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Part of a control linkage for an airplane consists of a rigid member CB and a flexible cable AB Originally the cable is unstr
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If a force is applied to the end B of the member and causes it to rotate by 0-0.61, determine the normal strain in the cable
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PLz UPvote Thank YouSolution | LAB = /Bc? + Ac? 800mm (800) + (600) ber LAB = 1000mm A 1. LAB = 1 K 600mm Consider DACB ; - (:O = 0.61 (given) )Normal Strain in the Cable (EAB; EAR = 1 LABI - LABI LAB putting values LAB=994.877mm LAB = 1000 mm EAB = 994.877 - 1000 1 1

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