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Volumn 21, Issue 17, 2002, Pages 1561-1585

Finite element analysis of composite wing T-joints

Author keywords

Bending; Composite joint; Composite shell element; Deflection; Finite element; Stresses

Indexed keywords

BENDING STRENGTH; DEFLECTION (STRUCTURES); FINITE ELEMENT METHOD; INTERFACES (MATERIALS); NUMERICAL METHODS; PARAMETER ESTIMATION; STRESSES; WINGS;

EID: 0036454384     PISSN: 07316844     EISSN: None     Source Type: Journal    
DOI: 10.1177/0731684402021017474     Document Type: Article
Times cited : (51)

References (11)
  • 1
    • 0018025586 scopus 로고
    • Behavior of integral composite joints-finite element and experimental evaluation
    • Gillesspie, J. W. Jr. and Pipes, R. B. (1978). Behavior of integral composite joints-finite element and experimental evaluation. Journal of Composite Materials, 12.
    • (1978) Journal of Composite Materials , vol.12
    • Gillesspie J.W., Jr.1    Pipes, R.B.2
  • 2
    • 0026852346 scopus 로고
    • Influence of geometric nonlinearities on skin-stiffener interface stresses
    • Cohen, D. and Hyer, M.W. (1991). Influence of geometric nonlinearities on skin-stiffener interface stresses. AIAA Journal, 3:1055-1062.
    • (1991) AIAA Journal , vol.3 , pp. 1055-1062
    • Cohen, D.1    Hyer, M.W.2
  • 4
    • 4243375544 scopus 로고
    • Investigation of the bond strength of a discrete skin-stiffener interface
    • NLR TP 92183 U
    • Thuis, H.G.S.J. and Wiggenraad, J.F.M. (1992). Investigation of the bond strength of a discrete skin-stiffener interface. NLR TP 92183 U.
    • (1992)
    • Thuis, H.G.S.J.1    Wiggenraad, J.F.M.2
  • 5
    • 4243376345 scopus 로고
    • Interlaminar stress analysis at the skin-stiffener interface of a grid stiffened composite panel
    • NLR TP 91011 U
    • Wiggenraad, J.F.M. and Bauld, N. R. Jr. (1991). Interlaminar stress analysis at the skin-stiffener interface of a grid stiffened composite panel. NLR TP 91011 U.
    • (1991)
    • Wiggenraad, J.F.M.1    Bauld N.R., Jr.2
  • 6
    • 4243244820 scopus 로고    scopus 로고
    • Failure criterion for the skin-stiffener interface in composite aircraft panels
    • NLR TP 98264
    • Rijn, J.C.F.N. van (1998). Failure criterion for the skin-stiffener interface in composite aircraft panels, NLR TP 98264.
    • (1998)
    • Van Rijn, J.C.F.N.1
  • 9
    • 0003474648 scopus 로고    scopus 로고
    • New Delhi: Prentice Hall of India Private Limited
    • Bathe, K. (1997). Finite Element Procedures. New Delhi: Prentice Hall of India Private Limited.
    • (1997) Finite Element Procedures
    • Bathe, K.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.