Skip to main content

2019 | OriginalPaper | Buchkapitel

6. Post-buckling Progressive Failure Analysis of Composite Panels Using a Two-Way Global-Local Coupling Approach Including Intralaminar Failure and Debonding

verfasst von : M. Akterskaia, E. Jansen, S. R. Hallet, P. M. Weaver, R. Rolfes

Erschienen in: Advances in Predictive Models and Methodologies for Numerically Efficient Linear and Nonlinear Analysis of Composites

Verlag: Springer International Publishing

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

search-config
loading …

Abstract

A novel two-way global-local coupling approach to model progressive separation of skin and stringer in combination with intralaminar damage in stiffened CFRP panels under compression is presented. The methodology makes it possible to examine the damage at two levels of accuracy, taking advantage of fast calculations at the global level and assessing in detail the damage propagation at the local level. The required appropriate information exchange between the global and local level in both directions has been attained. This chapter presents an overview of this efficient approach for progressive failure analysis of composite panels and illustrates the approach on the basis of a one-stringer panel, in particular for the case of skin-stringer debonding.

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!

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!

Literatur
1.
Zurück zum Zitat Abaqus 6.14 Documentation (2017) Dassault systemes 6.14 edn (V):1–172 Abaqus 6.14 Documentation (2017) Dassault systemes 6.14 edn (V):1–172
2.
Zurück zum Zitat Akterskaia M, Jansen E, Hühne S, Rolfes R (2018) Efficient progressive failure analysis of multi-stringer stiffened composite panels through a two-way loose coupling global-local approach. Compos Struct 183:137–145CrossRef Akterskaia M, Jansen E, Hühne S, Rolfes R (2018) Efficient progressive failure analysis of multi-stringer stiffened composite panels through a two-way loose coupling global-local approach. Compos Struct 183:137–145CrossRef
3.
Zurück zum Zitat Akterskaia M, Jansen E, Hallett SR, Weaver R, Raimund R (2018) Analysis of skin-stringer debonding in composite panels through a two-way global-local method. Compos Struct 202:1280–1294CrossRef Akterskaia M, Jansen E, Hallett SR, Weaver R, Raimund R (2018) Analysis of skin-stringer debonding in composite panels through a two-way global-local method. Compos Struct 202:1280–1294CrossRef
4.
Zurück zum Zitat Akterskaia M, Jansen E, Hallett SR, Weaver R, Raimund R (2018) Progressive failure analysis of stiffened composite panels using a two-way loose coupling approach including intralaminar failure and debonding. In: AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference, pp 1–16 Akterskaia M, Jansen E, Hallett SR, Weaver R, Raimund R (2018) Progressive failure analysis of stiffened composite panels using a two-way loose coupling approach including intralaminar failure and debonding. In: AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference, pp 1–16
5.
Zurück zum Zitat Alesi H, Nguyen VM, Mileshkin M, Jones R (1998) Global/local postbuckling failure analysis of composite stringer/skin panels. AIAA J 36(9):1699–1705CrossRef Alesi H, Nguyen VM, Mileshkin M, Jones R (1998) Global/local postbuckling failure analysis of composite stringer/skin panels. AIAA J 36(9):1699–1705CrossRef
6.
Zurück zum Zitat Allix O, Ladevèze P (1992) Interlaminar interface modelling for the prediction of laminate delamination. Compos Struct 22:235–242CrossRef Allix O, Ladevèze P (1992) Interlaminar interface modelling for the prediction of laminate delamination. Compos Struct 22:235–242CrossRef
7.
Zurück zum Zitat Balzani C, Wagner W (2010) Numerical treatment of damage propagation in axially compressed composite airframe panels. Int J Struct Stab Dyn 10(4):683–703CrossRef Balzani C, Wagner W (2010) Numerical treatment of damage propagation in axially compressed composite airframe panels. Int J Struct Stab Dyn 10(4):683–703CrossRef
8.
Zurück zum Zitat Barenblatt GI (1962) The mathematical theory of equilibrium cracks in brittle fracture. Adv Appl Mech 7(C):55–129 Barenblatt GI (1962) The mathematical theory of equilibrium cracks in brittle fracture. Adv Appl Mech 7(C):55–129
9.
Zurück zum Zitat Benzeggagh ML, Kenane M (1996) Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus. Compos Sci Technol 56:439–449CrossRef Benzeggagh ML, Kenane M (1996) Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus. Compos Sci Technol 56:439–449CrossRef
10.
Zurück zum Zitat Bertolini J, Castanié B, Barrau JJ, Navarro JP, Petiot C (2009) Multi-level experimental and numerical analysis of composite stiffener debonding. Part 2: element and panel level. Compos Struct 90(4):392–403CrossRef Bertolini J, Castanié B, Barrau JJ, Navarro JP, Petiot C (2009) Multi-level experimental and numerical analysis of composite stiffener debonding. Part 2: element and panel level. Compos Struct 90(4):392–403CrossRef
11.
Zurück zum Zitat Bettinotti O, Allix O, Perego U, Oancea V, Malherbe B (2017) Simulation of delamination under impact using a global-local method in explicit dynamics. Finite Elem Anal Des 125:1–13CrossRef Bettinotti O, Allix O, Perego U, Oancea V, Malherbe B (2017) Simulation of delamination under impact using a global-local method in explicit dynamics. Finite Elem Anal Des 125:1–13CrossRef
12.
Zurück zum Zitat Borg R, Nilsson L, Simonsson K (2001) Simulation of delamination in fiber composites with a discrete cohesive failure model. Compos Sci Technol 61(5):667–677CrossRef Borg R, Nilsson L, Simonsson K (2001) Simulation of delamination in fiber composites with a discrete cohesive failure model. Compos Sci Technol 61(5):667–677CrossRef
13.
Zurück zum Zitat Camanho PP, Dávila CG (2002) Mixed-mode decohesion finite elements for the simulation of delamination in composite materials. Technical memorandum TM-2002-211737. Hampton, VI 23681-2199, NASA, Langley Research Center, USA Camanho PP, Dávila CG (2002) Mixed-mode decohesion finite elements for the simulation of delamination in composite materials. Technical memorandum TM-2002-211737. Hampton, VI 23681-2199, NASA, Langley Research Center, USA
14.
Zurück zum Zitat Chrupalla D, Berg S, Kärger L, Doreille M, Ludwig T, Jansen E, Rolfes R, Kling A (2011) A homogenization-based two-way multiscale approach for composite structures. In: Rolfes R, Jansen EL (eds) Proceedings of the 3rd ECCOMAS thematic conference on the mechanical response of composites, Hannover, Germany, pp 263–270 Chrupalla D, Berg S, Kärger L, Doreille M, Ludwig T, Jansen E, Rolfes R, Kling A (2011) A homogenization-based two-way multiscale approach for composite structures. In: Rolfes R, Jansen EL (eds) Proceedings of the 3rd ECCOMAS thematic conference on the mechanical response of composites, Hannover, Germany, pp 263–270
15.
Zurück zum Zitat Dávila CG, Camanho PP, de Moura M (2001) Mixed-mode decohesion elements for analyses of proressive delamination. In: 19th AIAA applied aerodynamics conference Dávila CG, Camanho PP, de Moura M (2001) Mixed-mode decohesion elements for analyses of proressive delamination. In: 19th AIAA applied aerodynamics conference
16.
Zurück zum Zitat Degenhardt R, Kling A, Klein H, Hillger W, Goetting HC, Zimmermann R, Rohwer K (2007) Experiments on buckling and postbuckling of thin-walled CFRP structures using advanced measurement systems. Int J Struct Stab Dyn 7(2):337–358CrossRef Degenhardt R, Kling A, Klein H, Hillger W, Goetting HC, Zimmermann R, Rohwer K (2007) Experiments on buckling and postbuckling of thin-walled CFRP structures using advanced measurement systems. Int J Struct Stab Dyn 7(2):337–358CrossRef
17.
Zurück zum Zitat Dugdale DS (1960) Yielding of steel sheets containing slits. J Mech Phys Solids 8:100–104CrossRef Dugdale DS (1960) Yielding of steel sheets containing slits. J Mech Phys Solids 8:100–104CrossRef
18.
Zurück zum Zitat Faggiani A, Falzon BG (2007) Optimization strategy for minimizing damage in postbuckling stiffened panels. AIAA J 45(10):2520–2528CrossRef Faggiani A, Falzon BG (2007) Optimization strategy for minimizing damage in postbuckling stiffened panels. AIAA J 45(10):2520–2528CrossRef
19.
Zurück zum Zitat Falzon BG, Stevens KA, Davies GO (2000) Postbuckling behaviour of a blade-stiffened composite panel loaded in uniaxial compression. Compos Part A 31:459–468CrossRef Falzon BG, Stevens KA, Davies GO (2000) Postbuckling behaviour of a blade-stiffened composite panel loaded in uniaxial compression. Compos Part A 31:459–468CrossRef
20.
Zurück zum Zitat Falzon BG, Davies GAO, Greenhalgh E (2001) Failure of thick-skinned stiffener runout sections loaded in uniaxial compression. Compos Struct 53:223–233CrossRef Falzon BG, Davies GAO, Greenhalgh E (2001) Failure of thick-skinned stiffener runout sections loaded in uniaxial compression. Compos Struct 53:223–233CrossRef
21.
Zurück zum Zitat Hallett SR, Wisnom MR (2006) Numerical investigation of progressive damage and the effect of layup in notched tensile tests. J Compos Mater 40(14):1229–1245CrossRef Hallett SR, Wisnom MR (2006) Numerical investigation of progressive damage and the effect of layup in notched tensile tests. J Compos Mater 40(14):1229–1245CrossRef
22.
Zurück zum Zitat Hillerborg A, Modeer M, Petersson PE (1976) Analysis of crack formation and crack growth in concrete by means of fracture mechanics and finite elements. Cement Concrete Res 6:773–782CrossRef Hillerborg A, Modeer M, Petersson PE (1976) Analysis of crack formation and crack growth in concrete by means of fracture mechanics and finite elements. Cement Concrete Res 6:773–782CrossRef
23.
Zurück zum Zitat Hinton MJ, Kaddour AS, Soden PD (2002) A comparison of the predictive capabilities of current failure theories for composite laminates, judged against experimental evidence. Compos Sci Technol 62:1725–1797CrossRef Hinton MJ, Kaddour AS, Soden PD (2002) A comparison of the predictive capabilities of current failure theories for composite laminates, judged against experimental evidence. Compos Sci Technol 62:1725–1797CrossRef
24.
Zurück zum Zitat Hühne S, Reinoso J, Jansen E, Rolfes R (2016) A two-way loose coupling procedure for investigating the buckling and damage behaviour of stiffened composite panels. Compos Struct 136:513–525CrossRef Hühne S, Reinoso J, Jansen E, Rolfes R (2016) A two-way loose coupling procedure for investigating the buckling and damage behaviour of stiffened composite panels. Compos Struct 136:513–525CrossRef
25.
Zurück zum Zitat Jiang WG, Hallett SR, Green BG, Wisnom MR (2007) A concise interface constitutive law for analysis of delamination and splitting in composite materials and its application to scaled notched tensile specimens. Int J Numer Methods Eng 69(9):1982–1995CrossRef Jiang WG, Hallett SR, Green BG, Wisnom MR (2007) A concise interface constitutive law for analysis of delamination and splitting in composite materials and its application to scaled notched tensile specimens. Int J Numer Methods Eng 69(9):1982–1995CrossRef
26.
Zurück zum Zitat Jones RM (1998) Mechanics of composite materials. CRC Press, Boca Raton Jones RM (1998) Mechanics of composite materials. CRC Press, Boca Raton
27.
Zurück zum Zitat Kaddour AS, Hinton MJ (2013) Maturity of 3D failure criteria for fibre-reinforced composites: comparison between theories and experiments: Part B of WWFE-II. J Compos Mater 47:925–966CrossRef Kaddour AS, Hinton MJ (2013) Maturity of 3D failure criteria for fibre-reinforced composites: comparison between theories and experiments: Part B of WWFE-II. J Compos Mater 47:925–966CrossRef
28.
Zurück zum Zitat Kaddour AS, Hinton MJ, Soden PD (2004) A comparison of the predictive capabilities of current failure theories for composite laminates: additional contributions. Compos Sci Technol 64:449–476CrossRef Kaddour AS, Hinton MJ, Soden PD (2004) A comparison of the predictive capabilities of current failure theories for composite laminates: additional contributions. Compos Sci Technol 64:449–476CrossRef
29.
Zurück zum Zitat Kaddour AS, Hinton MJ, Smith PA, Li S (2013) Mechanical properties and details of composite laminates for the test cases used in the third world-wide failure exercise. J Compos Mater 47(20–21):2427–2442CrossRef Kaddour AS, Hinton MJ, Smith PA, Li S (2013) Mechanical properties and details of composite laminates for the test cases used in the third world-wide failure exercise. J Compos Mater 47(20–21):2427–2442CrossRef
30.
Zurück zum Zitat Krueger R (2015) The virtual crack closure technique for modeling interlaminar failure and delamination in advanced composite materials. Woodhead publishing series in composites science and engineering, pp 3–53 Krueger R (2015) The virtual crack closure technique for modeling interlaminar failure and delamination in advanced composite materials. Woodhead publishing series in composites science and engineering, pp 3–53
31.
Zurück zum Zitat Labeas GN, Belesis SD, Diamantakos I, Tserpes KI (2012) Adaptative progressive damage modeling for large-scale composite structures. Int J Damage Mech 21(3):441–462CrossRef Labeas GN, Belesis SD, Diamantakos I, Tserpes KI (2012) Adaptative progressive damage modeling for large-scale composite structures. Int J Damage Mech 21(3):441–462CrossRef
32.
Zurück zum Zitat Lauterbach S, Orifici AC, Wagner W, Balzani C, Abramovich H, Thomson R (2010) Damage sensitivity of axially loaded stringer-stiffened curved CFRP panels. Compos Sci Technol 70(2):240–248CrossRef Lauterbach S, Orifici AC, Wagner W, Balzani C, Abramovich H, Thomson R (2010) Damage sensitivity of axially loaded stringer-stiffened curved CFRP panels. Compos Sci Technol 70(2):240–248CrossRef
33.
Zurück zum Zitat Linde P, Pleitner J, Boer H, Carmone C (2004) Modelling and simulation of fibre metal laminates. In: ABAQUS users’ conference, pp 421–439 Linde P, Pleitner J, Boer H, Carmone C (2004) Modelling and simulation of fibre metal laminates. In: ABAQUS users’ conference, pp 421–439
34.
Zurück zum Zitat Loehnert S, Belytschko T (2007) A multiscale projection method for macro/microcrack simulations. Int J Numer Methods Eng 71:1466–1482MathSciNetCrossRef Loehnert S, Belytschko T (2007) A multiscale projection method for macro/microcrack simulations. Int J Numer Methods Eng 71:1466–1482MathSciNetCrossRef
35.
Zurück zum Zitat Mao KM, Sun CT (1991) A refined global-local finite element analysis method. Int J Numer Methods Eng 32:29–43CrossRef Mao KM, Sun CT (1991) A refined global-local finite element analysis method. Int J Numer Methods Eng 32:29–43CrossRef
37.
Zurück zum Zitat Noor AK (1986) Global-local methodologies and their application to nonlinear analysis. Finite Elem Anal Des 2:333–346CrossRef Noor AK (1986) Global-local methodologies and their application to nonlinear analysis. Finite Elem Anal Des 2:333–346CrossRef
38.
Zurück zum Zitat Orifici AC, Ortiz I, Alberdi DZ, Thomson RS, Bayandor J (2008) Compression and post-buckling damage growth and collapse analysis of flat composite stiffened panels. Compos Sci Technol 68(15–16):3150–3160CrossRef Orifici AC, Ortiz I, Alberdi DZ, Thomson RS, Bayandor J (2008) Compression and post-buckling damage growth and collapse analysis of flat composite stiffened panels. Compos Sci Technol 68(15–16):3150–3160CrossRef
39.
Zurück zum Zitat Reinoso J, Blázquez A, Estefani A, París F, Cañas J, Arévalo E, Cruz F (2012) Experimental and three-dimensional global-local finite element analysis of a composite component including degradation process at the interfaces. Compos Part B 43(4):1929–1942CrossRef Reinoso J, Blázquez A, Estefani A, París F, Cañas J, Arévalo E, Cruz F (2012) Experimental and three-dimensional global-local finite element analysis of a composite component including degradation process at the interfaces. Compos Part B 43(4):1929–1942CrossRef
40.
Zurück zum Zitat Riccio A, Raimondo A (2016) Inter-laminar and intra-laminar damage evolution in composite panels with skin-stringer debonding under compression. Compos Part B 94:139–151CrossRef Riccio A, Raimondo A (2016) Inter-laminar and intra-laminar damage evolution in composite panels with skin-stringer debonding under compression. Compos Part B 94:139–151CrossRef
41.
Zurück zum Zitat Riccio A, Raimondo A, Scaramuzzino F (2015) A robust numerical approach for the simulation of skin-stringer debonding growth in stiffened composite panels under compression. Compos Part B 71:131–142CrossRef Riccio A, Raimondo A, Scaramuzzino F (2015) A robust numerical approach for the simulation of skin-stringer debonding growth in stiffened composite panels under compression. Compos Part B 71:131–142CrossRef
42.
Zurück zum Zitat Rybicki EF, Kanninen MF (1997) A finite element calculation of stress intensity factors by modified crack closure integral. Eng Fract Mech 9:931–938CrossRef Rybicki EF, Kanninen MF (1997) A finite element calculation of stress intensity factors by modified crack closure integral. Eng Fract Mech 9:931–938CrossRef
43.
Zurück zum Zitat Turon A, Camanho PP (2006) A damage model for the simulation of delamination in advanced composites under variable-mode loading. Mech Mater 38:1072–1089CrossRef Turon A, Camanho PP (2006) A damage model for the simulation of delamination in advanced composites under variable-mode loading. Mech Mater 38:1072–1089CrossRef
44.
Zurück zum Zitat Turon A, Camanho PP, Costa J (2007) An engineering solution for mesh size effects in the simulation of delamination using cohesive zone models. Eng Fract Mech 74:1665–1682CrossRef Turon A, Camanho PP, Costa J (2007) An engineering solution for mesh size effects in the simulation of delamination using cohesive zone models. Eng Fract Mech 74:1665–1682CrossRef
45.
Zurück zum Zitat Wang JTS, Bigger SB (1984) Skin-stiffener interface stresses in composite stiffened panels. NASA Contractor Report 172261 Wang JTS, Bigger SB (1984) Skin-stiffener interface stresses in composite stiffened panels. NASA Contractor Report 172261
46.
Zurück zum Zitat Whitcomb JD (1991) Iterative global/local finite element analysis. Comput Struct 40(4):1027–1031CrossRef Whitcomb JD (1991) Iterative global/local finite element analysis. Comput Struct 40(4):1027–1031CrossRef
47.
Zurück zum Zitat Wisnom MR, Chang FK (2000) Modelling of splitting and delamination in notched cross-ply laminates. Compos Sci Technol 60(15):2849–2856CrossRef Wisnom MR, Chang FK (2000) Modelling of splitting and delamination in notched cross-ply laminates. Compos Sci Technol 60(15):2849–2856CrossRef
48.
Zurück zum Zitat Xie D, Waas AM (2006) Discrete cohesive zone model for mixed-mode fracture using finite element analysis. Eng Fract Mech 73(13):1783–1796CrossRef Xie D, Waas AM (2006) Discrete cohesive zone model for mixed-mode fracture using finite element analysis. Eng Fract Mech 73(13):1783–1796CrossRef
49.
Zurück zum Zitat Yap JWH, Scott ML, Thomson RS, Hachenberg D (2002) The analysis of skin-to-stiffener debonding in composite aerospace structures. Compos Struct 57:425–435CrossRef Yap JWH, Scott ML, Thomson RS, Hachenberg D (2002) The analysis of skin-to-stiffener debonding in composite aerospace structures. Compos Struct 57:425–435CrossRef
50.
Zurück zum Zitat Zubillaga L, Turon A, Renart J, Costa J, Linde P (2015) An experimental study on matrix crack induced delamination in composite laminates. Compos Struct 127:10–17CrossRef Zubillaga L, Turon A, Renart J, Costa J, Linde P (2015) An experimental study on matrix crack induced delamination in composite laminates. Compos Struct 127:10–17CrossRef
Metadaten
Titel
Post-buckling Progressive Failure Analysis of Composite Panels Using a Two-Way Global-Local Coupling Approach Including Intralaminar Failure and Debonding
verfasst von
M. Akterskaia
E. Jansen
S. R. Hallet
P. M. Weaver
R. Rolfes
Copyright-Jahr
2019
DOI
https://doi.org/10.1007/978-3-030-11969-0_6

    Marktübersichten

    Die im Laufe eines Jahres in der „adhäsion“ veröffentlichten Marktübersichten helfen Anwendern verschiedenster Branchen, sich einen gezielten Überblick über Lieferantenangebote zu verschaffen.