A shaft composed of segments AC, CD, and DB is fastened to rigid supports and loaded as shown below. For bronze, aluminum, and steel the G, modulus of rigidity are 35 GPa, 28 GPA, and 83 GPa respectively. Determine the maximum shearing stress (in MPa) developed in each segment. Hint: EOIB =0 rotation of Brelative to AL0B =0 rotation of B relative to A Tools: J = D* T = D³t TL .. derive t JG 16 Hint: = 0 rotation of B relative to A T. = 500 N-m Tp = 800 N-m C Aluminum A Bronze Steel 25 mm 25 mm o 50 mm 2 m 2 m 2.5 m

Mechanics of Materials (MindTap Course List)
9th Edition
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Barry J. Goodno, James M. Gere
Chapter8: Applications Of Plane Stress (pressure Vessels, Beams, And Combined Loadings)
Section: Chapter Questions
Problem 8.3.10P: Solve the preceding problem if F =90 mm, F = 42 kN, and t = 40°MPa
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A shaft composed of segments AC, CD, and DB is fastened to rigid supports and loaded as shown
below. For bronze, aluminum, and steel the G, modulus of rigidity are 35 GPa, 28 GPA, and 83 GPa
respectively. Determine the maximum shearing stress (in MPa) developed in each segment. Hint:
= 0 rotation of B relative to A£ 0A13 = 0 rotation of B relative to A
Tools:
TL
J = "D4
D³ t ... derive t
16
T =
JG
32
Hint: E0AIR = 0 rotation of B relative to A
Tc = 500 N-m
Aluminum D
Tp = 800 N-m
C
A Bronze
Steel
TA
TB
25 mm
25 mm o
50 mm o
2 m
2 m
2.5 m
Transcribed Image Text:A shaft composed of segments AC, CD, and DB is fastened to rigid supports and loaded as shown below. For bronze, aluminum, and steel the G, modulus of rigidity are 35 GPa, 28 GPA, and 83 GPa respectively. Determine the maximum shearing stress (in MPa) developed in each segment. Hint: = 0 rotation of B relative to A£ 0A13 = 0 rotation of B relative to A Tools: TL J = "D4 D³ t ... derive t 16 T = JG 32 Hint: E0AIR = 0 rotation of B relative to A Tc = 500 N-m Aluminum D Tp = 800 N-m C A Bronze Steel TA TB 25 mm 25 mm o 50 mm o 2 m 2 m 2.5 m
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