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The strain components for a point in a body subjected to plane strain are &x=210 μe, &y=260μe and Yxy=-1009 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 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= 0p- urad.

The strain components for a point in a body subjected to plane strain are &x=210 μe, &y=260μe and Yxy=-1009 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 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= 0p- urad.

Structural Analysis
Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
Section: Chapter Questions
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The strain components for a point in a body subjected to plane strain are &x = 210 μ, y = 260μe and Yxy=-1009 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 0₂ (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= Op- 0 urad.
Transcribed Image Text:The strain components for a point in a body subjected to plane strain are &x = 210 μ, y = 260μe and Yxy=-1009 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 0₂ (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= Op- 0 urad.
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