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MCQ Questions for CBSE Class 12 with Answers
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Structural Analysis MCQ Interview Questions and Answers
1.
The number of independent equations to be satisfied for static equilibrium of a plane structure is
1
2
3
6
2.
If there are m unknown member forces, r unknown reaction components and j number of joints, then the degree of static indeterminacy of a pin-jointed plane frame is given by
m + r + 2j
m – r + 2j
m + r – 2j
m + r – 3j
3.
Number of unknown internal forces in each member of a rigid jointed plane frame is
1
2
3
6
4.
Degree of static indeterminacy of a rigid-jointed plane frame having 15 members, 3 reaction components and 14 joints is
2
3
6
8
5.
Degree of kinematic indeterminacy of a pin-jointed plane frame is given by
2j – r
j – 2r
3j – r
2j + r
6.
Independent displacement components at each joint of a rigid-jointed plane frame are
three linear movements
two linear movements and one rotation
one linear movement and two rotations
three rotations
7.
If in a pin-jointed plane frame (m + r) > 2j, then the frame is where m is number of members, r is reaction components and j is number of joints
stable and statically determinate
stable and statically indeterminate
unstable
none of the above
8.
A pin-jointed plane frame is unstable if where m is number of members, r is reaction components and j is number of joints
(m + r)<2j
m + r = 2j
(m + r)>2j
none of the above
9.
A rigid-jointed plane frame is stable and statically determinate if where m is number of members, r is reaction components and j is number of joints
(m + r) = 2j
(m + r) = 3j
(3m + r) = 3j
(m + 3r) = 3j
10.
The number of independent equations to be satisfied for static equilibrium in a space structure is
2
3
4
6
11.
The degree of static indeterminacy of a pin-jointed space frame is given by where m is number of unknown member forces, r is unknown reaction components and j is number of joints
m + r – 2j
m + r – 3j
3m + r – 3j
m + r + 3j
12.
The degree of static indeterminacy of a rigid-jointed space frame is where m, r and j have their usual meanings
m + r – 2j
m + r – 3j
3m + r – 3j
6m + r – 6j
13.
The degree of kinematic indeterminacy of a pin-jointed space frame is where j is number of joints and r is reaction components
2j-r
3j-r
j-2r
j-3r
14.
The number of independent displacement components at each joint of a rigid-jointed space frame is
1
2
3
6
15.
If in a rigid-jointed space frame, (6m + r) < 6j, then the frame is
unstable
stable and statically determinate
stable and statically indeterminate
none of the above
16.
The principle of virtual work can be applied to elastic system by considering the virtual work of
internal forces only
external forces only
internal as well as external forces
none of the above
17.
Castigliano’s first theorem is applicable
for statically determinate structures only
when the system behaves elastically
only when principle of superposition is valid
none of the above
18.
Principle of superposition is applicable when
deflections are linear functions of applied forces
material obeys Hooke’s law
the action of applied forces will be affected by small deformations of the structure
none of the above
19.
In moment distribution method, the sum of distribution factors of all the members meeting at any joint is always
zero
less than 1
1
greater than 1
20.
The carryover factor in a prismatic member whose far end is fixed is
0
1/2
3/4
1
21.
In column analogy method, the area of an analogous column for a fixed beam of span L and flexural rigidity El is taken as
L/EI
L/2EI
L/3EI
L/4EI
22.
The degree of static indeterminacy up to which column analogy method can be used is
2
3
4
unrestricted
23.
The deflection at any point of a perfect frame can be obtained by applying a unit load at the joint in
vertical direction
horizontal direction
inclined direction
the direction in which the deflection is required
24.
In the slope deflection equations, the deformations are considered to be caused by i) bending moment ii) shear force iii) axial force The correct answer is
only (i)
(i)and(ii)
(ii) and (iii)
(i), (ii) and (iii)
25.
The three moments equation is applicable only when
the beam is prismatic
there is no settlement of supports
there is no discontinuity such as hinges within the span
the spans are equal
26.
While using three moments equation, a fixed end of a continuous beam is replaced by an additional span of
zero length
infinite length
zero moment of inertia
none of the above
27.
The Castigliano’s second theorem can be used to compute deflections
in statically determinate structures only
for any type of structure
at the point under the load only
for beams and frames only
28.
Bending moment at any section in a conjugate beam gives in the actual beam
slope
curvature
deflection
bending moment
29.
For a two-hinged arch, if one of the supports settles down vertically, then the horizontal thrust
is increased
is decreased
remains unchanged
becomes zero
30.
For a symmetrical two hinged parabolic arch, if one of the supports settles horizontally, then the horizontal thrust
is increased
is decreased
remains unchanged
becomes zero
31.
A single rolling load of 8 kN rolls along a girder of 15 m span. The absolute maximum bending moment will be
8 kN.m
15 kN.m
30 kN.m
60 kN.m
32.
The maximum bending moment due to a train of wheel loads on a simply supported girder
always occurs at centre of span
always occurs under a wheel load
never occurs under a wheel load
none of the above
33.
When a uniformly distributed load, longer than the span of the girder, moves from left to right, then the maximum bending moment at mid section of span occurs when the uniformly distributed load occupies
less than the left half span
whole of left half span
more than the left half span
whole span
34.
When a uniformly distributed load, shorter than the span of the girder, moves from left to right, then the conditions for maximum bending moment at a section is that
the head of the load reaches the section
the tail of the load reaches the section
the load position should be such that the section divides it equally on both sides
the load position should be such that the section divides the load in the same ratio as it divides the span
35.
When a series of wheel loads crosses a simply supported girder, the maximum bending moment under any given wheel load occurs when
the centre of gravity of the load system is midway between the centre of span and wheel load under consi-deration
the centre of span is midway between the centre of gravity of the load system and the wheel load under consideration
the wheel load under consideration is midway between the centre of span and the centre of gravity of the load system
none of the above
36.
Which of the following is not the displacement method ?
Equilibrium method
Column analogy method
Moment distribution method
Kani’s method
37.
Study the following statements. i) The displacement method is more useful when degree of kinematic indeterminacy is greater than the degree of static indeterminacy. ii) The displacement method is more useful when degree of kinematic indeterminacy is less than the degree of static indeterminacy. iii) The force method is more useful when degree of static indeterminacy is greater than the degree of kinematic indeterminacy. iv) The force method is more useful when degree of static indeterminacy is less than the degree of kinematic indeterminacy. The correct answer is
(i) and (iii)
(ii) and (iii)
(i) and (iv)
(ii) and (iv)
38.
Select the correct statement
Flexibility matrix is a square symmetrical matrix
Stiffness matrix is a square symmetrical matrix
both (a) and (b)
none of the above
39.
To generate the j th column of the flexibility matrix
a unit force is applied at coordinate j and the displacements are calculated at all coordinates
a unit displacement is applied at co-ordinate j and the forces are calculated at all coordinates
a unit force is applied at coordinate j and the forces are calculated at all coordinates
a unit displacement is applied at co-ordinate j and the displacements are calculated at all co-ordinates
40.
For stable structures, one of the important properties of flexibility and stiffness matrices is that the elements on the main diagonal i) of a stiffness matrix must be positive ii) of a stiffness matrix must be negative iii) of a flexibility matrix must be positive iv) of a flexibility matrix must be nega¬tive The correct answer is
(i) and (iii)
(ii) and (iii)
(i) and (iv)
(ii) and (iv)
41.
Effects of shear force and axial force on plastic moment capacity of a structure are respectively to
increase and decrease
increase and increase
decrease and increase
decrease and decrease
42.
Which of the following methods of structural analysis is a force method ?
slope deflection method
column analogy method
moment distribution method
none of the above
43.
Which of the following methods of structural analysis is a displacement method ?
moment distribution method
column analogy method
three moment equation
none of the above
44.
In the displacement method of structural analysis, the basic unknowns are
displacements
force
displacements and forces
none of the above
45.
The fixed support in a real beam becomes in the conjugate beam a
roller support
hinged support
fixed support
free end
46.
The width of the analogous column in the method of column analogy is
2/EI
1/EI
1/2 EI
1/4 EI
47.
A simply supported beam deflects by 5 mm when it is subjected to a concentrated load of 10 kN at its centre. What will be deflection in a 1/10 model of the beam if the model is subjected to a 1 kN load at its centre ?
5 mm
0.5 mm
0.05 mm
0.005mm
48.
The deformation of a spring produced by a unit load is called
stiffness
flexibility
influence coefficient
unit strain
49.
For a single point load W moving on a symmetrical three hinged parabolic arch of span L, the maximum sagging moment occurs at a distance x from ends. The value of x is
0.211 L
0.25 L
0.234 L
0.5 L
50.
Muller Breslau’s principle for obtaining influence lines is applicable to ) trusses i) statically determinate beams and frames ii) statically indeterminate structures, the material of which is elastic and follows Hooke’s law v) any statically indeterminate structure he correct answer is
(i), (ii) and (iii)
(i), (ii) and (iv)
(i) and (ii)
only (i)
51.
Consider the following statements: Sinking of an intermediate support of a continuous beam 1. reduces the negative moment at support. 2. increases the negative moment at support. 3. reduces the positive moment at support. 4. increases the positive moment at the centre of span. Of these statements
i and 4 are correct
1 and 3 are correct
2 and 3 are correct
2 and 4 are correct
52.
A load ‘W is moving from left to right support on a simply supported beam of span T. The maximum bending moment at 0.4 1 from the left support is
0.16 Wl
0.20 Wl
0.24 Wl
0.25 Wl
53.
When a load crosses a through type Pratt truss in the direction left to right, the nature of force in any diagonal member in the left half of the span would
change from compression to tension
change from tension to compression
always be compression
always be tension
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