The strain components for a point in a body subjected to plane strain are Ex - 930 JE, Ey - -112Que and Wxy - -583 urad. Using Mohr's circle. determine the principal strains (6p1 > p2), the maximum inplane shear strain yip, and the absolute maximum shear strain Ymax at the point. Show the angle , (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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Author:KASSIMALI, Aslam.
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Chapter2: Loads On Structures
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The strain components for a point in a body subjected to plane strain are Ex - 930 JE, Ey - -112Que and Wxy - -583 urad. Using Mohr's
circle. determine the principal strains (6p1 > p2), the maximum inplane shear strain yip, and the absolute maximum shear strain Ymax at
the point. Show the angle , (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 ɛx = 930 pɛ, ɛ, = -1120µe and yy = -583 prad. 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 0, (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 =
prad.
Ymax =
prad.
Transcribed Image Text:The strain components for a point in a body subjected to plane strain are ɛx = 930 pɛ, ɛ, = -1120µe and yy = -583 prad. 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 0, (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 = prad. Ymax = prad.
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