Aerospace Engineering > GATE 2010 > Column Buckling
A column of length I and flexural rigidity El, has one end fixed and the other end hinged. The
critical buckling load for the column is
A
π2EI/(0.5l)2
B
π2EI/(0.7i)2
C
π2EI/t2
D
π2EI/(2l)2

Correct : b

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Related Topics

critical buckling load Euler buckling load fixed hinged column effective length of column GATE Aerospace Engineering 2010 GATE AE 2010 Q16 flexural rigidity column buckling column buckling formula

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