The wing of an aircraft can be considered as a cantilever beam of length L, as shown in the Figure below. If the airlift is approximated as a sinusoidally distributed load, q(x)=q, sin- L find the displacement of the tip A. Consider only bending. The bending rigidity is El, uniform. y L q=qosin(x/L) A X

The wing of an aircraft can be considered as a cantilever beam of length L, as shown in the Figure below. If the airlift is approximated as a sinusoidally distributed load, q(x)=q, sin- L find the displacement of the tip A. Consider only bending. The bending rigidity is El, uniform. y L q=qosin(x/L) A X

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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