A study of the mechanics and failure modes of delamination initiated from a surface flaw in angle-ply fiber-reinforced composites is presented. The analysis employs a hybrid-stress finite-element method including a crack-tip singular element with its field variables expressed by Muskhelishvili’s complex stress functions. Solutions are obtained for the delaminated composites with various laminate parameters. The results elucidate unique and important characteristics of delamination crack-tip response and interlaminar stress transfer mechanisms. Of particular interest are the mixed-mode stress-intensity factors associated with the delamination crack. The influence of ply orientation on KI and KII and their effects on subsequent crack extension are discussed.
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March 1980
Research Papers
An Analysis of Delamination in Angle-Ply Fiber-Reinforced Composites
S. S. Wang
S. S. Wang
Department of Theoretical and Applied Mechanics, University of Illinois, Urbana, Ill. 61801
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S. S. Wang
Department of Theoretical and Applied Mechanics, University of Illinois, Urbana, Ill. 61801
J. Appl. Mech. Mar 1980, 47(1): 64-70 (7 pages)
Published Online: March 1, 1980
Article history
Received:
August 1, 1978
Revised:
June 1, 1979
Online:
July 21, 2009
Citation
Wang, S. S. (March 1, 1980). "An Analysis of Delamination in Angle-Ply Fiber-Reinforced Composites." ASME. J. Appl. Mech. March 1980; 47(1): 64–70. https://doi.org/10.1115/1.3153639
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