An element in plane stress on the fuselage of an airplane (figure part a) is subjected to compressive stresses with a magnitude of 42 MPa in the horizontal direction and tensile stresses with a magnitude of 9.5 MPa in the vertical direction (see figure part b). Also, shear stresses with a magnitude of 15.5 MPa act in the directions shown. having solutionspile.com

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An element in plane stress on the fuselage of an airplane (figure part a) is subjected to compressive stresses with a magnitude of 42 MPa in the horizontal direction and tensile stresses with a magnitude of 9.5 MPa in the vertical direction (see figure part b). Also, shear stresses with a magnitude of 15.5 MPa act in the directions shown.  having a brittle material, it has properties of Sut-205 Mpa and Sy= 620 Mpa. Use modified Mohr's theory to determine the factor of safety in the following states of plane stress  (a) 9.5 MPa ? (b) 42 MPa 15.5 MPa solutionspile.com

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