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This section includes 719 Mcqs, each offering curated multiple-choice questions to sharpen your Civil Engineering knowledge and support exam preparation. Choose a topic below to get started.
501. |
Two bars of different materials and same size are subjected to the same tensile force. If the bars have unit elongation in the ratio of 2:5, then the ratio of modulus of elasticity of the two materials will be |
A. | 2:5 |
B. | 5:2 |
C. | 4:3 |
D. | 3:4 |
Answer» C. 4:3 | |
502. |
The unit of Young's modulus is same as that of stress. |
A. | True |
B. | False |
Answer» B. False | |
503. |
Modulus of rigidity may be defined as the ratio of |
A. | linear stress to lateral strain |
B. | lateral strain to linear strain |
C. | linear stress to linear strain |
D. | shear stress to shear strain |
Answer» E. | |
504. |
Young's modulus may be defined as the ratio of |
A. | linear stress to lateral strain |
B. | lateral strain to linear strain |
C. | linear stress to linear strain |
D. | shear stress to shear strain |
Answer» D. shear stress to shear strain | |
505. |
The change in length due to a tensile or compressive force acting on a body is given by (where P = Tensile or compressive force acting on the body, l = Original length of the body, A = Cross-sectional area of the body, and E = Young's modulus for the material of the body) |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
Answer» C. [C]. | |
506. |
When a change in length takes place, the strain is known as |
A. | linear strain |
B. | lateral strain |
C. | volumetric strain |
D. | shear strain |
Answer» B. lateral strain | |
507. |
The ratio of linear stress to the linear strain is called |
A. | modulus of rigidity |
B. | modulus of elasticity |
C. | bulk modulus |
D. | Poisson's ratio |
Answer» C. bulk modulus | |
508. |
The unit of modulus of elasticity is same as those of |
A. | stress, strain and pressure |
B. | stress, force and modulus of rigidity |
C. | strain, force and pressure |
D. | stress, pressure and modulus of rigidity |
Answer» E. | |
509. |
Which of the following is a proper sequence? |
A. | proportional limit, elastic limit, yielding, failure |
B. | elastic limit, proportional limit, yielding, failure |
C. | yielding, proportional limit, elastic limit, failure |
D. | none of the above |
Answer» B. elastic limit, proportional limit, yielding, failure | |
510. |
Hook's law holds good up to |
A. | yield point |
B. | elastic limit |
C. | plastic limit |
D. | breaking point |
Answer» C. plastic limit | |
511. |
When a body is subjected to two equal and opposite forces, acting tangentially across the resisting section, as a result of which the body tends to shear off across the section, the stress and strain induced is |
A. | tensile stress, tensile strain |
B. | compressive stress, compressive strain |
C. | shear stress, tensile strain |
D. | shear stress, shear strain |
Answer» E. | |
512. |
When a body is subjected to two equal and opposite pulls, as a result of which the body tends to extend its length, the stress and strain induced is |
A. | compressive stress, tensile strain |
B. | tensile stress, compressive strain |
C. | tensile stress, tensile strain |
D. | compressive stress, compressive strain |
Answer» D. compressive stress, compressive strain | |
513. |
Strain is equal to (where l = Original length, and δl = Change in length) |
A. | l/δl |
B. | δl/l |
C. | l.δl |
D. | l + δl |
Answer» C. l.δl | |
514. |
The unit of stress in S.I. units is |
A. | N/mm2 |
B. | kN/mm2 |
C. | N/m2 |
D. | any one of these |
Answer» E. | |
515. |
Whenever some external system of forces acts on a body, it undergoes some deformation. As the body undergoes some deformation, it sets up some resistance to the deformation. This resistance per unit area to deformation, is called |
A. | strain |
B. | stress |
C. | pressure |
D. | modulus of elasticity |
Answer» C. pressure | |
516. |
As compared to uniaxial tension or compression, the strain energy stored in bending is only |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
Answer» D. [D]. | |
517. |
Shear deflection of a cantilever of length L, cross sectional area A and shear modulus G, subjected to w/m u.d.l., is |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
Answer» B. [B]. | |
518. |
Shear deflection of a cantilever of length L, cross sectional area A and shear modulus G, under a concentrated load W at its free end, is |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
Answer» D. [D]. | |
519. |
If S is the shear force at a section of an I-joist, having web depth d and moment of inertia I about its neutral axis, the difference between the maximum and mean shear stresses in the web is, |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
Answer» E. | |
520. |
For a channel section, the shear centre lies at a distance of |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
Answer» D. [D]. | |
521. |
The width of a beam of uniform strength having a constant depth d length L, simply supported at the ends with a central load W is |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
Answer» C. [C]. | |
522. |
The energy stored in a beam of length L subjected to a constant B.M. is |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
Answer» B. [B]. | |
523. |
A cast iron T section beam is subjected to pure bending. For maximum compressive stress to be three times the maximum tensile stress, centre of gravity of the section from flange side is |
A. | h/4 |
B. | h/3 |
C. | h/2 |
D. | 2/3 h. |
Answer» B. h/3 | |
524. |
A rectangular bar of width b and height h is being used as a cantilever. The loading is in a plane parallel to the side b. The section modulus is |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | none of these. |
Answer» D. none of these. | |
525. |
An open-ended cylinder of radius r and thickness t is subjected to internal pressure p. The Young's modulus for the material is E and Poisson's ratio is μ. The longitudinal strain is |
A. | zero |
B. | [B]. |
C. | [C]. |
D. | none of these. |
Answer» B. [B]. | |
526. |
For a simply supported beam of length L, the bending moment M is described as M = a (x - x3/L2), 0 ≤ x < L; where a is a constant. The shear force will be zero at |
A. | the supports |
B. | x = L/2 |
C. | x = L/3 |
D. | x = L/3 |
Answer» D. x = L/3 | |
527. |
A closely coiled helical spring of radius R, contains n turns and is subjected to an axial load W. If the radius of the coil wire is r and modulus of rigidity of the coil material is C, the stress developed in the helical spring is |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
Answer» C. [C]. | |
528. |
A closely coiled helical spring of radius R, contains n turns and is subjected to an axial load W. If the radius of the coil wire is r and modulus of rigidity of the coil material is C, the deflection of the coil is |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
Answer» E. | |
529. |
A composite member shown in below figure was formed at 25°C and was made of two materials a and b. If the coefficient of thermal expansion of a is more than that of b and the composite member is heated upto 45°C, then |
A. | a will be in tension and b in compression |
B. | both will be in compression |
C. | both will be in tension |
D. | a will be in compression and b in tension. |
Answer» E. | |
530. |
The structure shown in below figure is stable, if |
A. | [A]. |
B. | x = 2y |
C. | x = y |
D. | 2x = y. |
Answer» E. | |
531. |
The maximum deflection of |
A. | a simply supported beam carrying a uniformly increasing load from either end and having the apex at the mid span is |
B. | a fixed ended beam carrying a distributed load over the span is |
C. | a fixed ended beam carrying a concentrated load at the mid span is |
D. | a cantilever beam subjected to a moment M at the free end is |
E. | All the above. |
Answer» F. | |
532. |
The bending moment at C of a portal frame shown in below figure is(1st distance 4m) |
A. | 8 t-m |
B. | 4 t-m |
C. | 28 t-m |
D. | 16 t-m |
E. | zero. |
Answer» F. | |
533. |
In a simply supported beam (l + 2a) with equal overhangs (a) and carrying a uniformly distributed load over its entire length, B.M. at the middle point of the beam will be zero if |
A. | l = 2a |
B. | l = 4a |
C. | l < 2a |
D. | l > a |
E. | l > 3a. |
Answer» B. l = 4a | |
534. |
If a circular beam of diameter d experiences a longitudinal strain and a lateral strain the volumetric strain is |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
E. | none of these. |
Answer» C. [C]. | |
535. |
If a member carries a tensile force P on its area of cross-section A, the normal stress introduced on an inclined plane making an angle θ with its transverse plane, is |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
E. | [E]. |
Answer» C. [C]. | |
536. |
The stress in the wall of a cylinder in a direction normal to its longitudinal axis, due to a force acting along the circumference, is known as |
A. | yield stress |
B. | longitudinal stress |
C. | hoop stress |
D. | circumferential stress |
E. | ultimate stress. |
Answer» D. circumferential stress | |
537. |
If p is the internal pressure in a thin cylinder of diameter d and thickness t, the developed hoop stress, is |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
E. | [E]. |
Answer» B. [B]. | |
538. |
If a shaft is rotating N revolutions per minute with an applied torque T kg-m, the horse power being transmitted by the shaft, is |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
E. | none of these. |
Answer» D. [D]. | |
539. |
The tension coefficient of any member is |
A. | force divided by the length |
B. | tension divided by the length |
C. | tension per unit area |
D. | tension in the member. |
Answer» C. tension per unit area | |
540. |
The stiffness factor for a prismatic beam of length L and moment of inertia I, is |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
E. | [E]. |
Answer» B. [B]. | |
541. |
If n is the ratio of internal and external diameters of a hollow shaft, the ratio of the weight of the hollow shaft and that of solid shaft of same strength, will be |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
Answer» C. [C]. | |
542. |
If a shaft is simultaneously subjected to a toque T and a bending moment M, the ratio of maximum bending stress and maximum shearing stress is |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
E. | [E]. |
Answer» D. [D]. | |
543. |
If a solid shaft is subjected to a torque T at its end such that maximum shear stress does not exceed fz the diameter of the shaft will be |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | none of these. |
Answer» D. none of these. | |
544. |
The ratio of the moments of resistance of a solid circular shaft of diameter D and a hollow shaft (external diameter D and internal diameter d), is |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
E. | none of these. |
Answer» B. [B]. | |
545. |
Reactions at the supports of a structure can be determined by equating the algebraic sum of |
A. | horizontal forces to zero |
B. | vertical forces to zero |
C. | moment about any point to zero |
D. | all the above. |
Answer» E. | |
546. |
The reaction at the supports will be vertical to the plane of the support if the frame structure rests on |
A. | roller supports |
B. | free supports |
C. | hinged supports |
D. | all the above. |
Answer» E. | |
547. |
The rise of a parabolic arch at quarter points, is equal to |
A. | times the rise of the crown |
B. | times the rise of the crown |
C. | times the rise of the crown |
D. | times the rise of the crown |
E. | times the rise of the crown. |
Answer» E. times the rise of the crown. | |
548. |
If a three hinged parabolic arch carries a uniformly distributed load on its entire span, every section of the arch resists. |
A. | compressive force |
B. | tensile force |
C. | shear force |
D. | bending moment. |
Answer» B. tensile force | |
549. |
The greatest eccentricity which a load W can have without producing tension on the cross-section of a short column of external diameter D and internal diameter d, is |
A. | [A]. |
B. | [B]. |
C. | [C]. |
D. | [D]. |
E. | [E]. |
Answer» D. [D]. | |
550. |
The length of a column, having a uniform circular cross-section of 7.5 cm diameter and whose ends are hinged, is 5 m. If the value of E for the material is 2100 tonnes/cm2, the permissible maximum crippling load will be |
A. | 1.288 tonnes |
B. | 12.88 |
C. | 128.8 tonnes |
D. | 288 |
E. | none of these. |
Answer» C. 128.8 tonnes | |