A structural component in a fighter jet aircraft has a cellular cross-section (Fig. Q1). The component is 2 m long and is fabricated from an Al alloy, whose modulus of rigidity is 30 GPa. During a certain maneuver of the aircraft, a torque of 40 Nm is applied to the component. Using the Membrane Analogy Method, calculate: (a) the torsional shear stress in each cell of the cross-section; and (b) the angle of twist of the component, giving your answer in degrees. 2mm Imm 15 -1:5y 600mm

A structural component in a fighter jet aircraft has a cellular cross-section (Fig. Q1). The component is 2 m long and is fabricated from an Al alloy, whose modulus of rigidity is 30 GPa. During a certain maneuver of the aircraft, a torque of 40 Nm is applied to the component. Using the Membrane Analogy Method, calculate: (a) the torsional shear stress in each cell of the cross-section; and (b) the angle of twist of the component, giving your answer in degrees. 2mm Imm 15 -1:5y 600mm

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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