A point in a structural member is subjected to plane strain. Determine εn for an angle magnitude of |θ| = 46° in the direction shown.εx = –780 μεεy = –550 μεγxy = –300 μrad

Determine the deflection at B. Let P = 150 lb, a = 70 in., b = 40 in., and EI = 49 × 106 lb·in.2.

A point in a structural member is subjected to the following stress magnitudes. The stress directions are shown in the image. Determine τnt for an angle magnitude of |θ| = 32° in the direction shown.|σx| = 95 MPa|σy| = 30 MPa|τxy| = 100 MPa

At a point on the free surface of an aluminum component [E = 68 MPa,ν = 0.3], a strain rosette was used to obtain normal strains of εa = 142 με, εb = –495 με, and εc = 495 με. Determine normal strain εx at the point.

A point in a structural member [E = 115 GPa, G = 45 GPa] is subjected to the following stress magnitudes. The stress directions are shown in the image. Determine εx.|σx| = 70 MPa|σy| = 85 MPa|τxy| = 30 MPa

A point in a structural member is subjected to the following stress magnitudes. The stress directions are shown in the image. Determine the smaller principal stress in the x-y plane.|σx| = 55 MPa|σy| = 70 MPa|τxy| = 30 MPa

A point in a structural member is subjected to plane strain. Determine the center εcenter of the corresponding in-plane Mohr’s circle.εx = –810 μεεy = –580 μεγxy = –710 μrad

A point in a structural member is subjected to plane strain. Determine the absolute maximum shear strain.εx = –650 μεεy = –610 μεγxy = –290 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| = 97.2 MPa|σy| = 81.2 MPa|τxy| = 57.1 MPa

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