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Theory of Structures

Theory of Structures
The load on a spring per unit deflection, is called

Proof stress
Proof load
Proof resilience
Stiffness

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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
Rankine
Parabolic formula
Perry

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Theory of Structures
Principal planes are subjected to

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

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Theory of Structures
Stress may be expressed in Newtons

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

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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

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

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Theory of Structures
If Q is load factor, S is shape factor and F is factor of safety in elastic design, the following:

Q = S × F
Q = S – F
Q = F – S
Q = S + F

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