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>

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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Concept explainers

Stress transformation

The term stress indicates the measure of internal forces that develop due to an external force's application on an object. When a specific external force is applied to an object, internal stress generates in the material. The value of stress can obtain by taking the ratio of the externally applied force and cross-sectional area of the object. There are different types of stress depending on the type of external force.

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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, and
transverse shear stress vectors for the Points A through F.
У м
D = 100 mm
0 = 30°
F = (10000,
M = (8000,
For additional practice, vary force and moment vectors
Point
A
B
C
D
F
25000,
35000) N
7500, 11000) N - m
Axial 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>
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>
F
B
E
N
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>

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