Aerospace Engineering > GATE 2022 > Combined Loading
A 0.5 m long thin-walled circular shaft of radius 2 cm is to be designed for an axial load of 7.4 kN and a torque of 148 Nm applied at its tip, as shown in the figure. The allowable stress under uniaxial tension is 100 MPa.
Using the maximum principal stress criterion, the minimum thickness, t, of the shaft so that it does not fail is _______ mm. (rounded off to the nearest integer)

Correct : 1 to 1

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Related Topics

Aerospace Engineering GATE 2022 GATE AE 2022 Q59 thin-walled circular shaft maximum principal stress criterion axial load torque shaft minimum thickness calculation shaft design stress failure criteria aerospace

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