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Theory of Structures

Theory of Structures
The moment of inertia of a triangular section (height h, base b) about its base, is

b²h/12
bh²/12
bh³/12
b³h/12

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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
Parabolic formula
Perry
Rankine

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Theory of Structures
Maximum shear stress theory for the failure of a material at the elastic limit, is known

Haig's theory
Rankine's theory
Guest's or Trecas' theory
St. Venant's theory

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Theory of Structures
Flat spiral springs

All of these
Consist of uniform thin strips
Consist of uniform thin strips
Are wound by applying a torque

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Theory of Structures
In case of principal axes of a section

Product of moment of inertia is zero
Difference of moment inertia is zero
Sum of moment of inertia is zero
None of these

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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
1/7
3/7
4/7

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