Aerospace Engineering > GATE 2019 > Column Buckling
All the bars in the given truss are elastic with Young's modulus 200 GPa, and have identical cross-sections with moment of inertia 0.1 cm^4. The lowest value of the load P at which the truss fails due to buckling is _______ kN (round off to the nearest integer).

Correct : 550 to 570

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truss buckling critical buckling load Aerospace Engineering GATE 2019 elastic truss failure Young's modulus moment of inertia GATE AE 2019 Q44 structural buckling

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