Consider a point in a structural member that is subjected to plane stress. Normal and shear stress magnitudes acting on horizo vertical planes at the point are Sx = 26.9 ksi, Sy = 6.8 ksi, and Sxy= 19.0 ksi. (a) Determine the principal stresses and the maximum in-plane shear stress acting at the point. (b) On a piece of paper, show these stresses on an appropriate sketch (e.g., see Figure 12.15 or Figure 12.16). For the sketch, ca 0p, the angle between the x axis and the principal stress orientation. Also, calculate avg, the normal stress on planes of maxim plane shear stress. (c) Compute the absolute maximum shear stress at the point. Answers: (a) Opl = Op2 = (0) Tmax = (b) 0,= Oavg = || Sxy T i i Mi i ¡ ksi ksi ksi 0 ksi ksi

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Consider a point in a structural member that is subjected to plane stress. Normal and shear stress magnitudes acting on horizontal and
vertical planes at the point are Sx = 26.9 ksi, Sy = 6.8 ksi, and Sxy= 19.0 ksi.
(a) Determine the principal stresses and the maximum in-plane shear stress acting at the point.
(b) On a piece of paper, show these stresses on an appropriate sketch (e.g., see Figure 12.15 or Figure 12.16). For the sketch, calculate
0p, the angle between the x axis and the principal stress orientation. Also, calculate avg, the normal stress on planes of maximum in-
plane shear stress.
(c) Compute the absolute maximum shear stress at the point.
Answers:
(a) Opl =
Op2 =
Tmax =
(b) 0,=
Oavg
=
(c) Tabs max
Sxy
=
i
i
Mi
i
i
ksi
ksi
ksi
0
ksi
ksi
Transcribed Image Text:Consider a point in a structural member that is subjected to plane stress. Normal and shear stress magnitudes acting on horizontal and vertical planes at the point are Sx = 26.9 ksi, Sy = 6.8 ksi, and Sxy= 19.0 ksi. (a) Determine the principal stresses and the maximum in-plane shear stress acting at the point. (b) On a piece of paper, show these stresses on an appropriate sketch (e.g., see Figure 12.15 or Figure 12.16). For the sketch, calculate 0p, the angle between the x axis and the principal stress orientation. Also, calculate avg, the normal stress on planes of maximum in- plane shear stress. (c) Compute the absolute maximum shear stress at the point. Answers: (a) Opl = Op2 = Tmax = (b) 0,= Oavg = (c) Tabs max Sxy = i i Mi i i ksi ksi ksi 0 ksi ksi
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