GATE AE · 2019 · AE
Question 53: Flight Vehicle Structures
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Question 53
AENAT2 marksNeeds review
A thin-walled tube, with the cross-section shown in the figure, is subjected to a torque of
kN-m. The walls have uniform thickness
mm and shear modulus
GPa. Assume that the curved portion is semi-circular. The shear stress in the wall is _____ MPa (round off to 1 decimal place). 
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2019AE
GATE AE 2019 · Paper 1
Aerospace Engineering · Original paper archive
- Section
- Aerospace Engineering
- Question type
- Numerical answer (NAT)
- Marks
- 2 marks
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