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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 PI0. Use this information to answer questions 10 to 13. 750 min 750 mi SAN 500 mm Figure P10

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

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
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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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