The principal strains in a plane, measured experimentally at a point on the aluminum fuselage of a jet aircraft, are ϵ1 = 630(10−6) and ϵ2− 350(10−6). If this is a case of plane stress, determine the associated principal stresses at the point in the same plane. Eal = 10(103) ksi and νal = 0.33.
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