Question 29

AEMCQ2 marksNeeds review
A load

is applied to the free end of a stepped cantilever beam as shown in the figure. The Young’s modulus of the material is

, and the moments of inertia of the two sections of length 2 m and 1 m are

and

, respectively. Ignoring transverse shear and stress concentration effects, the deflection at the point where the load is applied at the free end of the cantilever is
Diagram for Aerospace Engineering question 29

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2020AE

GATE AE 2020 · Paper 1

Aerospace Engineering · Original paper archive

Section
Aerospace Engineering
Question type
Multiple choice (MCQ)
Marks
2 marks

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