The strain components for a point in a body subjected to plane strain are ɛ, = 820 µE, Ey = -360µE and yy = 804 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 e, (counterclockwise is positive, clockwise is negative), the principal strain deformations, and the maximum in-plane shear strain distortion in a sketch. Answers: Ep1 = 942.81 με Ep2 = -482.82 με. Vip = 1180 prad. Ymax = 1427.87 prad. ep- 9.406

Structural Analysis
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Chapter2: Loads On Structures
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Your answer is partially correct.
The strain components for a point in a body subjected to plane strain are ɛx = 820 µɛ, ɛ, = -360µɛ and yYxy = 804 prad. Using
Mohr's circle, determine the principal strains (€p1 > Ep2), the maximum inplane shear strain yip, and the absolute maximum shear
strain ymax at the point. Show the angle 0, (counterclockwise is positive, clockwise is negative), the principal strain deformations,
and the maximum in-plane shear strain distortion in a sketch.
Answers:
Ep1 =
942.81
με.
Ep2 =
-482.82
με.
Yip =
1180
prad.
Ymax =
1427.87
prad.
6,- 9.406
Transcribed Image Text:Your answer is partially correct. The strain components for a point in a body subjected to plane strain are ɛx = 820 µɛ, ɛ, = -360µɛ and yYxy = 804 prad. Using Mohr's circle, determine the principal strains (€p1 > Ep2), the maximum inplane shear strain yip, and the absolute maximum shear strain ymax at the point. Show the angle 0, (counterclockwise is positive, clockwise is negative), the principal strain deformations, and the maximum in-plane shear strain distortion in a sketch. Answers: Ep1 = 942.81 με. Ep2 = -482.82 με. Yip = 1180 prad. Ymax = 1427.87 prad. 6,- 9.406
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