The strain components εx, εy, and γxy are given for a point in a body subjected to plane strain. 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 on a sketch. εx = -700 με, εy = -335 με, and γxy = 1100 μrad. Enter the angle such that -45°≤θp≤ +45°.

Structural Analysis
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Author:KASSIMALI, Aslam.
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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. 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 on a sketch. εx = -700 με, εy = -335 με, and γxy = 1100 μrad. Enter the angle such that -45°≤θp≤ +45°.
The strain components Ex, Ey, and Yxy are given
for a point in a body subjected to plane strain.
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
on a sketch. Ex = -700 µe, y = -335 μe, and Yxy =
1100 μrad. Enter the angle such that -45°≤0p<
+45°.
Ep1 =
με
Ep2 =
με
Ymax in-plane
Yabsolute max.
0p=
=
urad
urad
Transcribed Image Text:The strain components Ex, Ey, and Yxy are given for a point in a body subjected to plane strain. 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 on a sketch. Ex = -700 µe, y = -335 μe, and Yxy = 1100 μrad. Enter the angle such that -45°≤0p< +45°. Ep1 = με Ep2 = με Ymax in-plane Yabsolute max. 0p= = urad urad
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