Hostname: page-component-78c5997874-g7gxr Total loading time: 0 Render date: 2024-11-05T16:56:55.660Z Has data issue: false hasContentIssue false

Progressive failure analysis for the interaction of interlaminar and intralaminar failure modes in composite structures with an initial delamination

Published online by Cambridge University Press:  27 January 2016

W. Ji
Affiliation:
Department of Aerospace Engineering, Composite Structures Laboratory, University of Michigan, Ann Arbor, Michigan, USA
A. M. Waas*
Affiliation:
University of Michigan, Ann Arbor, Michigan, USA Imperial College, London, UK

Abstract

This paper is concerned with the development of a failure initiation and progressive failure analysis (PFA) method for advanced composite structures. The present PFA model is capable of predicting interactive out-of-plane and in-plane failure modes observed in fiber reinforced composite laminates including interlaminar behavior and matrix microdamage at the mesoscale. A probability analysis tool is coupled with the PFA to account for uncertainty in modelling parameters caused by material variability and manufacturing inconsistencies. The progressive damage response of a laminated composite panel with an initial delamination is studied and used to demonstrate the PFA modelling framework that is presented here.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 2013 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Robinson, P. and Davies, G.A.O. Impactor mass and specimen geometry effects in low velocity impact of laminated composites, Int J Impact Eng, 1992, 12, (2), pp 189207.Google Scholar
2. Davies, G.A.O. and Zhang, X. Impact damage prediction in carbon composite structures, Int J Impact Eng, 1995, 16, (1), pp 149170.Google Scholar
3. Davies, G.A.O. and Zhang, X. Predicting impact damage of composite stiffened panels, Aeronaut J, 2000, 104, (1032), pp 97103.Google Scholar
4. Davies, G.A.O. and Olsson, R. Impact on composite structures, Aeronaut J, 2004, 108, (1089), pp 541563.Google Scholar
5. Shi, Y. and Soutis, C. A finite element analysis of impact damage in composite laminates, Aeronaut J, 2012, 116, (1186).Google Scholar
6. Song, S.J. and Waas, A.M. Nonlinear elastic foundation model for crack growth in laminates, J Composites Eng, 1993, 3, (10), pp 945959.Google Scholar
7. Xie, D. and Waas, A.M. Discrete cohesive zone model for mixed-mode fracture using finite element analysis, Eng Fracture Mechanics, 2006, 73, (13), pp 17831796.Google Scholar
8. Gustafson, P.A. and Waas, A.M. T650/AFR-PE-4/FM680-1 mode I critical energy release rate at high temperatures: Experiments and numerical models, 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, American Institute of Aeronautics and Astronautics, Honolulu HI, USA, 2007, AIAA 2007-2305.Google Scholar
9. Gustafson, P.A. and Waas, A.M. Efficient and robust traction laws for the modelling of adhesively bonded joints, 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, American Institute of Aeronautics and Astronautics, Schaumburg, IL, USA, 2008, AIAA 2008-1847.Google Scholar
10. Gustafson, P.A. and Waas, A.M. Experiments and cohesive zone model parameters for T650/AFR-PE-4/FM680-1 at high temperatures, J Aerospace Eng, 2011, 24, (3), pp 285297.Google Scholar
11. Kheng, E., Iyer, H.R., Podsiadlo, P., Kaushik, A.K., Kotov, N.A., Arruda, E.M. and Waas, A.M. Fracture toughness of exponential layer-by-layer polyurethane/poly(acrylic acid) nanocomposite films, Engineering Fracture Mechanics, 2010, 77, (16), pp 32273245.Google Scholar
12. Pankow, M., Waas, A.M., Yen, C.F. and Ghiorse, S. Resistance to delamination of 3D woven textile composites evaluated using End Notch Flexure (ENF) tests: Cohesive zone based computational results, Composites Part A: Applied Science and Manufacturing, 2011, 4212, pp 18631872.Google Scholar
13. Davidson, P., Waas, A.M. and Yerramalli, C. Experimental determination of validated, critical interfacial modes I and II energy release rates in a composite sandwich panel, Composite Structures, 2012, 94, (2), pp 477483.Google Scholar
14. Basu, S., Waas, A.M. and Ambur, D.R. Prediction of progressive failure in multidirectional composite laminated panels, Int J Solids and Structures, 2007, 44, (9), pp 26482676.Google Scholar
15. Rybicki, E.F. and Kanninen, M.F. Finite element calculation of stress intensity factors by modified crack closure integral, Engineering Fracture Mechanics, 1977, 9, (4), pp 931938.Google Scholar
16. Schapery, R.A. Theory of mechanical behavior of elastic media with growing damage and other changes in structure, J Mechanics and Physics of Solids, 1990, 38, (2), pp 215253.Google Scholar
17. Schapery, R.A. Prediction of compressive strength and kink bands in composites using a work potential, Int J Solids and Structures, 1995, 32, (6-7), pp 739765.Google Scholar
18. Rice, J.R. Inelastic constitutive relations for solids: an internal variable theory and its application to metal plasticity, J Mechanics and Physics of Solids, 1971, 19, (6), pp 433455.Google Scholar
19. Reeder, J.R., Song, K., Chunchu, P.B. and Ambur, D.R. Postbuckling and growth of delaminations in composite plates subjected to axial compression, 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, American Institute of Aeronautics and Astronautics, Denver, CO, 2002, AIAA 2002-1746.Google Scholar
20. Ranatunga, V., Bednarcyk, B.A. and Arnold, S.M. Modelling progressive damage using local displacement discontinuities within the FEAMAC multiscale modelling framework, 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, American Institute of Aeronautics and Astronautics, Orlando, FL, USA, 2010, AIAA 2010-2619.Google Scholar
21. Sicking, D.L. Mechanical characterization of nonlinear laminated composites with transverse crack growth, PhD thesis, Texas A M University, 1992.Google Scholar
22. Southwest Research Institute, NESSUS Users Manual, Ver. 9.5, 2010.Google Scholar
23. Wu, Y.T., Millwater, H.R. and Cruse, T.A. Advanced probabilistic structural-analysis method for implicit performance functions, AIAA J, 1990, 28, (9), pp 16631669.Google Scholar
24. Riha, D.S., Thacker, B.H., Pleming, J.B., Walker, J.D., Mullin, S.A., Weiss, C.E. and Rodriguez, E.A. and Leslie, P.O. Verification and validation for a penetration model using a deterministic and probabilistic design tool, Int J Impact Eng, 2006, 33, (1-12), pp 681690.Google Scholar
25. Thacker, B.H., Riha, D.S., Fitch, S.K., Huyse, L.J. and Pleming, J.B. Probabilistic engineering analysis using the NESSUS software, Structural Safety, 2006, 28, (1-2), pp 83107.Google Scholar