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The principal strains at a point on the aluminum fuselage of a jet aircraft are = 780(106) and e2 = 430(106). Part A Determine
The principal strains at a point on the aluminum fuselage of a jet aircraft are = 780(106) and e2 = 430(106). Part A Determine the associated principal stresses at the point in the same plane. Eal = 10(103) ksi, val = 0.33. Express your answers, separated by a comma, to three significant figures. 01,02= Submit vec - Previous Answers Request Answer ? ksi Review
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