메뉴 건너뛰기




Volumn 68, Issue 15-16, 2008, Pages 3150-3160

Compression and post-buckling damage growth and collapse analysis of flat composite stiffened panels

Author keywords

B. Debonding; C. Buckling; C. Damage mechanics; C. Delamination; C. Finite element analysis

Indexed keywords

BUCKLING; CRACK CLOSURE; CRACKING (CHEMICAL); DATA COMPRESSION; DEFORMATION; DEGRADATION; FAILURE ANALYSIS; FORECASTING; JOINTS (STRUCTURAL COMPONENTS); MACHINE DESIGN; NUMERICAL ANALYSIS; QUALITY ASSURANCE; SKIN;

EID: 55649088003     PISSN: 02663538     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compscitech.2008.07.017     Document Type: Article
Times cited : (121)

References (27)
  • 1
    • 55649106451 scopus 로고    scopus 로고
    • Camanho PP, Dávila CG. Mixed-mode decohesion finite elements for the simulation of delamination in composite materials. NASA/TM-2002-211737, VA, USA: NASA Langley Research Center; 2002.
    • Camanho PP, Dávila CG. Mixed-mode decohesion finite elements for the simulation of delamination in composite materials. NASA/TM-2002-211737, VA, USA: NASA Langley Research Center; 2002.
  • 2
    • 0026715451 scopus 로고
    • Damage modelling of the elementary ply for laminated composites
    • Ladeveze P., and Le Dantec E. Damage modelling of the elementary ply for laminated composites. J Compos Sci Technol 43 (1992) 257-267
    • (1992) J Compos Sci Technol , vol.43 , pp. 257-267
    • Ladeveze, P.1    Le Dantec, E.2
  • 3
    • 0023420567 scopus 로고
    • A progressive damage model for laminated composites containing stress concentrations
    • Chang F.K., and Chang K.Y. A progressive damage model for laminated composites containing stress concentrations. J Compos Mater 21 (1987) 834-855
    • (1987) J Compos Mater , vol.21 , pp. 834-855
    • Chang, F.K.1    Chang, K.Y.2
  • 4
    • 0032125046 scopus 로고    scopus 로고
    • Failure analysis of FRP laminates by means of physically based phenomenological models
    • Puck A., and Schürmann H. Failure analysis of FRP laminates by means of physically based phenomenological models. J Compos Sci Technol 58 (1998) 1045-1067
    • (1998) J Compos Sci Technol , vol.58 , pp. 1045-1067
    • Puck, A.1    Schürmann, H.2
  • 5
    • 32044446233 scopus 로고    scopus 로고
    • Buckling and postbuckling of stringer stiffened fibre composite curved panels - tests and computations
    • Zimmermann R., Klein H., and Kling A. Buckling and postbuckling of stringer stiffened fibre composite curved panels - tests and computations. Compos Struct 73 (2006) 150-161
    • (2006) Compos Struct , vol.73 , pp. 150-161
    • Zimmermann, R.1    Klein, H.2    Kling, A.3
  • 6
    • 17644365142 scopus 로고    scopus 로고
    • Stiffener debonding mechanisms in post-buckled CFRP aerospace panels
    • Meeks C., Greenhalgh E., and Falzon B.G. Stiffener debonding mechanisms in post-buckled CFRP aerospace panels. Compos A: Appl Sci Manuf 36 7 (2005) 934-946
    • (2005) Compos A: Appl Sci Manuf , vol.36 , Issue.7 , pp. 934-946
    • Meeks, C.1    Greenhalgh, E.2    Falzon, B.G.3
  • 7
    • 55649102889 scopus 로고    scopus 로고
    • Krueger R, Minguet PJ. Skin-stiffener debond prediction based on computational fracture analysis. NASA/CR-2005-213915, NASA Langley Research Center, VA, USA; 2005.
    • Krueger R, Minguet PJ. Skin-stiffener debond prediction based on computational fracture analysis. NASA/CR-2005-213915, NASA Langley Research Center, VA, USA; 2005.
  • 8
    • 44349164511 scopus 로고    scopus 로고
    • Prediction of flange debonding in composite stiffened panels using an analytical crack tip element-based methodology
    • Mikulik Z., Kelly D.W., Prusty B.G., and Thomson R.S. Prediction of flange debonding in composite stiffened panels using an analytical crack tip element-based methodology. Compos Struct 85 3 (2008) 233-244
    • (2008) Compos Struct , vol.85 , Issue.3 , pp. 233-244
    • Mikulik, Z.1    Kelly, D.W.2    Prusty, B.G.3    Thomson, R.S.4
  • 10
    • 32044471533 scopus 로고    scopus 로고
    • COCOMAT - improved material exploitation of composite airframe structures by accurate simulation of postbuckling and collapse
    • Degenhardt R., Rolfes R., Zimmermann R., and Rohwer K. COCOMAT - improved material exploitation of composite airframe structures by accurate simulation of postbuckling and collapse. Compos Struct 73 (2006) 8-175
    • (2006) Compos Struct , vol.73 , pp. 8-175
    • Degenhardt, R.1    Rolfes, R.2    Zimmermann, R.3    Rohwer, K.4
  • 11
    • 55649091302 scopus 로고    scopus 로고
    • COCOMAT Home Page, http://www.cocomat.de; 2008.
    • COCOMAT Home Page, http://www.cocomat.de; 2008.
  • 12
    • 55649096327 scopus 로고    scopus 로고
    • Orifici AC, Thomson RS, Degenhardt R, Bayandor J. Development of a finite element methodology for the collapse analysis of composite aerospace structures. In: Proceedings of the ECCOMAS thematic conference on mechanical response of composites, Porto, Portugal, 12-14 September, 2007.
    • Orifici AC, Thomson RS, Degenhardt R, Bayandor J. Development of a finite element methodology for the collapse analysis of composite aerospace structures. In: Proceedings of the ECCOMAS thematic conference on mechanical response of composites, Porto, Portugal, 12-14 September, 2007.
  • 13
    • 55649114744 scopus 로고    scopus 로고
    • Orifici AC. Degradation models for the collapse analysis of composite aerospace structures. Ph.D. thesis, Royal Melbourne Institute of Technology; 2007.
    • Orifici AC. Degradation models for the collapse analysis of composite aerospace structures. Ph.D. thesis, Royal Melbourne Institute of Technology; 2007.
  • 14
    • 0030712526 scopus 로고    scopus 로고
    • An assessment of failure criteria to predict the strength of adhesively bonded double lap joints
    • Tong L. An assessment of failure criteria to predict the strength of adhesively bonded double lap joints. J Reinf Plas Comp 16 (1997) 698-715
    • (1997) J Reinf Plas Comp , vol.16 , pp. 698-715
    • Tong, L.1
  • 15
    • 55649113423 scopus 로고    scopus 로고
    • Orifici AC, Herszberg I, Thomson RS, Weller T, Kotler A, Bayandor J. Failure in stringer interfaces in postbuckled composite stiffened panels. In: Proceedings of the 12th Australian international aerospace congress, Melbourne, Australia, 19-22 March, 2007.
    • Orifici AC, Herszberg I, Thomson RS, Weller T, Kotler A, Bayandor J. Failure in stringer interfaces in postbuckled composite stiffened panels. In: Proceedings of the 12th Australian international aerospace congress, Melbourne, Australia, 19-22 March, 2007.
  • 16
    • 0003684655 scopus 로고
    • Failure criteria for unidirectional composites
    • Hashin Z. Failure criteria for unidirectional composites. J Appl Mech 47 (1980) 34-329
    • (1980) J Appl Mech , vol.47 , pp. 34-329
    • Hashin, Z.1
  • 17
    • 0025741967 scopus 로고
    • Damage tolerance of laminated composites containing an open hole and subject to compressive loadings: part I analysis
    • Chang F.K., and Lessard L.B. Damage tolerance of laminated composites containing an open hole and subject to compressive loadings: part I analysis. J Comp Mat 25 (1991) 2-43
    • (1991) J Comp Mat , vol.25 , pp. 2-43
    • Chang, F.K.1    Lessard, L.B.2
  • 18
    • 34147186652 scopus 로고    scopus 로고
    • Development of a finite element methodology for the propagation of delaminations in composite structures
    • Orifici A.C., Thomson R.S., Degenhardt R., Bisagni C., and Bayandor J. Development of a finite element methodology for the propagation of delaminations in composite structures. Mech Comp Mat 43 1 (2007) 9-28
    • (2007) Mech Comp Mat , vol.43 , Issue.1 , pp. 9-28
    • Orifici, A.C.1    Thomson, R.S.2    Degenhardt, R.3    Bisagni, C.4    Bayandor, J.5
  • 19
    • 55649109291 scopus 로고    scopus 로고
    • Orifici AC, Thomson RS, Degenhardt R, Büsing S, Bayandor J. Development of a finite element methodology for modelling mixed-mode delamination growth in composite structures. In: Proceedings of the 12th Australian international aerospace congress, Melbourne, Australia, 19-22 March 2007.
    • Orifici AC, Thomson RS, Degenhardt R, Büsing S, Bayandor J. Development of a finite element methodology for modelling mixed-mode delamination growth in composite structures. In: Proceedings of the 12th Australian international aerospace congress, Melbourne, Australia, 19-22 March 2007.
  • 20
    • 0017561766 scopus 로고
    • A finite element calculation of stress intensity factors by a modified crack closure integral
    • Rybicki E.F., and Kanninen M.F. A finite element calculation of stress intensity factors by a modified crack closure integral. Eng Fract Mech 9 (1977) 8-931
    • (1977) Eng Fract Mech , vol.9 , pp. 8-931
    • Rybicki, E.F.1    Kanninen, M.F.2
  • 21
    • 55649091130 scopus 로고    scopus 로고
    • Krueger R. The virtual crack closure technique: history, approach and applications. NASA/CR-2002-211628, ICASE Virginia, USA; 2002.
    • Krueger R. The virtual crack closure technique: history, approach and applications. NASA/CR-2002-211628, ICASE Virginia, USA; 2002.
  • 22
    • 0030111809 scopus 로고    scopus 로고
    • Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus
    • Benzeggagh M.L., and Kenane M. Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus. Compos Sci Tech 56 (1996) 49-439
    • (1996) Compos Sci Tech , vol.56 , pp. 49-439
    • Benzeggagh, M.L.1    Kenane, M.2
  • 23
    • 55649091526 scopus 로고    scopus 로고
    • Hansen P, Martin R. DCB, 4ENF and MMB delamination characterisation of S2/8552 and IM7/8552. Materials Engineering Research Laboratory Ltd. (MERL), Hertford, UK, N68171-98-M-5177; 1999.
    • Hansen P, Martin R. DCB, 4ENF and MMB delamination characterisation of S2/8552 and IM7/8552. Materials Engineering Research Laboratory Ltd. (MERL), Hertford, UK, N68171-98-M-5177; 1999.
  • 24
    • 34250770504 scopus 로고    scopus 로고
    • Experiments on buckling and postbuckling of thin-walled CFRP structures using advanced measurement systems
    • Degenhardt R., Kling A., Klein H., Hillger W., Goetting H.C., Zimmermann R., et al. Experiments on buckling and postbuckling of thin-walled CFRP structures using advanced measurement systems. Int J Struct Stab Dyn 7 (2007) 58-337
    • (2007) Int J Struct Stab Dyn , vol.7 , pp. 58-337
    • Degenhardt, R.1    Kling, A.2    Klein, H.3    Hillger, W.4    Goetting, H.C.5    Zimmermann, R.6
  • 25
    • 3042790015 scopus 로고    scopus 로고
    • Dependence of fracture toughness of composite laminates on interface ply orientations and delamination growth direction
    • Andersons J., and König M. Dependence of fracture toughness of composite laminates on interface ply orientations and delamination growth direction. Compos Sci Tech 64 (2004) 52-2139
    • (2004) Compos Sci Tech , vol.64 , pp. 52-2139
    • Andersons, J.1    König, M.2
  • 26
    • 55649102419 scopus 로고    scopus 로고
    • Krueger R, Ratcliffe J, Minguet PJ. Analysis of composite panel-stiffener debonding using a shell/3D modelling technique, NASA/CR-2007-214879, NASA Langley Research Center, VA, USA; 2007.
    • Krueger R, Ratcliffe J, Minguet PJ. Analysis of composite panel-stiffener debonding using a shell/3D modelling technique, NASA/CR-2007-214879, NASA Langley Research Center, VA, USA; 2007.
  • 27
    • 0038218500 scopus 로고    scopus 로고
    • Capturing mode-switching in postbuckling composite panels using a modified explicit procedure
    • Falzon B.G., and Hitchings D. Capturing mode-switching in postbuckling composite panels using a modified explicit procedure. Compos Struct 60 (2003) 447-453
    • (2003) Compos Struct , vol.60 , pp. 447-453
    • Falzon, B.G.1    Hitchings, D.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.