Prob. 4.4-6. (a) determine the maximum tensile stress, the maximum compressive stress, and the maximum shear stress; and (b) show the stresses determined in Part (a) on properly oriented stress elements (e.g., see Fig. 4.14). In solving these problems, make the sense of the stresses consistent with the sense of the torque T shown on the generic torsion member figure. = T= 400 N m. d. = 40 mm, and d dol 0 32 mm. =relative twist angle d T T 45° (b) FIGURE 4.14 A pure- shear element, and the associ- ated maximum-normal-stress element.
Prob. 4.4-6. (a) determine the maximum tensile stress, the maximum compressive stress, and the maximum shear stress; and (b) show the stresses determined in Part (a) on properly oriented stress elements (e.g., see Fig. 4.14). In solving these problems, make the sense of the stresses consistent with the sense of the torque T shown on the generic torsion member figure. = T= 400 N m. d. = 40 mm, and d dol 0 32 mm. =relative twist angle d T T 45° (b) FIGURE 4.14 A pure- shear element, and the associ- ated maximum-normal-stress element.
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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Please show all steps, given data, what to find, and a free body diagram.
Transcribed Image Text:Prob. 4.4-6.
(a) determine the maximum tensile stress, the
maximum compressive stress, and the maximum shear
stress; and (b) show the stresses determined in Part (a) on
properly oriented stress elements (e.g., see Fig. 4.14).
In solving these problems, make the sense of the
stresses consistent with the sense of the torque T shown
on the generic torsion member figure.
T = 400 Nm, d, 40 mm, and d = 32 mm.
dol
T
FO
=relative
twist angle
di
T
(a)
(b)
FIGURE 4.14 A pure-
shear element, and the associ-
ated maximum-normal-stress
element.
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