The strain components for a point in a body subjected to plane strain are εx = -940 με, εy = -450με and γxy = 865 μrad. Using Mohr’s circle, determine the principal strains (εp1 > εp2), the maximum inplane shear strain γip, and the absolute maximum shear strain γmax at the point. Show the angle θp (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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Chapter2: Loads On Structures
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The strain components for a point in a body subjected to plane strain are εx = -940 με, εy = -450με and γxy = 865 μrad. Using Mohr’s circle, determine the principal strains (εp1 > εp2), the maximum inplane shear strain γip, and the absolute maximum shear strain γmax at the point. Show the angle θp (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 = -940 µɛ, ɛy = -450µe and yxy = 865 µrad. Using Mohr's
circle, determine the principal strains (ɛp1 > 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.
HE,
%3D
Answers:
Ep1=
με.
%3D
Ep2 =
HE.
Vip =
prad.
%3D
Ymax
prad.
Op =
Transcribed Image Text:The strain components for a point in a body subjected to plane strain are ɛx = -940 µɛ, ɛy = -450µe and yxy = 865 µrad. Using Mohr's circle, determine the principal strains (ɛp1 > 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. HE, %3D Answers: Ep1= με. %3D Ep2 = HE. Vip = prad. %3D Ymax prad. Op =
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