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  3. 4 a part of the segment on the fuselage skin...

Question: 4 a part of the segment on the fuselage skin...

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4. A part of the segment on the fuselage skin has a state of stress at a point as shown in the figure. Determine the equivalent state of stress on an element at the point, which represents (a) the principal stresses and (b) the maximum in-plane shear stress and the associated average normal stress. Also, for each case, determine the corresponding orientation of the element with respect to the element shown and sketch the results on the element. 20 points 50 MPa 15 MPa

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