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The 1 inch diameter rod is subjected to the loads shown below. Determine the state of stress at point "A" and show the results on a differential volume element at point "A". Also, determine the principle stresses (0₁, 02, and 03) at point "A", the absolute maximum normal stress (Abs max) in the material at point "A", and the absolute maximum shear stress (TAbs max) in the material at point "A". (Assume the stress caused by atmospheric (air) pressure is negligible.)

The 1 inch diameter rod is subjected to the loads shown below. Determine the state of stress at point "A" and show the results on a differential volume element at point "A". Also, determine the principle stresses (0₁, 02, and 03) at point "A", the absolute maximum normal stress (Abs max) in the material at point "A", and the absolute maximum shear stress (TAbs max) in the material at point "A". (Assume the stress caused by atmospheric (air) pressure is negligible.)

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 1 inch diameter rod is subjected to the loads shown below. Determine the state of stress at point "A" and show the results on a differential volume element at point "A". Also, determine the principle stresses (01, 02, and 03) at point "A", the absolute maximum normal stress (Abs max) in the material at point "A", and the absolute maximum shear stress (TAbs max) in the material at point "A". (Assume the stress caused by atmospheric (air) pressure is negligible.) 3 in. 80 lb 75 lb 100 lb B 8 in. Ans. 6895 psi TAbs Max A = 3588 psi Abs Max A =
Transcribed Image Text:The 1 inch diameter rod is subjected to the loads shown below. Determine the state of stress at point "A" and show the results on a differential volume element at point "A". Also, determine the principle stresses (01, 02, and 03) at point "A", the absolute maximum normal stress (Abs max) in the material at point "A", and the absolute maximum shear stress (TAbs max) in the material at point "A". (Assume the stress caused by atmospheric (air) pressure is negligible.) 3 in. 80 lb 75 lb 100 lb B 8 in. Ans. 6895 psi TAbs Max A = 3588 psi Abs Max A =
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