35 mm10 kN-m2.36 x106 mm70 GPa%3D%3D(1)C240 mm(2)4.02 x106 mm%3DB2800 mm45 GPaC3600 mmA composite torsion member consists of two solidshafts joined at flange B. Shafts (1) and (2) areattached to rigid supports at A and C, respectively.T1kN-mA concentrated torque T is applied to flange B in theT2kN-mdirection shown. Determine the internal torques andMPаshear stresses in each shaft. Also, determine therotation angle of flange B.MPa((Use the sign convention detailed in the fourthscene of this movie for internal torques and rotationangles.)PBrad1st2nd3rdEnterShaft propertiesI| ||||

GIVEN DATA- A COMPOSITE SHAFT GIVEN C1=35mm J1=2.36*10^6 mm^4 G1=70GPa C2=40mm J2=4.02*10^6 mm^4…

35 mm 10 kN-m 2.36 x10° mm* G1 = 70 GPa (1) 40 mm C2 = (2) 4.02 x106 mm B 45 GPa 2800 mm 3600 mm A composite torsion member consists of two solid shafts joined at flange B. Shafts (1) and (2) are kN-m T1 attached to rigid supports at A and C, respectively. kN-m A concentrated torque T is applied to flange B in the direction shown. Determine the internal torques and shear stresses in each shaft. Also, determine the rotation angle of flange B. T2 MPa MPa ((Use the sign convention detailed in the fourth rad scene of this movie for internal torques and rotation angles.) PB I| || || I| |||| Shaft properties

35 mm 10 kN-m 2.36 x10° mm* G1 = 70 GPa (1) 40 mm C2 = (2) 4.02 x106 mm B 45 GPa 2800 mm 3600 mm A composite torsion member consists of two solid shafts joined at flange B. Shafts (1) and (2) are kN-m T1 attached to rigid supports at A and C, respectively. kN-m A concentrated torque T is applied to flange B in the direction shown. Determine the internal torques and shear stresses in each shaft. Also, determine the rotation angle of flange B. T2 MPa MPa ((Use the sign convention detailed in the fourth rad scene of this movie for internal torques and rotation angles.) PB I| || || I| |||| Shaft properties

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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Slope and Deflection

The slope in a deflected beam is described as an angle in radians made by the tangent of the section with the original axis of the beam. The deflection at any point on the axis of the beam is defined as the lateral displacement of the point before and after loading.

Question

35 mm
10 kN-m
2.36 x106 mm
70 GPa
%3D
%3D
(1)
C2
40 mm
(2)
4.02 x106 mm
%3D
B
2800 mm
45 GPa
C
3600 mm
A composite torsion member consists of two solid
shafts joined at flange B. Shafts (1) and (2) are
attached to rigid supports at A and C, respectively.
T1
kN-m
A concentrated torque T is applied to flange B in the
T2
kN-m
direction shown. Determine the internal torques and
MPа
shear stresses in each shaft. Also, determine the
rotation angle of flange B.
MPa
((Use the sign convention detailed in the fourth
scene of this movie for internal torques and rotation
angles.)
PB
rad
1st
2nd
3rd
Enter
Shaft properties
I| ||||

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