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Theory of Structures

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

1.34
2.5
2.34
1.5

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Theory of Structures
The maximum deflection of a simply supported beam of span L, carrying an isolated load at the centre of the span; flexural rigidity being EI, is

WL3/24EL
WL3/8EL
WL3/48EL
WL3/3EL

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Theory of Structures
Stress may be expressed in Newtons

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

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Theory of Structures
The ratio of maximum and average shear stresses on a rectangular section, is

1.5
1.25
1
2.5

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

1/4
1/2
1
2

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

1½
½
1
2

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