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Theory of Structures

Theory of Structures
The ratio of the deflections of the free end of a cantilever due to an isolated load at 1/3rd and 2/3rd of the span, is

2/7
4/7
1/7
3/7

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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

Straight line formula
Perry
Rankine
Parabolic formula

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Theory of Structures
The maximum magnitude of shear stress due to shear force F on a rectangular section of area A at the neutral axis, is

F/2A
F/A
3F/2A
2F/3A

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Theory of Structures
At any point of a beam, the section modulus may be obtained by dividing the moment of inertia of the section by

Depth of the section
Depth of the neutral axis
Maximum tensile stress at the section
Maximum compressive stress at the section

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Theory of Structures
A body is said to be in equilibrium if

None of these
It moves vertically
It rotates about its C.G.
It moves horizontally

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Theory of Structures
Stress may be expressed in Newtons

Per millimetre square (N/mm²)
None of these
Per metre square (N/m2)
Per centimetre square (N/cm²)

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