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Volumn 15, Issue 5, 2002, Pages 429-442

Predicting progressive delamination of stiffened fibre-composite panel and repaired sandwich panel by decohesion models

Author keywords

Composite materials and repairs; Delamination growth; Interface finite element; Interfacial decohesion models; Mixed damage scale

Indexed keywords

COMPOSITE MATERIALS; COMPUTER SIMULATION; CRACK PROPAGATION; DELAMINATION; FAILURE ANALYSIS; FRACTURE MECHANICS; MATHEMATICAL MODELS; REPAIR; SANDWICH STRUCTURES;

EID: 0036709643     PISSN: 08927057     EISSN: None     Source Type: Journal    
DOI: 10.1177/0892705702015005736     Document Type: Article
Times cited : (57)

References (10)
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    • (1999) Journal of Solids and Structures , vol.1 , pp. 1-24
    • Rahulkumar, P.1    Jagota, A.2    Bennison, S.J.3    Saigal, S.4
  • 4
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    • The influence of plasticity on mixed mode interface toughness
    • Tvergaard, V., Hutchinson, J.W. (1993). The influence of plasticity on mixed mode interface toughness. J. Mech. Phys. Solids, 41: 1119-1135.
    • (1993) J. Mech. Phys. Solids , vol.41 , pp. 1119-1135
    • Tvergaard, V.1    Hutchinson, J.W.2
  • 5
    • 0000458408 scopus 로고
    • A combined stress-based and fracture-mechanics-based model for predicting delamination in composites
    • Cui, W. and Wisnom, M.R. (1993). A combined stress-based and fracture-mechanics-based model for predicting delamination in composites. Composites, 6: 467-474.
    • (1993) Composites , vol.6 , pp. 467-474
    • Cui, W.1    Wisnom, M.R.2
  • 6
    • 0005183147 scopus 로고    scopus 로고
    • Research report, EPSRC Grant GR/133047, March 1999, No. 9, Centre for Composite Materials of Imperial College, London, UK
    • Research report, EPSRC Grant GR/133047, March 1999, No. 9, Centre for Composite Materials of Imperial College, London, UK.
  • 7
    • 0004072205 scopus 로고    scopus 로고
    • Through-thickness test methods for laminated composite materials
    • PhD Thesis, Department of Aeronautics, Imperial College
    • Mespoulet, S. (1998). Through-thickness test methods for laminated composite materials. PhD Thesis, Department of Aeronautics, Imperial College.
    • (1998)
    • Mespoulet, S.1
  • 8
    • 0003634603 scopus 로고    scopus 로고
    • A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading
    • NASA Langley Research Center, TM-209365, ARL-TR-2012
    • Kruege, R., Mingue, P.J. O'Brien, T.K. (1999). A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading. NASA Langley Research Center, TM-209365, ARL-TR-2012.
    • (1999)
    • Kruege, R.1    Mingue, P.J.2    O'Brien, T.K.3
  • 9
    • 0005105472 scopus 로고    scopus 로고
    • Report from DLR (Germany) 1999: BE-3444/BREU-0183
    • Report from DLR (Germany) 1999: BE-3444/BREU-0183.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.