A point in a structural member [E = 77 GPa, G = 30 GPa] is subjected to the following stress magnitudes. The stress directions are shown in the image. Determine εy.|σx| = 95 MPa|σy| = 75 MPa|τxy| = 100 MPa

A point in a structural member is subjected to plane strain. Determine the smaller principal strain in the x-y plane.εx = –200 μεεy = –570 μεγxy = –160 μrad

A point in a structural member is subjected to plane strain. Determine εn for an angle magnitude of |θ| = 72° in the direction shown.εx = –590 μεεy = –600 μεγxy = –350 μrad

A point in a structural member is subjected to the following stress magnitudes. The stress directions are shown in the image. Determine σn for an angle magnitude of |θ| = 70° in the direction shown.|σx| = 70 MPa|σy| = 35 MPa|τxy| = 65 MPa

A point in a structural member [E = 110 GPa, G = 43 GPa] is subjected to the following stress magnitudes. The stress directions are shown in the image. Determine εz.|σx| = 45 MPa|σy| = 80 MPa|τxy| = 75 MPa

At a point on the free surface of an aluminum component [E = 68 MPa,ν = 0.34], a strain rosette was used to obtain normal strains of εa = 334 με, εb = –95 με, and εc = 445 με. Determine normal strain εx at the point.

A point in a structural member is subjected to plane strain. Determine the larger principal strain in the x-y plane.εx = –750 μεεy = –850 μεγxy = –400 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| = 15.6 MPa|σy| = 96.1 MPa|τxy| = 40.9 MPa

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

At a point on the free surface of an aluminum component [E = 67 MPa,ν = 0.32], a strain rosette was used to obtain normal strains of εa = 162 με, εb = –235 με, and εc = 220 με. Determine normal strain εx at the point.