nach oben

Erschienen in:

2015 | OriginalPaper | Buchkapitel

5. Influence of Intralaminar Damage on the Delamination Crack Evolution

verfasst von : Cédric Huchette, Thomas Vandellos, Frédéric Laurin

Erschienen in: Damage Growth in Aerospace Composites

Verlag: Springer International Publishing

Einloggen

Aktivieren Sie unsere intelligente Suche, um passende Fachinhalte oder Patente zu finden.

search-config

KI-gestützte Suche

Aus

Abstract

The aim of this chapter is to investigate the influence of the intralaminar damage (transverse matrix cracks and their associated local delaminations) on the interlaminar damage (delamination) evolution in composite laminate materials. Using specific device setups and coupons, this influence on the delamination onset and growth is demonstrated experimentally. In order to model this inter/intralaminar damage coupling, a cohesive zone model is developed. It takes into account the influence of the local delamination cracks resulting from transverse matrix cracking in the adjacent plies, damages which are both predicted through a continuum damage model of the ply behavior in the laminate. The application of these models to a double-edge-notched specimen under tensile loading clearly demonstrates the importance of the contribution of the introduced coupling on damage pattern. The aim of this chapter is to investigate the influence of the intralaminar damage (transverse matrix cracks and their associated local delaminations) on the interlaminar damage (delamination) evolution in composite laminate materials. Using specific device setups and coupons, this influence on the delamination onset and growth is demonstrated experimentally. In order to model this inter/intralaminar damage coupling, a cohesive zone model is developed. It takes into account the influence of the local delamination cracks resulting from transverse matrix cracking in the adjacent plies, damages which are both predicted through a continuum damage model of the ply behavior in the laminate. The application of these models to a double-edge-notched specimen under tensile loading clearly demonstrates the importance of the contribution of the introduced coupling on damage pattern.

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

über 102.000 Bücher
über 537 Zeitschriften

aus folgenden Fachgebieten:

Automobil + Motoren
Bauwesen + Immobilien
Business IT + Informatik
Elektrotechnik + Elektronik
Energie + Nachhaltigkeit
Finance + Banking
Management + Führung
Marketing + Vertrieb
Maschinenbau + Werkstoffe
Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Jetzt informieren

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

über 67.000 Bücher
über 390 Zeitschriften

aus folgenden Fachgebieten:

Automobil + Motoren
Bauwesen + Immobilien
Business IT + Informatik
Elektrotechnik + Elektronik
Energie + Nachhaltigkeit
Maschinenbau + Werkstoffe

Jetzt Wissensvorsprung sichern!

Jetzt informieren

Vorheriges Kapitel Delamination Growth in Composite Plates Under Fatigue Loading Conditions

Nächstes Kapitel Microdamage Modeling in Laminates

Abisset, E., Daghia, F., Ladevèze, P.: On the validation of a damage mesomodel for laminated composites by means of open-hole tensile tests on quasi-isotropic laminates. Compos. Part A Appl. Sci. Manuf. 42, 1515–1524 (2011)CrossRef

Allix, O., Deu, J.F.: Delayed-damage modelling for fracture prediction of laminated composites under dynamic loading. Eng. Trans. Rozprawy Inzynierskie 45(1), 29–46 (1997)

Allix, O., Ladevèze, P.: Interlaminar interface modeling for the prediction of laminate delamination. Compos. Struct. 22, 235–242 (1992)CrossRef

Allix, O., Ladevèze, P., Corigliano, A.: Damage analysis of interlaminar fracture specimens. Compos. Struct. 31, 61–74 (1995)CrossRef

Allix, O., Lévêque, D., Perret, L.: Identification and forecast of delamination in composite laminates by an interlaminar interface model. Compos. Sci. Technol. 58(5), 671–678 (1998)CrossRef

Andersons, J., Knig, M.: Dependence of fracture toughness of composite laminates on interface ply orientations and delamination growth direction. Compos. Sci. Technol. 64, 2139–2152 (2004)CrossRef

ASTM (1994) Standard test method for mode I interlaminar fracture toughness of unidirectional continuous fiber reinforced composite materials. D5528-94A, Philadelphia, PA

ASTM (2001) Standard test method for mixed mode I-mode II interlaminar fracture toughness of unidirectional fiber-reinforced polymer matrix composites. D6671-01

ASTM (2006a) Standard test method for measuring the curved beam strength of fibre reinforced polymer matrix composite. D6415/D6415M-06a

10.

ASTM (2006b) Standard test method for short-beam strength of polymer matrix composite materials and their laminates. D2344/D2344M-00

11.

Barenblatt, G.: Mathematical theory of equilibrium cracks in brittle failure. Adv. Appl. Mech. 7, 55–129 (1962)CrossRefMathSciNet

12.

Benzeggagh, M., Kenane, M.: Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus. Compos. Sci. Technol. 56, 439–449 (1996)CrossRef

13.

Berthelot, J.M.: Transverse cracking and delamination in cross-ply glass-fiber and carbon-fiber reinforced plastic laminates: Static and fatigue loading. Appl. Mech. Rev. 56(1), 111–147 (2003)CrossRef

14.

Blackman, B., Kinloch, A.: Fracture tests for structural adhesive joints. In: Moore, D., Pavan, A., Williams, J. (eds.) Fracture Mechanics Testing Methods for Polymers, Adhesives and Composites, pp. 225–270. Elsevier, Amsterdam (2001)CrossRef

15.

Caiazzo, A., Costanzo, F.: Modeling the constitutive behavior of layered composites with evolving cracks. Int. J. Solid Struct. 38(20), 3469–3485 (2001)CrossRefMATH

16.

Camanho, P., Dávila, C., de Moura, M.: Numerical simulation of mixed-mode progressive delamination in composite materials. J. Compos. Mater. 37(16), 1415–1438 (2003)CrossRef

17.

Carlsson, L., Gillepsie, J., Pipes, R.: On the analysis and design of the end notched flexure (ENF) specimen for mode II testing. J. Compos. Mater. 20, 594–604 (1986)CrossRef

18.

Charrier, J., Carrère, N., Laurin, F., Bretheau, T., Goncalves-Novo, E., Mahdi, S.: Proposition of 3D progressive failure approach and validation on tests cases. In: 14th European Conference on Composite Materials (ECCM/14) (2010)

19.

Charrier, J., Carrère, N., Laurin, F., Goncalves-Novo, E., Mahdi, S.: Proposition d’une méthode d’analyse dédiée aux structures composites soumises à des sollicitations hors-plan. In: 17ème Journées Nationales sur les Composites (JNC 17) (2013)

20.

Choi, N., Kinloch, A., Williams, J.: Delamination fracture of multidirectional carbon-fiber/epoxy composites under mode I, mode II and mixed-mode I/II loading. J. Compos. Mater. 33, 73–100 (1999)CrossRef

21.

Crews, J., Reeder, J.: A mixed-mode bending apparatus for delamination testing. Technical report, Langley Research Center, Virginia, USA (1988)

22.

Cui, W., Wisnom, M., Jones, M.: A comparison of failure criteria to predict delamination of unidirectional glass/epoxy specimens waisted through the thickness. Composites 23(3), 158–166 (1992)CrossRef

23.

Daghia, F., Ladevèze, P.: Identification and validation of an enhanced mesomodel for laminated composites within the WWFE-III. J. Compos. Mater. 47(20–21), 2675–2693 (2013). doi:10.1177/0021998313494095. URL http://jcm.sagepub.com/content/47/20-21/2675

24.

Daudeville, L., Ladevèze, P.: A damage mechanics tool for laminate delamination. Compos. Struct. 25, 547–555 (1993)CrossRef

25.

Dávila, C., Camanho, P., Turon, A.: Effective simulation of delamination in aeronautical structures using shells and cohesive elements. J. Aircr. 45, 663–672 (2008)CrossRef

26.

de Morais, A., Pereira, A.: Mixed-mode I + II interlaminar fracture of glass/epoxy multidirectional laminates—part 1: analysis. Compos. Sci. Technol. 66, 1889–1895 (2006)CrossRef

27.

de Morais, A., Pereira, A.: Application of the effective crack method to mode I and mode II interlaminar fracture of carbon/epoxy unidirectional laminates. Compos. Part A Appl. Sci. Manuf. 38, 785–794 (2007)CrossRef

28.

de Morais, A., de Moura, M., Marques, A., de Castro, P.: Mode I interlaminar fracture of carbon/epoxy cross-ply composites. Compos. Sci. Technol. 62, 679–686 (2002)CrossRef

29.

Dugdale, D.: Yielding of steel sheets containing slits. J. Mech. Phys. Solids 8, 100–104 (1960)CrossRef

30.

Germain, N., Besson, J., Feyel, F.: Composite layered materials: anisotropic nonlocal damage models. Comput. Method Appl. Mech. 196(4144), 4272–4282 (2007). doi:10.1016/j.cma.2007.04.009. URL http://www.sciencedirect.com/science/article/pii/S004578250700182X

31.

Gong, X., Benzeggagh, M.: Mixed mode interlaminar fracture toughness of unidirectional glass/epoxy composite. In: Composite Materials: Fatigue and Fracture, vol. 5, pp. 100–123. ASTM STP 1230 (1995)

32.

Guinard, S., Allix, O., Guédra-Degeorges, D., Vinet, A.: A 3D damage analysis of low-velocity impacts on laminated composites. Compos. Sci. Technol. 62, 585–589 (2002)CrossRef

33.

Hinton, M., Kaddour, A., Soden, P.: Failure Criteria in Fibre Reinforced Polymer Composites: The World-Wide Failure Exercise. Elsevier Science Ltd., Oxford (2004)

34.

Huchette, C., Guinot, F.: Experimental and numerical analysis on delamination growth in damaged composite material. In: 13th European Conference on Composite Materials (ECCM/13) (2008)

35.

Huchette, C., Lévêque, D., Carrère, N.: A multiscale damage model for composite laminate based on numerical and experimental complementary tests. In: Sadowski, T. (ed.) IUTAM Symposium on Multiscale Modelling of Damage and Fracture Processes in Composite Materials, No. 135 in Solid Mechanics and Its Applications, pp. 241–248. Springer, Netherlands (2006). URL http://link.springer.com/chapter/10.1007/1-4020-4566-2_28

36.

Huchette, C.: Sur la complémentarité des approches expérimentales et numériques pour la modélisation des mécanismes d’endommagement des composites stratifiés. Ph.D. thesis, University of Paris VI—Pierre et Marie Curie, France (2005)

37.

ISO (1987) Adhesives—determination of Tensile Strength of Butt Joints. ISO 6922

38.

Jackson, W., Ifju, P.: Through-the-thickness tensile strength of textile composites. Composite materials: testing and design 12, ASTM STP 1274, 218–238 (1996)

39.

Ju, J.: On energy-based coupled elastoplastic damage theories: constitutive modeling and computational aspects. Int. J. Solids Struct. 25, 803–833 (1989)CrossRefMATH

40.

Kortschot, M., Beaumont, P.: Damage mechanics of composite materials. I: a damage based notched strength model. Compos. Sci. Technol. 39, 289–301 (1990)CrossRef

41.

Kortschot, M., Beaumont, P.: Damage mechanics of composite materials. II: measurements of damage and strength. Compos. Sci. Technol. 39, 303–326 (1990)CrossRef

42.

Kortschot, M., Beaumont, P., Ashby, M.: Damage mechanics of composite materials. III: prediction of damage growth and notched strength. Compos. Sci. Technol. 40, 147–165 (1991)CrossRef

43.

Krueger, R.: The virtual crack closure technique: history, approach and applications. Technical report, ICASE, Hampton, Virginia (2002)

44.

Ladevèze, P., LeDantec, E.: Damage modelling of the elementary ply for laminated composites. Compos. Sci. Technol. 43(3), 257–267 (1992). doi:10.1016/0266-3538(92)90097-M. URL http://www.sciencedirect.com/science/article/pii/026635389290097M

45.

Ladevèze, P., Lubineau, G., Marsal, D.: Towards a bridge between the micro- and mesomechanics of delamination for laminated composites. Compos. Sci. Technol. 66, 698–712 (2006)CrossRef

46.

Laurin, F., Carrère, N., Huchette, C., Maire. J.F.: A multiscale hybrid approach for damage and final failure predictions of composite structures. J. Compos. Mater 47(20–21), 2713–2747 (2013). doi:10.1177/0021998312470151. URL http://jcm.sagepub.com/content/47/20-21/2713

47.

Laurin, F., Carrère, N., Maire, J.F.: A multiscale progressive failure approach for composite laminates based on thermodynamical viscoelastic and damage models. Compos. Part A Appl. Sci. Manuf. 38, 198–209 (2007)CrossRef

48.

Laurin, F., Charrier, J.S., Lévêque, D., Maire, J.F., Mavel, A., Nunez, P.: Determination of the properties of composite materials thanks to digital image correlation measurements. Procedia IUTAM 4, 106–115 (2012)CrossRef

49.

Leguillon, D.: Strength or toughness? A criterion for crack onset at a notch. Eur. J. Mech. A-Solid 21, 61–72 (2002)CrossRefMATH

50.

Lekhnitskii, S.G.: Theory of Elasticity of an Anisotropic Elastic Body. Holden-Day Edn. Inc., San Francisco (1963)

51.

NASA.: Standard tests for toughened resin composites. Technical report, Langley Research Center, Virginia, USA (1982)

52.

O’Brien, T.: Mixed-mode strain energy-release rate effects on edge delamination of composites. In: 836 AS (ed.) Effects of Defects in Composite Materials. American Society for Testing and Materials, pp. 125–142 (1984)

53.

Olsson, R.: Review—a survey of test methods for multiaxial and out-of-plane strength of composite laminates. Compos. Sci. Technol. 71, 773–783 (2011)CrossRefMathSciNet

54.

Ozdil, F., Carlsson, L.: Beam analysis of angle-ply laminate DCB specimens. Compos. Sci. Technol. 59, 305–315 (1999)CrossRef

55.

Pereira, A., de Morais, A.: Mixed-mode I + II interlaminar fracture of glass/epoxy multidirectional laminates—part 2: experiments. Compos. Sci. Technol. 66, 1896–1902 (2006)CrossRef

56.

Pereira, A., de Morais, A.: Mixed-mode I + II interlaminar fracture of carbon/epoxy laminates. Compos. Part A Appl. Sci. Manuf. 39, 322–333 (2008)CrossRef

57.

Pereira, A., de Morais, A.: Mixed-mode I+III interlaminar fracture of carbon/epoxy laminates. Compos. Part A Appl. Sci. Manuf. 40, 518–523 (2009)CrossRef

58.

Pinho, S., Iannucci, L., Robinson, P.: Formulation and implementation of decohesion elements in an explicit finite element code. Compos. Part A Appl. Sci. Manuf. 37, 778–789 (2006)CrossRef

59.

Prombut, P.: Caractâ€šrisation de la propagation de délaminage des stratifiés composites multidirectionnels. Ph.D. thesis, University of Toulouse III—Paul Sabatier, France (2007)

60.

Prombut, P., Michel, L., Lachaud, F., Barrau, J.J.: Delamination of multidirectional composite laminates at 0/± ply interfaces. Eng. Fract. Mech. 73, 2427–2442 (2006)CrossRef

61.

Reeder, J., Crews, J.: Mixed-mode bending method for delamination testing. AIAA J. 28, 1270–1276 (1990)CrossRef

62.

Reeder, J., Crews, J.: Redesign of the mixed-mode bending delamination test to reduce nonlinear effects. J. Compos. Technol. Res. 14, 12–19 (1992)CrossRef

63.

Reeder, J.: An evaluation of mixed-mode delamination failure criteria. Technical report, Langley Research Center, Virginia, USA (1992)

64.

Schuecker, C., Davidson, B.: Evaluation of the accuracy of the four-point bend end-notched flexure test for mode II delamination toughness determination. Compos. Sci. Technol. 60, 2137–2146 (2000)CrossRef

65.

Sun, C., Zheng, S.: Delamination characteristics of double-cantilever beam and end-notched flexure composite specimens. Compos. Sci. Technol. 56, 451–459 (1996)CrossRef

66.

Talreja, R.: Stiffness properties of composite laminates with matrix cracking and interior delamination. Eng. Fract. Mech. 25(5), 751–762 (1986)CrossRef

67.

Thionnet, A., Renard. J.: Meso-macro approach to transverse cracking in laminated composites using Talreja’s model. Compos. Eng. 3(9), 851–871 (1993). doi:10.1016/0961-9526(93)90044-K. URL http://www.sciencedirect.com/science/article/pii/096195269390044K

68.

Turon, A.: Simulation of delamination in composites under quasi-static and fatigue loading using cohesive zone models. Ph.D. thesis, Department d’Enginyeria Mecánica i de la Construcció Industrial, Universitat de Girona, Spain (2006)

69.

Turon, A., Dávila, C., Camanho, P., Costa, J.: An engineering solution for mesh size effects in the simulation of delamination using cohesive zone models. Eng. Fract. Mech. 74, 1665–1682 (2007)CrossRef

70.

Turon, A., Camanho, P., Costa, J., Renart, J.: Accurate simulation of delamination growth under mixed-mode loading using cohesive elements: definition of intralaminar strengths and elastic stiffness. Compos. Struct. 92, 1857–1864 (2010)CrossRef

71.

Vandellos, T., Hautier, M., Carrère, N., Huchette, C.: Development of a new fracture test to identify the critical energy release rate: the tensile flexure test on notched specimen. Eng. Fract. Mech. 96, 641–655 (2012)CrossRef

72.

Vandellos, T., Huchette, C., Carrère, N.: Proposition of a framework for the development of a cohesive zone model adapted to carbon-fiber reinforced plastic laminated composites. Compos. Struct. 105, 199–206 (2013)CrossRef

73.

Whitcomb, J.: Analysis of instability-related growth of a through-width delamination. Technical report, Langley Research Center, Virginia, USA (1984)

74.

Wisnom, M., Hallett, S.: The role of delamination in strength, failure mechanism and hole size effect in open hole tensile tests on quasi-isotropic laminates. Compos. Part A Appl. Sci. Manuf. 40, 335–342 (2009)CrossRef

75.

Zébulon (2014). URL http://www.zset-software.com/products/zebulon/

Titel: Influence of Intralaminar Damage on the Delamination Crack Evolution
verfasst von: Cédric Huchette
Thomas Vandellos
Frédéric Laurin
Verlag: Springer International Publishing
Buch: Damage Growth in Aerospace Composites
Print ISBN: 978-3-319-04003-5

Electronic ISBN: 978-3-319-04004-2

Copyright-Jahr: 2015
DOI: https://doi.org/10.1007/978-3-319-04004-2_5

Springer Professional

Abstract

Bitte loggen Sie sich ein, um Zugang zu Ihrer Lizenz zu erhalten.

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Springer Professional "Technik"

Premium Partner