A plane element removed from a thin-walled cylindrical shell loaded in torsion is subject to the shearing stresses shown in Fig. 3-20. Determine the principal stresses existing in this element and the directions of the planes on which they occur. Ans. 50 MPa at 45° 50 MPa 50 MPa 50 MPa 50 MPa

A plane element removed from a thin-walled cylindrical shell loaded in torsion is subject to the shearing stresses shown in Fig. 3-20. Determine the principal stresses existing in this element and the directions of the planes on which they occur. Ans. 50 MPa at 45° 50 MPa 50 MPa 50 MPa 50 MPa

Structural Analysis

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Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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Question

A plane element removed from a thin-walled cylindrical shell loaded in torsion is subject to the shearing stresses
shown in Fig. 3-20. Determine the principal stresses existing in this element and the directions of the planes on
which they occur.
Ans. 50 MPa at 45°
50 MPa
50 MPa
50 MPa
50 MPa

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