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Theory of Structures

Theory of Structures
The ratio of the stresses produced by a suddenly applied load and by a gradually applied load on a bar, is

1
1/2
1/4
2

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Theory of Structures
In case of principal axes of a section

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

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Theory of Structures
In plastic analysis, the shape factor for a circular section, is

1.2
1.3
1.7
1.5

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Theory of Structures
Total strain energy theory for the failure of a material at elastic limit, is known

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

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

bh³/12
bh²/12
b³h/12
b²h/12

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Theory of Structures
The locus of the end point of the resultant of the normal and tangential components of the stress on an inclined plane, is

Ellipse
Circle
Parabola
Straight line

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