
The state of strain at the point on the arm has components of εx = 200 (10−6), εy = −300 (10−6), and γxy = 400(10−6). Use the strain transformation equations to determine the equivalent in-plane strains on an element oriented at an angle of 30° counterclockwise from the original position, Sketch the deformed element due to these strains within the x–y plane.

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