helloput 58 in roll no. thanks. urQ-1 The principal strains in a plane, measured experimentally at a point on the aluminumfuselage of a jet aircraft, are ɛ = (your roll number +100) x 106 , and ɛ2 = (your roll number +150) x 106. If this is a case of plane stress, determine the associated principal stresses at thepoint in the same plane.E = 10(103) ksiVal0.33.

Given e1 = 158 x 10-6 e2 = 208 x 10-6 Eal = 104 ksi' val = 0.33

Q-1 The principal strains in a plane, measured experimentally at a point on the aluminum fuselage of a jet aircraft, are ɛ1 = (your roll number +100) x 106 , and ɛ2 = (your roll number + 150) x 106. If this is a case of plane stress, determine the associated principal stresses at the point in the same plane. %3D 0.33. Eal 10(10³) ksi Val %3D

Q-1 The principal strains in a plane, measured experimentally at a point on the aluminum fuselage of a jet aircraft, are ɛ1 = (your roll number +100) x 106 , and ɛ2 = (your roll number + 150) x 106. If this is a case of plane stress, determine the associated principal stresses at the point in the same plane. %3D 0.33. Eal 10(10³) ksi Val %3D

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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