Failure analysis of laminated composite decks structures has attracted a great deal of interest in recent years due to the increased application of composite materials in a wide range of high-performance structures. Intensive experimental and theoretical studies of failure analysis and prediction are being reviewed. Delamination, the separation of two adjacent plies in composite laminates, represents one of the most critical failure modes in composite laminates. In fact, it is an essential issue in the evaluation of composite laminates for durability and damage tolerance. Thus, broken fibers, delaminated regions, cracks in the matrix material, as well as holes, foreign inclusions and small voids constitute material and structural imperfections that can exist in composite structures. Imperfections have always existed and their effect on the structural response of a system has been very significant in many cases. These imperfections can be classified into two broad categories: initial geometrical imperfections and material or constructional imperfections. Delamination is a critical failure mode in fiber-reinforced composite decks plates and beams. It may lead directly to through-thickness failure owing to interlaminar stresses caused by out of plane loading, curved or tapered geometry, or discontinuities owing to cracks, ply drops or free edges. Impact loading causes multiple delaminations, which can propagate in conjunction with sub laminate buckling, greatly reducing the residual compressive strength.
| Published in | Bioprocess Engineering (Volume 4, Issue 1) |
| DOI | 10.11648/j.be.20200401.12 |
| Page(s) | 9-16 |
| Creative Commons |
This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited. |
| Copyright |
Copyright © The Author(s), 2024. Published by Science Publishing Group |
Delamination, Composite Laminates, Rectangular Plates, Review
| [1] | David Roylance, ' an introduction to composite materials', Department of material science and engineering, Massachusetts Institute of Technology, Cambridge; (2000). |
| [2] | Stephen W. Tsai, Thomas Hahn H., ' introduction to composite materials', Technomic publishing company; (1980). |
| [3] | Turvey G. J., Marshall I. H., 'buckling and post buckling of composite plates', Great Britain, T. J. press Ltd, Padstow, Cornwall; (1995). |
| [4] | Vernon B. John, ' introduction to engineering materials', second edition; (1972). |
| [5] | Jan Stegmann and Erik Lund, ' notes on structural analysis of composite shell structures', Aalborg University, Denmark; (2001). |
| [6] | A. C. Garg, A damage model in composite structures, Engineering Fracture Mech., 1998. vol. 29. |
| [7] | O. O. Ochoa. and Reddy J. N, Finite elements analysis of composites laminates, Kluwer, 1992. |
| [8] | S. Jain and D. C. H. Yang, Effects of federate and chisel edge on delamination in composite drilling. Processing and Manufacturing of Composite Materials, ASME PED 49. 1991. Vol. 27. |
| [9] | D. Engrand, Boundary layer approach to the Calculation of Transverse stresses along the Free Edge of a Symmetric Laminated Plate of Arbitrary Width under in Plane Loading, Composites Structures, 1981. |
| [10] | H. Dumontet., Study of Boundary layer Problem in Elastic composite Materials, M2AN, 20, 1986. |
| [11] | R. Y. Kim. and S. R. Sony, Delamination of Composite Laminates Stimulated by interlaminar Shear, ASTM-STP 893, 1986. |
| [12] | A. S. D. Wang, M. Slomania. and R. B. Bucinell, Delamination Crack Growth in Composite Laminates. Delamination and Debonding of Materials, JOHNSON W. S (Ed.), ASTMSTP, 1985. |
| [13] | A. S. D. WANG, Fracture Analysis of Interlaminar cracking, Interlaminar response of Composite Materials, Composite materials Series, PAGANO N. J. (Ed.) Elsevier, 1989. |
| [14] | D. B. Davidson., R. Kruger and M. König. Effect of stacking sequence on energy release rate distribution in multi-directional DCB and ENF specimens. Engineering Fracture Mech., 1996. vol. 55-4. |
| [15] | T. K. O'Brien, Mixed-mode strain-energy-release rate effects on edge delamination of composites, In: damage in composite Materials, ASTM STP 836, ASTM, Philadelphia, PA, 1984. |
| [16] | M. Fremond. Adherence des solides, J. Mécan. Théor. Appl. 6, 1987. |
| [17] | M. Fremond. Contact with Adhesion. In Topic in Non-smooth Mechanics, Birkhäuser, 1988. |
| [18] | N. Point, Approche Mathématiques de problèmes à frontières libres: Application à des exemples physiques, Thèse de doctorat d’Etat Es-Sciences Mathématiques de l’Université Paris XIII, 1989. |
| [19] | J. M. Truong Dinh Tien, Contact avec adhérence. Thèse de Doctorat de l’Université Paris VI, 1990. |
| [20] | L. Ascione and D, Bruno On delamination problem of two layer plates. In unilateral problems in Structural Analysis, Springer, Berlin, 1985. |
| [21] | A. Girmaldi and J. N, Reddy On delamination in plates: a unilateral contact approach. In Unilateral Problems in Structural Analysis, Springer, Berlin, 1985. |
| [22] | PLadevèze. A damage computational method for composite structures. Computer Structures, (1992). vol. 44. |
| [23] | O. Allix. and P. Ladevèze, Interlaminar interface modeling for the prediction of delamination, Composites Structures, 1992. |
| [24] | A. Corigliano, Formulation identification and use of interface models in the numerical analysis of composite delamination, Int. J. Solids Structures, 1993. vol. 30. |
| [25] | J. C. Schellekens and DE R. Borst, Free edge delamination in carbon epoxy laminates: A novel numerical/experimental approach, Composites Structures, 1993. vol. 28. |
| [26] | Leandro José da Silva1, TúlioHallak Panzera, André Luis Christoforo, Luís Miguel Pereira Durão, Francisco Antonio Rocco Lahr, Numerical and Experimental Analyses of Bio composites Reinforced with Natural Fibers, International Journal of Materials Engineering 2012, 2 (4): 43-49. |
| [27] | D. Benzerga, A. Haddi., ASeddak. and ALavie, mixed-mode damage model for delamination growth applied to a new woven composite, Computational Materials Science, 2008. vol. 41, pp. 515–521. |
| [28] | P. Ladevèze and E. Ledantec, Damage modeling of the elementary ply for laminated composites, Composites Sciences and technology, 1992. vol. 43. |
| [29] | O. Alix and P. Ladevèze, Interlaminar Interface modeling for Prediction of Delamination, Composites Structures, 1992. vol. 22. |
| [30] | F. Gruttmann and W. Wagner, On the numerical analysis of local effects, Composites structures, 1994. vol. 29. |
| [31] | J. C. Simo and M. S. Rifai. A, class of mixed assumed strain methods and the method of incompatible modes, Int. Num. Meth. Eng, 1990. vol. 29. |
| [32] | P. P. Camanho, C. G. Dàvila and D. R Ambur, Numerical Simulation of Delamination Growth in Composite Materials. NASA/TP -211041, 2001. |
| [33] | Naruoka M., 'Bibliography on theory of plates', Gihodo, Tokyo; (1981). |
| [34] | Winterstetter Th. A. and Schmidt H., 'Stability of circular cylindrical steel shells under combined loading', Thin–walled structures; (2002), 40: PP. (893–909). |
| [35] | Pircher M., and Bridge R., ' The influence of circumferential weld–induced imperfections on the buckling of silos and tanks', Journal of constructional steel research; (2001), 57 (5): PP. (569–580). |
| [36] | Deml M., and Wunderlich W.,' Direct evaluation of the worst imperfection shape in shell buckling', Computer methods in applied mechanics and engineering; (1997), 149 [1–4]: PP. (201–222). |
| [37] | Arbocz J., and Starnes J. H.,' Future directions and challenges in shell stability analysis', Thin–walled structures; (2002), 40: PP. (729–754). |
| [38] | Arbocz J.,' The effect of imperfect boundary conditions on the collapse behavior of anisotropic shells', International Journal of solids and structures; (2000), 37: PP. (6891–6915). |
| [39] | Huhne C., Zimmermann R., Rolfes R., and Geier B., 'loading imperfections–experiments and Computations', Euromech Colloquium 424; (2001), the Netherlands. |
| [40] | Geier B., Klein H., and Zimmermann R.,' Buckling tests with axially Compressed unstiffened cylindrical shells made from CFRP', proceedings, International Colloquium on buckling of shell structures on land, in the sea, and in the air, Elsevier applied sciences; (1991), London and New York: PP. (498–507). |
| [41] | Geier B., Klein H., and Zimmermann,' Experiments on buckling of CFRP Cylindrical shells under non–uniform axial load', proceedings of international conference on Composites engineering; (1994). |
| [42] | Albus J., Gomez–Garcia J., and oery H.,' Control of assembly induced stresses and deformations due to the waviness of the interface flanges of the ESC–An upper stage', 52nd International astronautical congress; (2001), Toulouse, France. |
| [43] | Zimmermann R.,' Buckling research for imperfection tolerant fiber composite structures', proceeding of the conference on spacecraft structures, material and mechanical testing, Nordwijk, The Netherlands: (1996). |
| [44] | Meyer–Piening H. R., Farshad M., Geier B., and Zimmermann, 'Buckling loads of CFRP Composite cylinders under combined axial and torsion loading–experiments and computations', Composite structures; (2001), 52: PP. (427–435). |
| [45] | CMH–17 (Composite Material Handbook–17), Material science corporation; (2010). |
| [46] | Guo S. J.,' Stress concentration and buckling behaviour of shear loaded composite panels with reinforced cutouts', Composite structures;( 2007): PP. (1–9). |
| [47] | Remmers J. J. C., and de Borst R.,' Delamination buckling of fiber–metal laminates', Composite science and technology; (2001): PP. (2207–2213). |
| [48] | Vit obdrzalek, and Jan Vrbka,' Buckling and post buckling of a large delaminated plate subjected to shear loading', Engineering mechanics, vol. 16; (2009), No. 4: PP. (297–312). |
| [49] | Vit obdrzalek, and Jan Vrbka,' On buckling of a plate with multiple delaminations', Engineering mechanics, vol. 17; (2010), No. 1: PP. (37–47). |
| [50] | Keiichi Nemoto, Hirakazu Kasuya, Hisao Kikugawa, and Takashi Asaka,' post buckling behavior of composite laminated plates with initial imperfections under biaxial compression', Materials transactions, vol. 50, No. 2; (2009): PP. (299–304). |
| [51] | Takao Y., Taya M., and Chou T. W.,' Stress field due to cylindrical inclusion with constant axial Eigen strain in an infinite elastic body', Journal of applied mechanics; (1981), 48 (4): PP. (853–858). |
| [52] | Lakshminarayana H. V., and Murthy M. V. V.,' On stresses around an arbitrarily oriented Crack in cylindrical shell', International Journal of fracture; (1976), 12 (4): PP. (547–566). |
| [53] | Twee J., and Rooke D. P,' The stress intensity factor for a crack at the edge of a loaded hole', International Journal of solids and structures; (1979), 15: PP. (899–906). |
| [54] | Dyshel M. S.,' Fracture of plates with cracks under tension after loss of stability', Journal of applied mathematics and mechanics (PMM); (1981), 17 (4): PP. (77–83). |
| [55] | Erdogan F., Ratwani M., and Yuceoglu U.,' On the effect of orthotropy in cracked cylindrical plates', International Journal of fracture; (1974), 10 (4): PP. (369–374). |
| [56] | Krenk S.,' Influence of transverse shear on an axial crack in a cylindrical shell', International Journal of fracture; (1978), 14 (2): PP. (123–142). |
| [57] | Delale F., and Erdogan F.,' Effect of transverse shear and material orthotropy in a cracked spherical cap', International Journal of solids and structures; (1979), 15: PP. (907–926). |
| [58] | Lakshminarayana H. V., and Murthy M. V. V,' On a finite element model for the analysis of through cracks in laminated anisotropic cylindrical shells', Engineering fracture mechanics; (1981), 14 (4): PP. (697–712). |
| [59] | Theocaris P. S., and Milios J.,' Crack–arrest at a bimaterial interface', International Journal of solids and structures; (1981), 17: PP. (217–230). |
| [60] | Rogers T. G.,' Crack extension and energy release rates in finitely deformed sheet reinforced with inextensible fibers', International Journal of solids and structures; (1982), 18: PP. (705–721). |
| [61] | Kachanov L. M.,' Separation failure of composite materials', polymer mechanics; (1976), 6 (12): PP. (812–815). |
| [62] | Williams J. G., and et al.,' Recent developments in the design, testing and impact damage–tolerance of stiffened composite plates', Nasa TM 80077; (1979), April. |
| [63] | Wilkins D. J, and et al.,' characterizing delamination growth in graphite–epoxy', Damage in composite materials; (1982): PP. (168–183). |
| [64] | Wang S. S.,' Edge delamination in angle–ply composite laminates', AIAA Journal; (1984), 22 (2): PP. (256–264). |
| [65] | Scott W. Beckwith,' Manufacturing defects in composite structures', Sample Journal, volume 48, No. 5; September/October (2012). |
| [66] | M. Vable,' Stability of columns', Mechanics of materials; (2014): chapter eleven: PP. (496–528). |
| [67] | CPNI EBP,' Influence of delamination of laminated glass on its blast performance', July (2013). |
APA Style
Osama Mohammed Elmardi Suleiman Khayal. (2020). Delamination Phenomenon in Composite Laminated Plates and Beams. Bioprocess Engineering, 4(1), 9-16. https://doi.org/10.11648/j.be.20200401.12
ACS Style
Osama Mohammed Elmardi Suleiman Khayal. Delamination Phenomenon in Composite Laminated Plates and Beams. Bioprocess Eng. 2020, 4(1), 9-16. doi: 10.11648/j.be.20200401.12
AMA Style
Osama Mohammed Elmardi Suleiman Khayal. Delamination Phenomenon in Composite Laminated Plates and Beams. Bioprocess Eng. 2020;4(1):9-16. doi: 10.11648/j.be.20200401.12
Share This Article
Twitter
Linked In
Facebook
Copy
Download@article{10.11648/j.be.20200401.12,
author = {Osama Mohammed Elmardi Suleiman Khayal},
title = {Delamination Phenomenon in Composite Laminated Plates and Beams},
journal = {Bioprocess Engineering},
volume = {4},
number = {1},
pages = {9-16},
doi = {10.11648/j.be.20200401.12},
url = {https://doi.org/10.11648/j.be.20200401.12},
eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.be.20200401.12},
abstract = {Failure analysis of laminated composite decks structures has attracted a great deal of interest in recent years due to the increased application of composite materials in a wide range of high-performance structures. Intensive experimental and theoretical studies of failure analysis and prediction are being reviewed. Delamination, the separation of two adjacent plies in composite laminates, represents one of the most critical failure modes in composite laminates. In fact, it is an essential issue in the evaluation of composite laminates for durability and damage tolerance. Thus, broken fibers, delaminated regions, cracks in the matrix material, as well as holes, foreign inclusions and small voids constitute material and structural imperfections that can exist in composite structures. Imperfections have always existed and their effect on the structural response of a system has been very significant in many cases. These imperfections can be classified into two broad categories: initial geometrical imperfections and material or constructional imperfections. Delamination is a critical failure mode in fiber-reinforced composite decks plates and beams. It may lead directly to through-thickness failure owing to interlaminar stresses caused by out of plane loading, curved or tapered geometry, or discontinuities owing to cracks, ply drops or free edges. Impact loading causes multiple delaminations, which can propagate in conjunction with sub laminate buckling, greatly reducing the residual compressive strength.},
year = {2020}
}
TY - JOUR T1 - Delamination Phenomenon in Composite Laminated Plates and Beams AU - Osama Mohammed Elmardi Suleiman Khayal Y1 - 2020/02/04 PY - 2020 N1 - https://doi.org/10.11648/j.be.20200401.12 DO - 10.11648/j.be.20200401.12 T2 - Bioprocess Engineering JF - Bioprocess Engineering JO - Bioprocess Engineering SP - 9 EP - 16 PB - Science Publishing Group SN - 2578-8701 UR - https://doi.org/10.11648/j.be.20200401.12 AB - Failure analysis of laminated composite decks structures has attracted a great deal of interest in recent years due to the increased application of composite materials in a wide range of high-performance structures. Intensive experimental and theoretical studies of failure analysis and prediction are being reviewed. Delamination, the separation of two adjacent plies in composite laminates, represents one of the most critical failure modes in composite laminates. In fact, it is an essential issue in the evaluation of composite laminates for durability and damage tolerance. Thus, broken fibers, delaminated regions, cracks in the matrix material, as well as holes, foreign inclusions and small voids constitute material and structural imperfections that can exist in composite structures. Imperfections have always existed and their effect on the structural response of a system has been very significant in many cases. These imperfections can be classified into two broad categories: initial geometrical imperfections and material or constructional imperfections. Delamination is a critical failure mode in fiber-reinforced composite decks plates and beams. It may lead directly to through-thickness failure owing to interlaminar stresses caused by out of plane loading, curved or tapered geometry, or discontinuities owing to cracks, ply drops or free edges. Impact loading causes multiple delaminations, which can propagate in conjunction with sub laminate buckling, greatly reducing the residual compressive strength. VL - 4 IS - 1 ER -
Information
Email: