The strain components εx, εy, and γxy are given for a point in a body subjected to plane strain. Determine the principal strains, the maximum in-plane shear strain, and the absolute maximum shear strain at the point. Show the angle θp, the principal strain deformations, and the maximum in-plane shear strain distortion on a sketch. εx = -750 με, εy = -345 με, and γxy = 1250 μrad. Enter the angle such that -45°≤θp≤ +45°. The strain components ɛx, ɛy, and Yxy are given for a point in a body subjected to plane strain. Determine the principal strains, themaximum in-plane shear strain, and the absolute maximum shear strain at the point. Show the angle 0, the principal straindeformations, and the maximum in-plane shear strain distortion on a sketch. Ex = -750 µɛ, ɛy = -345 µɛ, and yxy = 1250 µrad. Enter theangle such that -45°<0,< +45°.Answer:Ep1με%3DEp2 =με%3DYmax in-planepradYabsolute max.pradOp =

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The strain components εx, εy, and γxy are given for a point in a body subjected to plane strain. Determine the principal strains, the maximum in-plane shear strain, and the absolute maximum shear strain at the point. Show the angle θp, the principal strain deformations, and the maximum in-plane shear strain distortion on a sketch. εx = -750 με, εy = -345 με, and γxy = 1250 μrad. Enter the angle such that -45°≤θp≤ +45°.

The strain components εx, εy, and γxy are given for a point in a body subjected to plane strain. Determine the principal strains, the maximum in-plane shear strain, and the absolute maximum shear strain at the point. Show the angle θp, the principal strain deformations, and the maximum in-plane shear strain distortion on a sketch. εx = -750 με, εy = -345 με, and γxy = 1250 μrad. Enter the angle such that -45°≤θp≤ +45°.