Theory of Structures
Principal planes are subjected to

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

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Theory of Structures
Slenderness ratio of a long column, is

Length of column divided by least radius of gyration
Area of cross-section divided by least radius of gyration
Area of cross-section divided by radius of gyration
Radius of gyration divided by area of cross-section

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