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)
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)

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