The strain components ɛ, Ey, and yy 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 absolutemaximum shear strain at the point. Show the angle 6, the principal strain deformations, and the maximum in-plane shear strain distortion in a sketch. Ex = 500 µE, ɛ, = -550 µE, Yxy =-840 urad. Enter the angle such that -45°58,5 +45°. Answer: Ep1= Ep2= Ymax in-plane= prad Yabsolute max. prad O, =

Structural Analysis
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Chapter2: Loads On Structures
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The strain components ɛ,, Ey, and yy are given for a point in a body subjected to plane strain. Using Mohr's cirdle, determine the
principal strains, the maximum in-plane shear strain, and the absolutemaximum shear strain at the point. Show the angle 6, the
principal strain deformations, and the maximum in-plane shear strain distortion in a sketch.
Ex = 500 µE, ɛ, = -550 µE, Yxy = -840 urad. Enter the angle such that -45°58,5 +45°.
Answer:
Ep1=
Ep2=
Ymax in-plane=
prad
Yabsolute max.
prad
6, =
Transcribed Image Text:The strain components ɛ,, Ey, and yy are given for a point in a body subjected to plane strain. Using Mohr's cirdle, determine the principal strains, the maximum in-plane shear strain, and the absolutemaximum shear strain at the point. Show the angle 6, the principal strain deformations, and the maximum in-plane shear strain distortion in a sketch. Ex = 500 µE, ɛ, = -550 µE, Yxy = -840 urad. Enter the angle such that -45°58,5 +45°. Answer: Ep1= Ep2= Ymax in-plane= prad Yabsolute max. prad 6, =
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