The strain components for a point in a body subjected to plane strain are εx = 530 με, εy = 810με and γxy = -956 μrad. Using Mohr’s circle, determine the principal strains (εp1 > εp2), the maximum inplane shear strain γip, and the absolute maximum shear strain γmax at the point. Show the angle θp (counterclockwise is positive, clockwise is negative), the principal strain deformations, and the maximum in-plane shear strain distortion in a sketch.

Structural Analysis
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The strain components for a point in a body subjected to plane strain are εx = 530 με, εy = 810με and γxy = -956 μrad. Using Mohr’s circle, determine the principal strains (εp1 > εp2), the maximum inplane shear strain γip, and the absolute maximum shear strain γmax at the point. Show the angle θp (counterclockwise is positive, clockwise is negative), the principal strain deformations, and the maximum in-plane shear strain distortion in a sketch.

The strain components for a point in a body subjected to plane strain are &x = 530 μe, &y=810μe and Yxy = -956 urad. Using Mohr's
circle, determine the principal strains (Ep1 > Ep2), the maximum inplane shear strain Yip, and the absolute maximum shear strain ymax at
the point. Show the angle 8, (counterclockwise is positive, clockwise is negative), the principal strain deformations, and the maximum
in-plane shear strain distortion in a sketch.
Answers:
Ep1 =
Ep2 =
Yip =
Vmax =
Op=
0
με.
με.
urad.
urad.
Transcribed Image Text:The strain components for a point in a body subjected to plane strain are &x = 530 μe, &y=810μe and Yxy = -956 urad. Using Mohr's circle, determine the principal strains (Ep1 > Ep2), the maximum inplane shear strain Yip, and the absolute maximum shear strain ymax at the point. Show the angle 8, (counterclockwise is positive, clockwise is negative), the principal strain deformations, and the maximum in-plane shear strain distortion in a sketch. Answers: Ep1 = Ep2 = Yip = Vmax = Op= 0 με. με. urad. urad.
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