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Theory of Structures

Theory of Structures
section modulus of a square section of side B and that of a circular section of the ratio of the diameter D, is

2 /15
3 /16
/16
3 /8

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Theory of Structures
The general expression for the B.M. of a beam of length l is the beam carries M = (wl/2) x – (wx²/2)

None of these
A uniformly distributed load w/unit length
An isolated load at mid span
A load varying linearly from zero at one end to w at the other end

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Theory of Structures
Stress may be defined as

Force per unit area
None of these
Force per unit length
Force per unit volume

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Theory of Structures
The ratio of the length and diameter of a simply supported uniform circular beam which experiences maximum bending stress equal to tensile stress due to same load at its mid span, is

1/3
1/2
1/8
1/4

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Theory of Structures
The assumption in the theory of bending of beams is:

Material is isotropic
Young’s modulus is same in tension as well as in compression
All of these
Material is homogeneous

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Theory of Structures
A cantilever of length ‘L’ is subjected to a bending moment ‘M’ at its free end. If EI is the flexural rigidity of the section, the deflection of the free end, is

ML²/2EI
ML/2EI
ML²/3EI
ML/EI

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