The complex air tank AB has an inner diameter of 450 mm and a uniform wall thickness of 6-mm and the gage pressure in the tank is 1.2 MPa as shown in Figure PI0. Use this information to answer questions 10 to 13. 750 min 750 mi SAN 500 mm Figure P10

International Edition---engineering Mechanics: Statics, 4th Edition
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Author:Andrew Pytel And Jaan Kiusalaas
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Chapter8: Centroids And Distributed Loads
Section: Chapter Questions
Problem 8.122P: The 12-ft wide quarter-circular gate AB is hinged at A. Determine the contact force between the gate...
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The complex air tank AB has an inner diameter
of 450 mm and a uniform wall thickness of 6-mm
and the gage pressure in the tank is 1.2 MPa as
shown in Figure P10. Use this information to
answer questions 10 to 13.
750 mm
750 mm
D
5 KN
500 mm
Figure P10
Transcribed Image Text:The complex air tank AB has an inner diameter of 450 mm and a uniform wall thickness of 6-mm and the gage pressure in the tank is 1.2 MPa as shown in Figure P10. Use this information to answer questions 10 to 13. 750 mm 750 mm D 5 KN 500 mm Figure P10
ME 255 STRENGTH OF MATERIAL I
10. Determine the stress due to bending at point
a on the top of the tank.
(a) 22.50MPA
(c) 45.0MPA
(b) 3.88MPA
(d) 7.75MPA
11. Determine the stress due to bending at point
b on the top of the tank.
(a) 22.50MPA
(c) 45.0MPA
(b) 3.88MPа
(d) 7.75MPA
12. Determine the tangential stress due to
pressure at points a and b on the top of the
tank.
(a) 22.50MPA
(c) 45.0MPA
(b) 3.88MPа
(d) 7.75MPA
13. Determine the axial stress due to pressure at
points a and b on the top of the tank.
(а) 22.50MPа
(c) 45.0MPA
(b) 3.88MPа
(d) 7.75MPA
Transcribed Image Text:ME 255 STRENGTH OF MATERIAL I 10. Determine the stress due to bending at point a on the top of the tank. (a) 22.50MPA (c) 45.0MPA (b) 3.88MPA (d) 7.75MPA 11. Determine the stress due to bending at point b on the top of the tank. (a) 22.50MPA (c) 45.0MPA (b) 3.88MPа (d) 7.75MPA 12. Determine the tangential stress due to pressure at points a and b on the top of the tank. (a) 22.50MPA (c) 45.0MPA (b) 3.88MPа (d) 7.75MPA 13. Determine the axial stress due to pressure at points a and b on the top of the tank. (а) 22.50MPа (c) 45.0MPA (b) 3.88MPа (d) 7.75MPA
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