The strain components ɛx, Ɛy, and yxy are given for a point in a body subjected to plane strain. Using Mohr's circle, determine the principal strains, the maximum in-plane shear strain, and the absolute maximum shear strain at the point. Show the angle 0p, the principal strain deformations, and the maximum in-plane shear strain distortion in a sketch. Ex = 320 µɛ, ɛy = -910 µɛ, Yxy = -580 µrad. Enter the angle such that -45°s0,s +45°.

Structural Analysis
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ISBN:9781337630931
Author:KASSIMALI, Aslam.
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Chapter2: Loads On Structures
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Your answer is partially correct.
The strain components ɛx, ɛy, and yxy are given for a point
in a body subjected to plane strain. Using Mohr's circle,
determine the principal strains, the maximum in-plane
shear strain, and the absolute maximum shear strain at
the point. Show the angle 0p, the principal strain
deformations, and the maximum in-plane shear strain
distortion in a sketch.
εx-320 με, εy = -910 με, Υν -580 μrad. Enter the angle
such that -45°se,< +45°.
%3D
Answer:
Ep1 =
384.95
Ep2
-974.95
%|
Ymax in-plane
prad
-295
Yabsolute max.
1359.9
prad
12.62
Transcribed Image Text:Your answer is partially correct. The strain components ɛx, ɛy, and yxy are given for a point in a body subjected to plane strain. Using Mohr's circle, determine the principal strains, the maximum in-plane shear strain, and the absolute maximum shear strain at the point. Show the angle 0p, the principal strain deformations, and the maximum in-plane shear strain distortion in a sketch. εx-320 με, εy = -910 με, Υν -580 μrad. Enter the angle such that -45°se,< +45°. %3D Answer: Ep1 = 384.95 Ep2 -974.95 %| Ymax in-plane prad -295 Yabsolute max. 1359.9 prad 12.62
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