A variational method involving Lekhnitskii’s stress functions is used to determine the interlaminar stresses in a multilayered strip of laminate subjected to arbitrary combinations of axial extension, bending, and twisting loads. The stress functions in each layer are approximated by polynomial functions of the thickness coordinate. The equilibrium equations, the traction-free boundary conditions, and the continuity conditions of the interlaminar stresses are exactly satisfied in the present analysis, while the compatibility equations and the continuity of the displacements across the interfaces are enforced in an averaged sense by applying the principle of complementary virtual work. This yields an eigenvalue problem for the interfacial values of the stress functions and their normal derivatives. Interlaminar stresses for all three distinct loading cases may be obtained, in a single solution process, by combining the eigenfunctions with appropriate particular solutions (peculiar to each loading case) so as to ensure satisfaction of the traction-free boundary condition at the free edge.
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June 1994
Research Papers
Free-Edge Effects in Anisotropic Laminates Under Extension, Bending and Twisting, Part I: A Stress-Function-Based Variational Approach
W.-L. Yin
W.-L. Yin
School of Civil Engineering, Georgia Institute of Technology, Atlanta, GA 30332
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W.-L. Yin
School of Civil Engineering, Georgia Institute of Technology, Atlanta, GA 30332
J. Appl. Mech. Jun 1994, 61(2): 410-415 (6 pages)
Published Online: June 1, 1994
Article history
Received:
October 16, 1992
Revised:
April 14, 1993
Online:
March 31, 2008
Citation
Yin, W. (June 1, 1994). "Free-Edge Effects in Anisotropic Laminates Under Extension, Bending and Twisting, Part I: A Stress-Function-Based Variational Approach." ASME. J. Appl. Mech. June 1994; 61(2): 410–415. https://doi.org/10.1115/1.2901459
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