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Structural Analysis

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21 Q 2 Topics Take Mock Test
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Difficulty: All Easy Medium Hard 11–20 of 21
Topics in Civil Engineering
All Structural Analysis 92 Concrete Technology 19
For a beam element in finite element analysis, the shape functions are typically:
A Linear functions
B Cubic Hermite polynomials
C Quadratic functions
D Trigonometric functions
Correct Answer:  B. Cubic Hermite polynomials
EXPLANATION

Beam elements use cubic Hermite shape functions to ensure C¹ continuity (displacement and slope continuity).

Test
In plastic hinge formation, the condition for plastic collapse is:
A Bending moment equals yield moment
B Deflection becomes zero
C Sufficient plastic hinges form to create mechanism
D Shear force equals yield shear
Correct Answer:  C. Sufficient plastic hinges form to create mechanism
EXPLANATION

Plastic collapse occurs when sufficient plastic hinges develop to convert the structure into a mechanism, allowing unbounded deformation.

Test
In the direct stiffness method, the global stiffness matrix is formed by:
A Assembly of element stiffness matrices
B Averaging element stiffness matrices
C Selection of largest element stiffness
D Transformation of local to global coordinates only
Correct Answer:  A. Assembly of element stiffness matrices
EXPLANATION

Global stiffness matrix is assembled by superposition of element stiffness matrices after coordinate transformation.

Test
For a beam with varying moment of inertia, the flexibility coefficient method requires:
A Constant EI throughout
B Integration with variable EI
C Average value of EI
D Maximum value of EI
Correct Answer:  B. Integration with variable EI
EXPLANATION

Flexibility coefficients for non-uniform beams require integration accounting for variable EI along the length.

Test
In a moving load problem on a simply supported beam, the maximum bending moment under a point load occurs when the load is positioned:
A At the midspan
B At 0.577L from nearest support
C At any position for symmetry
D When the shear force equals zero
Correct Answer:  D. When the shear force equals zero
EXPLANATION

Maximum bending moment occurs at the section where shear force is zero (point of contraflexure). For moving loads, position varies but this principle always applies.

Test
A parabolic arch carries a uniformly distributed load. At the crown (center) of the arch, the horizontal thrust is minimum when the rise-to-span ratio is:
A 1/4
B 1/3
C 1/2
D 2/3
Correct Answer:  C. 1/2
EXPLANATION

For a parabolic arch under UDL, the horizontal thrust H = wL²/(8f), where f is rise. The thrust decreases with increase in rise-to-span ratio. Optimal ratio is 1/2 for many design considerations.

Test
A simply supported beam with central point load shows maximum deflection at:
A At the point of load
B At distance L/√3 from either support
C At distance 0.577L from either support
D Exactly at center for symmetric loading
Correct Answer:  C. At distance 0.577L from either support
EXPLANATION

For SS beam with central load, maximum deflection occurs at x = L/√3 ≈ 0.577L from support, not at center due to boundary conditions.

Test
In Williot-Mohr diagram for a truss, what do the lines represent?
A Member forces
B Deflected position of joints
C Strain of members
D Stress distribution
Correct Answer:  B. Deflected position of joints
EXPLANATION

Williot-Mohr diagram graphically represents the deflected shape showing displaced position of all joints in a truss.

Test
The Castigliano's first theorem relates:
A Deflection to external load
B Partial derivative of strain energy to deflection
C Partial derivative of strain energy to load equals deflection
D Stress to strain directly
Correct Answer:  C. Partial derivative of strain energy to load equals deflection
EXPLANATION

Castigliano's first theorem: ∂U/∂P = δ, where U is strain energy and δ is deflection at point of load P.

Test
A frame with 'j' joints, 'm' members, and 'r' reaction components is indeterminate with degree:
A DI = m + r - 2j
B DI = m + r - 3j
C DI = 3m + r - 2j
D DI = 2m + r - 3j
Correct Answer:  A. DI = m + r - 2j
EXPLANATION

For planar frames: DI = (m + r) - 2j, where 2j accounts for 2 equilibrium equations per joint in 2D.

Test
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