Time-dependent interlaminar stresses in elastic and viscoelastic laminated composites subjected to arbitrary combinations of axial extension, bending and/or twisting loads are obtained based on integral constitutive relations and Pipes and Pagano’s displacement field for laminates under a generalized plane deformation state. Numerical results obtained from the present formulation are compared against experimental data and excellent agreement within two percent was obtained between these results. Time-dependent interlaminar stresses for cross-ply and angle-ply laminates subjected to uniaxial extension, bending and twisting are also presented. Appreciable stress relaxation occurred during the loading period resulting in decreased magnitudes of residual stresses. It is seen that the rate of interlaminar shear stress relaxation is greater than the normal one, since the relaxation of shear moduli is larger than that of the normal moduli.
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July 1997
Technical Papers
Free Edge Stresses in Elastic and Viscoelastic Composites Under Uniaxial Extension, Bending, and Twisting Loadings
Sung Yi,
Sung Yi
School of Mechanical and Production Engineering, Nanyang Technological University, Singapore, 639798 Republic of Singapore
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H. H. Hilton
H. H. Hilton
Aeronautical and Astronautical Engineering Department and National Center for Supercomputing Applications, University of Illinois at Urbana-Champaign, Urbana, IL 61801-2935
Search for other works by this author on:
Sung Yi
School of Mechanical and Production Engineering, Nanyang Technological University, Singapore, 639798 Republic of Singapore
H. H. Hilton
Aeronautical and Astronautical Engineering Department and National Center for Supercomputing Applications, University of Illinois at Urbana-Champaign, Urbana, IL 61801-2935
J. Eng. Mater. Technol. Jul 1997, 119(3): 266-272 (7 pages)
Published Online: July 1, 1997
Article history
Received:
December 20, 1996
Revised:
April 15, 1997
Online:
November 27, 2007
Citation
Yi, S., and Hilton, H. H. (July 1, 1997). "Free Edge Stresses in Elastic and Viscoelastic Composites Under Uniaxial Extension, Bending, and Twisting Loadings." ASME. J. Eng. Mater. Technol. July 1997; 119(3): 266–272. https://doi.org/10.1115/1.2812255
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