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Theory of Structures

Theory of Structures
The ratio of maximum and average shear stresses on a rectangular section, is

1.5
1.25
1
2.5

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Theory of Structures
Principal planes are subjected to

Normal stresses as well as tangential stresses
Tangential stresses only
None of these
Normal stresses only

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Theory of Structures
For calculating the allowable stress of long columns σ0 = σy/n [1 - a (1/r)²]is the empirical formula, known as

Perry
Straight line formula
Parabolic formula
Rankine

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Theory of Structures
The ratio of shear stress and shear strain of an elastic material, is

Both A. and B.
Modulus of Rigidity
Shear Modulus
Modulus of Elasticity

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Theory of Structures
In a shaft, the shear stress is not directly proportional to

Modulus of rigidity
Angle of twist
Length of the shaft
Radius of the shaft

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Theory of Structures
The yield moment of a cross section is defined as the moment that will just produce the yield stress in

The outer most fibre of the section
The inner most fibre of the section
The fibre everywhere
The neutral fibre of the section

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