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DIGITAL LIBRARY: CAMX 2019 | ANAHEIM, CA | SEPTEMBER 23-26

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Predicting Failure of Woven Composite Laminates

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Title: Predicting Failure of Woven Composite Laminates

Authors: Daniel C. Munden, Arunkumar Satyanarayana, and David W. Sleight

DOI: 10.33599/nasampe/c.19.0661

Abstract: This paper seeks to develop and validate a methodology for predicting the failure of woven composite laminates. A material model and user-subroutine were created for woven composites, which were then used to carry out finite element analyses (FEA) for woven composite laminates. Forty coupon laminates made from T650/5320 graphite-epoxy material system were notched and tested under tensile loading conditions. Data was recorded using strain gages and digital image correlation (DIC). Portions of the test data were used to define the material model more completely and the rest of the test data was used for validation. The model predicted the failure load of more than half of the test cases within 5%, which indicates that the model performs well for the range of coupons tested and the intended application of the model.

References: 1. T. Johnson, "Composites In Aerospace," 2 April 2017. [Online]. Available: https://www.thoughtco.com/composites-in-aerospace-820418. 2. S. Tsai, THEORY OF COMPOSITES DESIGN, Dayton: Think Composites, 1992. 3. C. Sun, B. Quinn, J. Tao and D. Oplinger, "COMPARATIVE EVALUATION OF FAILURE ANALYSIS METHODS FOR COMPOSITE LAMINATES," U.S. Department of Transportation , Washington, D.C. , 1996. 4. University of Cambridge, "Failure of laminates and the Tsai–Hill criterion," [Online]. Available: https://www.doitpoms.ac.uk/tlplib/fibre_composites/laminate_failure.php. [Accessed 10 April 2018]. 5. A.Puck and H.Schürmann, "Failure analysis of FRP laminates by means of physically based phenomenological models," Composites Science and Technology, vol. 62, no. 12-13, pp. 1633-1662, 2002. 6. Z. Hashin, "Failure Criteria for Unidirectional Fiber Composites," Journal of Applied Mechanics , vol. 47, pp. 329-334, 1980. 7. J. Z. Wang and D. F. Socie, "Biaxial Testing and Failure Mechanisms in Tubular G-10 Composite Laminates," Composite Materials: Testing and Design, vol. 11, no. ASTM STP 1206, pp. 136-149, 1992. 8. L. Zhao, T. Qin, J. Zhang and R. A. Shenoi, "Modified maximum stress failure criterion for composite pi joints," Journal of Composite Materials, no. doi:10.1177/0021998312460713., 2012. 9. R. Zahari, A. H. Azmee, F. Mustapha, M. S. Salit, R. Varatharajoo and A. Shakrine, "PREDICTION OF PROGRESSIVE FAILURE IN WOVEN GLASS/EPOXY COMPOSITE LAMINATED PANELS," Jurnal Mekanikal, no. 25, pp. 80 - 91, 2008. 10. Z.-N. Feng, H. G. Allen and S. S. Moy, "Theoretical and experimental investigation of progressive failure of woven composite panels," Journal of Composite Materials, vol. 33, no. 11, pp. 1030-1047, 1999. 11. A. Satyanarayana, P. Bogert, K. Karayev, P. Nordman, H. Razi. April 2012. Influence of Finite Element Size in Residual Strength Prediction of Composite Structures. Structural Dynamics and Materials Conference. Honolulu, HI. 12. National Center for Advanced Materials Performance (NCAMP), National Institute for Aviation Research (NIAR). Cytec Cycom 5320-1 T650 3k-PW Fabric Qualification Material Property Data Report. October 2015. Wichita, KS. 13. Z. Hashin. Failure Criteria for Unidirectional Fiber Composites. Journal of Applied Mechanics, vol. 47, pp. 329-334, 1980.

Conference: CAMX 2019

Publication Date: 2019/09/23

SKU: TP19-0661

Pages: 15

Price: $30.00

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