Equations describing the stress field and velocity field occurring in a circular cylindrical shell at plastic collapse are derived corresponding to stress states lying on each face of a yield surface for a uniform shell of material obeying the Tresca yield condition. They are then applied to the case of a shell under combined axisymmetric loadings (moment, shear force, and axial force) at one end and uniform internal or external pressure on the lateral surface. For a sufficiently long shell, complete solutions are obtained for a fixed far end, and for a certain range of values of axial force and pressure, they are obtained for a free far end. All the solutions are represented by either closed form or by quadratures. It is shown that in many cases the radial velocity field is proportional to the shear force.
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November 1971
This article was originally published in
Journal of Engineering for Industry
Research Papers
Limit Analysis for Combined Edge and Pressure Loading on a Cylindrical Shell
H. S. Ho,
H. S. Ho
University of Southern California, Los Angeles, Calif.
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D. P. Updike
D. P. Updike
Lehigh University, Bethlehem, Pa.
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H. S. Ho
University of Southern California, Los Angeles, Calif.
D. P. Updike
Lehigh University, Bethlehem, Pa.
J. Eng. Ind. Nov 1971, 93(4): 998-1006
Published Online: November 1, 1971
Article history
Received:
February 4, 1971
Online:
July 15, 2010
Citation
Ho, H. S., and Updike, D. P. (November 1, 1971). "Limit Analysis for Combined Edge and Pressure Loading on a Cylindrical Shell." ASME. J. Eng. Ind. November 1971; 93(4): 998–1006. https://doi.org/10.1115/1.3428096
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