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Volumn 21, Issue 4, 2002, Pages 311-332

A comparative study of finite element models for the bonded repair of composite structures

Author keywords

Adhesively bonded repairs; Composite adherends; Finite element model

Indexed keywords

AIRCRAFT MATERIALS; CRACKS; DELAMINATION; ELASTIC MODULI; EPOXY RESINS; FINITE ELEMENT METHOD; LAMINATES; MATHEMATICAL MODELS; POISSON RATIO; STRESS CONCENTRATION; TENSILE STRESS; TENSILE TESTING;

EID: 0036091120     PISSN: 07316844     EISSN: None     Source Type: Journal    
DOI: 10.1177/0731684402021004257     Document Type: Article
Times cited : (31)

References (37)
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  • 9
    • 0037872019 scopus 로고
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    • SAE Paper 851830, Aerospace Technology Conference and Exposition, Long Beach, California, USA, 14-17 Oct
    • (1985) , pp. 15
    • Hart-Smith, L.J.1
  • 16
    • 4243205850 scopus 로고
    • Advanced composite repair guide
    • AFWAL-TR-83-3092, Air Force Wright Aeronautical Lab, USA
    • (1982)
    • Myhre, S.H.1
  • 20
    • 0003660293 scopus 로고
    • Analysis and design of advanced composite bonded joints
    • NASA contractor Report CR-2218
    • (1974)
    • Hart-Smith, L.J.1
  • 22
    • 0004196937 scopus 로고
    • Adhesive bonded scarf and stepped lap joints
    • NASA Contractor Report CR 112237
    • (1973)
    • Hart-Smith, L.J.1
  • 23
  • 25
    • 4244009886 scopus 로고
    • Modelling and analysis of peel and shear stresses in adhesively bonded joints
    • Paper 84-0913, AIAA
    • (1984)
    • Loss, K.R.1    Kedward, K.T.2
  • 28
    • 4243785190 scopus 로고
    • The development of an engineering standard for composite repair
    • AGARD-CP-550, AGARD, NATO
    • (1995)
    • Davis, M.J.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.