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Theory of Structures

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

2.5
1
1.25
1.5

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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

Straight line
Parabola
Circle
Ellipse

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Theory of Structures
Maximum principal stress theory for the failure of a material at elastic point, is known

Rankine's theory
Von Mises' theory
St. Venant's theory
Guest's or Trecas' theory

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Theory of Structures
Principal planes are subjected to

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

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

2.34
1.34
2.5
1.5

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Theory of Structures
A simply supported uniform rectangular bar breadth b, depth d and length L carries an isolated load W at its mid-span. The same bar experiences an extension e under same tensile load. The ratio of the maximum deflection to the elongation, is

L/2d
L/d
(L/3d)²
(L/2d)²

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