The principal strains at a point on the aluminum fuselage of a jet aircraft are =...

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The principal strains at a point on the aluminum fuselage of a jet aircraft are = 780(10-6) and 2 = 410(10-6). Part A Determine the associated principal stresses at the point in the same plane. Eal = 10(103) ksi, val = Express your answers, separated by a comma, to three significant figures. 01,02= 1 . 11 vec Submit Request Answer ? ksi 0.33. The principal strains at a point on the aluminum fuselage of a jet aircraft are = 780(10-6) and 2 = 410(10-6). Part A Determine the associated principal stresses at the point in the same plane. Eal = 10(103) ksi, val = Express your answers, separated by a comma, to three significant figures. 01,02= 1 . 11 vec Submit Request Answer ? ksi 0.33.