This paper considers the problem of determining stresses and deformations in elastic thin-walled, prismatical beams, subject to axial end forces and end bending and twisting moments, within the range of applicability of linear theory. The analysis, which generalizes recent work on the problem of torsion [1], is based on the differential equations of equilibrium and compatibility of thin shells in the form given by Gunther [2], together with constitutive equations given by the first-named author [3]. The technically most significant aspect of the work has to do with the analysis of the effect of anisotropy of the material, which is associated with previously not determined modes of coupling between stretching, bending, and twisting. Use of the general formulas of the theory is illustrated for a class of shells consisting of an “ordinary” material (unable to support stress moments with axes normal to the middle surface of the shell, and unable to undergo transverse shear deformation). Here explicit formulas are obtained for certain types of open as well as of closed-cross-section beams.
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March 1972
Research Papers
Pure Bending, Stretching, and Twisting of Anisotropic Cylindrical Shells
E. Reissner,
E. Reissner
University of California at San Diego, La Jolla, Calif.
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W. T. Tsai
W. T. Tsai
University of California at San Diego, La Jolla, Calif.
Search for other works by this author on:
E. Reissner
University of California at San Diego, La Jolla, Calif.
W. T. Tsai
University of California at San Diego, La Jolla, Calif.
J. Appl. Mech. Mar 1972, 39(1): 148-154 (7 pages)
Published Online: March 1, 1972
Article history
Received:
November 20, 1970
Online:
July 12, 2010
Citation
Reissner, E., and Tsai, W. T. (March 1, 1972). "Pure Bending, Stretching, and Twisting of Anisotropic Cylindrical Shells." ASME. J. Appl. Mech. March 1972; 39(1): 148–154. https://doi.org/10.1115/1.3422604
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