4. The state of strain at a point on the clamp has components of Yay=-500(106), &y=+500(106), and &x=-600(106). Use the strain transformation equations to determine a) The in-plane principal strains and the angle of orientation where they occur; b) The maximum in-plane shear strain, average normal strain, and the angle of orientation where they occur; Sketch the deformed element and show strain values due to a) and b). C
4. The state of strain at a point on the clamp has components of Yay=-500(106), &y=+500(106), and &x=-600(106). Use the strain transformation equations to determine a) The in-plane principal strains and the angle of orientation where they occur; b) The maximum in-plane shear strain, average normal strain, and the angle of orientation where they occur; Sketch the deformed element and show strain values due to a) and b). C
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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Transcribed Image Text:4.
The state of strain at a point on the clamp has components of Yxy=-500(10), &y=+500(106), and
&x=-600(106). Use the strain transformation equations to determine
The in-plane principal strains and the angle of orientation where they occur;
The maximum in-plane shear strain, average normal strain, and the angle of orientation
where they occur;
Sketch the deformed element and show strain values due to a) and b).
a)
b)
G
X
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