The principal strains at a point on the aluminum fuselage of a jet aircraft are €1 = 880(10-6) and €2 - 400(10-6). E-10 (10³) ksi, val = 0.33. Part A Determine the associated principal stresses at the point in the same plane. Hint. For the case of plane stress, Hooke's law can be written as στ E (1-v2) (E₂+Veg), = (Ez + VEy), σy E (1-2) (Ey+VER). Express your answers in kilopounds per square inch to three significant figures separated by a comma. 01,02 = ΜΕ ΑΣΦ JA vecl Submit Request Answer ? ksi Review

Please do not rely too much on chatgpt, because its answer may be wrong. Please consider it carefully and give your own answer. You can borrow ideas from gpt, but please do not believe its answer.Very very grateful!Please do not rely too much on chatgpt, because its answer may be wrong. Please consider it carefully and give your own answer. You can borrow ideas from gpt, but please do not believe its answer. and and Very very grateful!

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