Structural Analysis and Strength of Materials
Quiz covering structural analysis, stress mechanics, beam deflection, truss analysis, and strength of materials including thermal stress, shear stress, and influence lines.
Questions
A rigid bar is suspended by three rods made of the same material as shown in the figure. The area and length of the central rod are 3A and L respectively, while that of the two outer rods are 2A and 2L respectively. If a downward force of 50 kN is applied to the rigid bar, the forces in the central and each of the outer rods will be
- 16.67 kN each
- 30 kN and 15 kN
- 30 kN and 10 kN
- 21.4 kN and 14.3 kN
The maximum and minimum shear stresses in a hollow circular shaft of outer diameter 20 mm and thickness 2 mm, subjected to a torque of 92.7 Nm will be
- 59 MPa and 47.2 MPa
- 10 MPa and 80 MPa
- 118 MPa and 160 MPa
- 200 MPa and 160 MPa
The shear stress at the neutral axis in a beam of triangular section with a base of 40 mm and height of 20 mm, subjected to a shear force of 3 kN is
- 3 MPa
- 6 MPa
- 10 MPa
- 20 MPa
A metal bar of length 100 mm is inserted between two rigid supports and its temperature is increased by 10°C. If the coefficient of thermal expansion is 12 x 10–6 per °C and the Young’s modulus is 2 x 105 MPa, the stress in the bar is
- zero
- 12 MPa
- 24 MPa
- 2400 MPa
The right triangular truss is made of members having equal cross-sectional area of 1550 mm2 and Young’s modulus of 2 x 105 MPa. The horizontal deflection of the joint Q is

- 2.47 mm
- 10.25 mm
- 14.1 mm
- 15.68 mm
The influence line diagram (ILD) shown is for the member

- PS
- RS
- PQ
- QS
A two span continuous beam having equal spans each of length L is subjected to a uniformly distributed load $\omega$ per unit length. The beam has constant flexural rigidity.
The reaction at the middle support is
- $\omega$L
- $\frac{5 \omega L}{2}$
- $\frac{5 \omega L}{4}$
- $\frac{\omega L^2}{16}$
The span(s) to be loaded uniformly for maximum positive (upward) reaction at support P, as shown in the figure below, is (are)

- PQ only
- PQ and QR
- QR and RS
- PQ and RS
A vertical PQ of length L is fixed at its top end P and has a flange to the bottom end Q. A weight W is dropped vertically from a height h (<L) on to the flange.
The axial stress in the rod can be reduced by
- increasing the length of the rod
- decreasing the length of the rod
- decreasing the area of cross-section of the rod
- increasing the modulus of elasticity of the material
The members EJ and IJ of a steel truss (shown in the figure below) are subjected to a temperature rise of 30oC. The coefficient of thermal expansion of steel is 0.000012 per oC per unit length. The displacement (mm) of joint E relative to joint H along the direction HE of the truss is

- 0.255
- 0.589
- 0.764
- 1.026
Beam GHI is supported by the pontoons as shown in the figure below. The horizontal cross sectional area of each pontoon is 8 m2, the flexural rigidity of the beam is 10000 kN-m2 and the unit weight of water is 10 kN-m3.

When the middle pontoon is removed, the deflection at H will be
- 0.2 m
- 0.4 m
- 0.6 m
- 0.8 m
The degree of static indeterminacy of the rigid frame having two internal hinges as shown in the figure below, is

- 8
- 7
- 6
- 5
The unit load method used in structural analysis is
- applicable only to statistically indeterminate structures
- another name for stiffness method
- an extension of Maxwell’s reciprocal theorem
- derived from Castigliano’s theorem
For linear elastic systems, the type of displacement function for the strain energy is
- linear
- quadratic
- cubic
- quartic
For a linear elastic structural system, minimization of potential energy yields
- compatibility conditions
- constitutive relations
- equilibrium equations
- strain-displacement relations
Muller Breslau principle in structural analysis is used for
- drawing influence line diagram for any force function
- writing virtual work equation
- super position of load effects
- none of these
A curved member with a straight vertical leg is carrying a vertical load at Z, as shown in the figure. The stress resultant(s) in the XY segment is/are

- bending moment, shear force and axial force
- bending moment and axial force only
- bending moment and shear force only
- axial force only

A bar of varying square cross section is loaded symmetrically as shown in the figure. Loads shown are placed on one of the axes of symmetry of cross-section. Ignoring self weight, the maximum tensile stress in N/mm2 anywhere is
- 16.0
- 20.0
- 25.0
- 30.0
The stiffness K of a beam deflecting in a symmetric mode, as shown in the figure, is

- $\frac{EI}{L}$
- $\frac{2EI}{L}$
- $\frac{4EI}{L}$
- $\frac{6EI}{L}$
The symmetry of stress tensor at a point in the body under equilibrium is obtained from
- conservation of mass
- force equilibrium equations
- moment equilibrium equations
- conservation of energy












