Determine the maximum in-plane shear stress developed at point A on the cross section of the arm at section a-a. Point A is located on the web of the I beam, immediately below the flange. Please use the shear formula when calculating the shear stress, T. (See chapter 7 of the textbook if you're unsure). The question is asking for the maximum in-plane shear stress, you can use Mohr's circle to determine this, once you have calculated the stresses at Point A.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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Determine the maximum in-plane shear stress developed at point A on the cross
section of the arm at section a-a. Point A is located on the web of the I beam,
immediately below the flange. Please use the shear formula when calculating the
shear stress, T. (See chapter 7 of the textbook if you're unsure). The question is
asking for the maximum in-plane shear stress, you can use Mohr's circle to determine
this, once you have calculated the stresses at Point A.
F
B
k
b/3
b/3
L/4
a
a
*
A
b/3
L/4
3b
kb ➜
Section a-a
30°
The length if the arm, L, is 620.0 mm.
The applied force, P, is 600 N.
The width of the section a-a, b, is 20mm.
C
L/2
P
Transcribed Image Text:Determine the maximum in-plane shear stress developed at point A on the cross section of the arm at section a-a. Point A is located on the web of the I beam, immediately below the flange. Please use the shear formula when calculating the shear stress, T. (See chapter 7 of the textbook if you're unsure). The question is asking for the maximum in-plane shear stress, you can use Mohr's circle to determine this, once you have calculated the stresses at Point A. F B k b/3 b/3 L/4 a a * A b/3 L/4 3b kb ➜ Section a-a 30° The length if the arm, L, is 620.0 mm. The applied force, P, is 600 N. The width of the section a-a, b, is 20mm. C L/2 P
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