Many thermoplastic resin composite laminates, such as those made of APC-2, undergo a substantial temperature drop during their post-manufacturing cool down. This thermal excursion induces significant residual thermal stresses into the laminate due to the mutual geometric constraints among the multidirectional plies. In view of the considerable time-dependent relaxation which occurs during the cooling process, the residual thermal stresses exhibit strong dependence on the temperature history. However, in view of the high magnitudes of those stresses, the relaxation behavior is viscoelastically nonlinear. This paper demonstrates that it is possible to obtain an optimal cool-down path which minimizes the residual thermal stresses in APC-2 composites upon the termination of the cooling process.
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June 1994
Research Papers
Optimal Cool Down in Nonlinear Thermoviscoelasticity With Application to Graphite/Peek (APC-2) Laminates
K. Lee,
K. Lee
Department of Engineering Science and Mechanics, The University of Tennessee, Knoxville, TN 37996-2030
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Y. Weitsman
Y. Weitsman
Department of Engineering Science and Mechanics, The University of Tennessee, Knoxville, TN 37996-2030
Search for other works by this author on:
K. Lee
Department of Engineering Science and Mechanics, The University of Tennessee, Knoxville, TN 37996-2030
Y. Weitsman
Department of Engineering Science and Mechanics, The University of Tennessee, Knoxville, TN 37996-2030
J. Appl. Mech. Jun 1994, 61(2): 367-374 (8 pages)
Published Online: June 1, 1994
Article history
Received:
December 11, 1991
Revised:
September 24, 1992
Online:
March 31, 2008
Citation
Lee, K., and Weitsman, Y. (June 1, 1994). "Optimal Cool Down in Nonlinear Thermoviscoelasticity With Application to Graphite/Peek (APC-2) Laminates." ASME. J. Appl. Mech. June 1994; 61(2): 367–374. https://doi.org/10.1115/1.2901453
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