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Theory of Structures

Theory of Structures
The maximum bending moment for a simply supported beam with a uniformly distributed load w/unit length, is

WI²/4
WI²/8
WI²/12
WI/2

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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

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

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Theory of Structures
Principal planes are subjected to

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

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Theory of Structures
For beams of uniform strength, if depth is constant,

Width b 1/M
Width b M 2
Width b 3 M
Width b M

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

All of these
Magnitude
Point of application
Direction

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

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