The strain components for a point in a body subjected to plane strain are εx = 620 με, εy = -1030με and γxy = 320 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

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The strain components for a point in a body subjected to plane strain are εx = 620 με, εy = -1030με and γxy = 320 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 = 620 με, &y=-1030μe and Yxy = 320 μrad. Using Mohr's
circle, determine the principal strains (Ɛp1 > Ɛp2), the maximum inplane shear strain Yip, and the absolute maximum shear strain Ymax at
the point. Show the angle 8p (counterclockwise is positive, clockwise is negative), the principal strain deformations, and the maximum
in-plane shear strain distortion in a sketch.
Answers:
Ep1 =
με.
Ep2 =
με.
Yip =
urad.
Ymax =
Op=
0
urad.
Transcribed Image Text:The strain components for a point in a body subjected to plane strain are &x = 620 με, &y=-1030μe and Yxy = 320 μrad. Using Mohr's circle, determine the principal strains (Ɛp1 > Ɛp2), the maximum inplane shear strain Yip, and the absolute maximum shear strain Ymax at the point. Show the angle 8p (counterclockwise is positive, clockwise is negative), the principal strain deformations, and the maximum in-plane shear strain distortion in a sketch. Answers: Ep1 = με. Ep2 = με. Yip = urad. Ymax = Op= 0 urad.
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