Already have the answers filled in. I would just like to know how to arrive at those correct answers. Thank you. Using the Givens and Figure below, calculate the axial stresses, bending stress vectors, torsional shear stresses, andtransverse shear stress vectors for the Points A through F.У мD = 100 mm0 = 30°F = (10000,M = (8000,For additional practice, vary force and moment vectorsPointABCDF25000,35000) N7500, 11000) N - mAxial Stress[MPa](Ox, Oy, Oz)<0.0, 3.18, 0.0><0.0, 3.18, 0.0><0.0, 3.18, 0.0><0.0, 3.18, 0.0><0.0, 3.18, 0.0><0.0, 3.18, 0.0>Bending Stress(0x, Oy, 0₂)<0.0, 81.49, 0.0><0.0, -112.05, 0.0><0.0, -81.49, 0.0><0.0, 112.05, 0.0><0.0, 0.0, 0.0><0.0, 137.78, 0.0>TorsionalShear Stress(Txy, Txz, Tyz)<-38.2, 0.0, 0.0><0.0, 0.0, 38.2><38.2, 0.0, 0.0><0.0, 0.0, -38.2><0.0, 0.0, 0.0><-19.1, 0.0, -33.08>XTransverseShear Stress(Txy, Txz, Tyz)<1.7, 0.0, 0.0><0.0, 0.0, 5.94><1.7, 0.0, 0.0><0.0, 0.0, 5.94><0.85, 0.0, 2.97><0.42, 0.0, 4.46>FBENr0FDXTotal Stress(Ox, Oy, Oz, Txy, Txz, Tyz)<0.0, 84.67, 0.0, -36.5, 0.0, 0.0><0.0, -108.86, 0.0, 0.0, 0.0, 44.14><0.0, -78.3, 0.0, 39.89, 0.0, 0.0><0.0, 115.23, 0.0, 0.0, 0.0, -32.26><0.0, 3.18, 0.0, 0.85, 0.0, 2.97><0.0, 140.96, 0.0, -18.67, 0.0, -28.62>

Answered: Image /qna-images/answer/0df0314c-e1e3-4d9d-9252-dc519aabcf42.jpg

Using the Givens and Figure below, calculate the axial stresses, bending stress vectors, torsional shear stresses, and transverse shear stress vectors for the Points A through F. y M F D = 100 mm 0 = 30° F = (10000, M = (8000, For additional practice, vary force and moment vectors Point A B C Ꭰ E F 25000, 35000) N 7500, 11000) N - m Axial Stress [MPa] (0x, Oy, 0₂) <0.0, 3.18, 0.0> <0.0, 3.18, 0.0> <0.0, 3.18, 0.0> <0.0, 3.18, 0.0> <0.0, 3.18, 0.0> <0.0, 3.18, 0.0> Bending Stress (Ox, Oy, Oz) <0.0, 81.49, 0.0> <0.0, -112.05, 0.0> <0.0, -81.49, 0.0> <0.0, 112.05, 0.0> <0.0, 0.0, 0.0> <0.0, 137.78, 0.0> Torsional Shear Stress (Txy, Txz, Tyz) <-38.2, 0.0, 0.0> <0.0, 0.0, 38.2> <38.2, 0.0, 0.0> <0.0, 0.0, -38.2> <0.0, 0.0, 0.0> <-19.1, 0.0, -33.08> X Transverse Shear Stress (Txy, Txz, Tyz) <1.7, 0.0, 0.0> <0.0, 0.0, 5.94> <1.7, 0.0, 0.0> <0.0, 0.0, 5.94> <0.85, 0.0, 2.97> <0.42, 0.0, 4.46> B E C Z r 0 F D X Total Stress (Ox, Oy, Oz, Txy, Txz, Tyz) <0.0, 84.67, 0.0, -36.5, 0.0, 0.0> <0.0, -108.86, 0.0, 0.0, 0.0, 44.14> <0.0, -78.3, 0.0, 39.89, 0.0, 0.0> <0.0, 115.23, 0.0, 0.0, 0.0, -32.26> <0.0, 3.18, 0.0, 0.85, 0.0, 2.97> <0.0, 140.96, 0.0, -18.67, 0.0, -28.62>

Using the Givens and Figure below, calculate the axial stresses, bending stress vectors, torsional shear stresses, and transverse shear stress vectors for the Points A through F. y M F D = 100 mm 0 = 30° F = (10000, M = (8000, For additional practice, vary force and moment vectors Point A B C Ꭰ E F 25000, 35000) N 7500, 11000) N - m Axial Stress [MPa] (0x, Oy, 0₂) <0.0, 3.18, 0.0> <0.0, 3.18, 0.0> <0.0, 3.18, 0.0> <0.0, 3.18, 0.0> <0.0, 3.18, 0.0> <0.0, 3.18, 0.0> Bending Stress (Ox, Oy, Oz) <0.0, 81.49, 0.0> <0.0, -112.05, 0.0> <0.0, -81.49, 0.0> <0.0, 112.05, 0.0> <0.0, 0.0, 0.0> <0.0, 137.78, 0.0> Torsional Shear Stress (Txy, Txz, Tyz) <-38.2, 0.0, 0.0> <0.0, 0.0, 38.2> <38.2, 0.0, 0.0> <0.0, 0.0, -38.2> <0.0, 0.0, 0.0> <-19.1, 0.0, -33.08> X Transverse Shear Stress (Txy, Txz, Tyz) <1.7, 0.0, 0.0> <0.0, 0.0, 5.94> <1.7, 0.0, 0.0> <0.0, 0.0, 5.94> <0.85, 0.0, 2.97> <0.42, 0.0, 4.46> B E C Z r 0 F D X Total Stress (Ox, Oy, Oz, Txy, Txz, Tyz) <0.0, 84.67, 0.0, -36.5, 0.0, 0.0> <0.0, -108.86, 0.0, 0.0, 0.0, 44.14> <0.0, -78.3, 0.0, 39.89, 0.0, 0.0> <0.0, 115.23, 0.0, 0.0, 0.0, -32.26> <0.0, 3.18, 0.0, 0.85, 0.0, 2.97> <0.0, 140.96, 0.0, -18.67, 0.0, -28.62>

Mechanics of Materials (MindTap Course List)

9th Edition

ISBN:9781337093347

Author:Barry J. Goodno, James M. Gere

Publisher:Barry J. Goodno, James M. Gere

Chapter7: Analysis Of Stress And Strain

Section: Chapter Questions

Problem 7.7.19P: During a test of an airplane wing, the strain gage readings from a 45° rosette (see figure) are as...

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