The strain components εx, εy, and γxy 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 θp, the principal strain deformations, and the maximum in-plane shear strain distortion in a sketch. εx = 360 με, εy = -1000 με, γxy = -630 μrad. Enter the angle such that -45°≤θp≤ +45°.

Structural Analysis
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Chapter2: Loads On Structures
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The strain components εx, εy, and γxy 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 θp, the principal strain deformations, and the maximum in-plane shear strain distortion in a sketch.
εx = 360 με, εy = -1000 με, γxy = -630 μrad. Enter the angle such that -45°≤θp≤ +45°.

The strain components ɛx, Ɛy, and y,xy 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 = 360 µɛ, ɛy = -1000 µɛ, Yxy = -630 µrad. Enter the angle such that -45°<0,s +45°.
Answer:
Ep1 =
Ep2 =
Ymax in-plane
prad
Yabsolute max.
prad
%3D
Transcribed Image Text:The strain components ɛx, Ɛy, and y,xy 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 = 360 µɛ, ɛy = -1000 µɛ, Yxy = -630 µrad. Enter the angle such that -45°<0,s +45°. Answer: Ep1 = Ep2 = Ymax in-plane prad Yabsolute max. prad %3D
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