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A point in a structural member is subjected to the following stress magnitudes. The stress directions are shown in the image. Determine the absolute maximum shear stress.|σx| = 100 MPa|σy| = 70 MPa|τxy| = 25 MPa

A point in a structural member is subjected to plane strain. Determine the larger principal strain in the x-y plane.εx = –870 μεεy = –830 μεγxy = –50 μrad

At a point on the free surface of an aluminum component [E = 73 MPa,ν = 0.3], a strain rosette was used to obtain normal strains of εa = 84 με, εb = –250 με, and εc = 490 με. Determine normal strain εx at the point.

A point in a structural member [E = 138 GPa, G = 54 GPa] is subjected to the following stress magnitudes. The stress directions are shown in the image. Determine εz.|σx| = 10 MPa|σy| = 55 MPa|τxy| = 95 MPa

A point in a structural member is subjected to plane strain. Determine εt for an angle magnitude of |θ| = 38° in the direction shown.εx = 900 μεεy = 690 μεγxy = 120 μrad

A point in a structural member is subjected to plane strain. Determine the smaller principal strain in the x-y plane.εx = –730 μεεy = –740 μεγxy = –30 μrad

A point in a structural member is subjected to plane strain. Determine the maximum shear strain in the x-y plane.εx = 50 μεεy = 740 μεγxy = 760 μrad

A point in a structural member is subjected to plane strain. Determine the orientation of the principal planes, θp.εx = –70 μεεy = –660 μεγxy = –810 μrad

A point in a structural member is subjected to the following stress magnitudes. The stress directions are shown in the image. Determine the center σcenter of the corresponding in-plane Mohr’s circle.|σx| = 66.2 MPa|σy| = 66.5 MPa|τxy| = 92.4 MPa

A point in a structural member is subjected to plane strain. Determine the absolute maximum shear strain.εx = –890 μεεy = –900 μεγxy = –50 μrad