This paper deals with the nonlinear dynamic buckling of laminated composite rectangular plates subjected to uniform time-dependent in-plane temperature-induced loading. The dynamic post-buckling deflection response is obtained and dynamic critical temperatures are estimated. The nonlinear governing equations of motion are solved analytically using fast Chebyshev series technique. The numerical results for CCCC, CCCS, CCSS, CSCS, CSSS and SSSS boundary conditions are presented.
Buckling of Laminated Composite Rectangular Plates Under Transient Thermal Loading
Contributed by the Applied Mechanics Division of THE AMERICAN SOCIETY OF MECHANICAL ENGINEERS for publication in the ASME JOURNAL OF APPLIED MECHANICS. Manuscript received by the ASME Applied Mechanics Division, February 1, 2001; final revision, November 15, 2001. Associate Editor: R. C. Benson. Discussion on the paper should be addressed to the Editor, Prof. Robert M. McMeeking, Department of Mechanical and Environmental Engineering University of California–Santa Barbara, Santa Barbara, CA 93106-5070, and will be accepted until four months after final publication of the paper itself in the ASME JOURNAL OF APPLIED MECHANICS.
- Views Icon Views
- Share Icon Share
- Cite Icon Cite
- Search Site
Shukla, K. K., and Nath, Y. (August 16, 2002). "Buckling of Laminated Composite Rectangular Plates Under Transient Thermal Loading ." ASME. J. Appl. Mech. September 2002; 69(5): 684–692. https://doi.org/10.1115/1.1485755
Download citation file:
- Ris (Zotero)
- Reference Manager