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Theory of Structures

Theory of Structures
The ratio of circumferential stress to the longitudinal stress in the walls of a cylindrical shell, due to flowing liquid, is

2
½
1½
1

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Theory of Structures
Inertia of a rectangular section of width and depth about an axis passing the moment of through C.G. and parallel to its width is

B²D/6
BD³/12
BD²/6
BD³/6

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

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

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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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Theory of Structures
The maximum deflection due to a load W at the free end of a cantilever of length L and having flexural rigidity EI, is

WL3/3EI
WL²/3EI
WL3/2EI
WL²/2EI

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Theory of Structures
Gradually applied static loads do not change with time their

Magnitude
All of these
Point of application
Direction

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