10 KN at 2m from left side. Ha span of beam is 3m.Take E =
210Gpa and I = 72 X 104 mm4.
4 A bar 54mm in diameter is 4m long. An axial load of 180Kn is suddenly applied to it.
Find:
1) The maximum instantaneous stress.
2) The maximum instantaneous elongation
3) Take work stored in the bar at the instant of maximum elongation.
E = 200Gpa.
Submission Date:
Name & Sign of Subject In-charge :
SAQUIB SHAIKH
Laxmi Institute of Technology, Sarigam
Approved by AICTE, New Delhi; Affiliated to Gujarat Technological University, Ahmedabad
ASSIGNMENT: 8
Name of Subject: - Structural Analysis I [S.A.1] Subject Code: - 2140603
Given Date: - 00/00/2019
FIXED BEAM AND CONSISTENT DEFORMATION METHOD
Sr. No. Name of Question
1 Draw S.F. and B.M. Diagram for fixed beam carrying central point load load.
2 Draw S.F. and B.M. Diagram for fixed beam carrying central UDL on entire span.
3 Draw S.F. and B.M. Diagram for fixed beam carrying eccentric point load W.
4 Analyze a fixed beam of span 8 m which is subjected to an udl of 22 KN/m over its entire span
along with a point load of 60 KN at its center. Use area moment method. Draw S.F. and B.M.
diagram for the fixed beam.
5 A fixed beam AB of span 6m is subjected to a concentrated couple of 227 KN.m
applied at a section 4m from the end A. Find the end moment from first principles
and draw B.M. and S.F. diagram.
6 Analyze the propped cantilever beam with UDl on entire span by consistent
deformation method and draw S.F. and B.M. Diagram.
7 Analyze the propped cantilever beam with 1 m overhang. 30KN load is applied at
free end by consistent deformation method and draw S.F. and B.M. Diagram.
8 Determine support reaction of Propped cantilever with 2m overhang. Beam is
subjected 40KN point load at 3m from left side, 30KN at free end. Anlyse the beam
by consistent deformation method.
Submission Date:
Name & Sign of Subject In-charge :
ZEESHAN MUNSHI
Laxmi Institute of Technology, Sarigam
Approved by AICTE, New Delhi; Affiliated to Gujarat Technological University, Ahmedabad
Laxmi Institute of Technology , Sarigam
Approved by AICTE, New Delhi; Affiliated to Gujarat Technological University, Ahmedabad
Academic Year 2018-19 Centre Code: 086 Examination : Mid Semester -1 Examination Branch: Civil Engineering Semester: 48th Sub Code: 2140603 Sub: Structure Analysis 1 Date: 05/02/2019 Time: 9:00-10:00 Marks: 20
Q.1 Find the suitable size of 3m long hollow circular water tank which subjected
maximum load 3500 N. Its Outer diameter is 1.25 times inner diameter. The hollow
circular water tank with flexible base for capacity 5,00,000 liters. The modulus of
elasticity for the material of water tank is 210 KN/mm2.
5
Q.2 A Column length 2.4 m area of Cross Section 2000 mm2 and Moment of Inertia of
Ixx = 720 X 104 mm4 and Iyy = 80 X 104 mm4 is subjected to buckling load. Both ends
are fixed. What is the slenderness ratio of Column?
3
OR
Q.2 Find the Moment of Inertia of Symmetrical I Section. The size of Flange is 200 mm
X 40 mm and Size of Web is 20 mm X 200 mm.
3
Q.3 A Closed Cylindrical vessel made of steel plates 4 mm thick with plane ends carries a
fluid under a pressure 3 N/mm2. The diameter of cylinder is 250 mm and length is
750 mm. Calculate Longitudinal and Hoop stress in cylindrical wall & Determine
Change in Diameter, Length, and Volume of Cylinder. Take E = 2.1 X 105 N/mm2
and Poisson’s ratio is 0.286.
7
Q.4(a)
Q.4(b)
The Kinematics Indeterminacy of Plane truss as Shown in Fig. is The degree of Static Indeterminacy of Rigid frame having Two internal hinges as
shown in Fig. Below
5