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Volumn 64, Issue 2, 2004, Pages 227-234

Experimental study of failure and failure progression in T-stiffened skins

Author keywords

Bermuda triangle; T stiffened skins

Indexed keywords

CARBON; CURING; DEBONDING; FAILURE (MECHANICAL); INTERFACES (MATERIALS); SKIN; STIFFNESS; STRUCTURAL LOADS;

EID: 1542783167     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2003.08.007     Document Type: Article
Times cited : (44)

References (19)
  • 3
    • 0019149508 scopus 로고
    • On experimental versus theoretical incipient buckling of narrow graphite/epoxy plates in compression
    • Proceedings of the AIAA/ASME/ASCE/AHS 21st Structures, Structural Dynamics and Materials Conference
    • Spier EE, On experimental versus theoretical incipient buckling of narrow graphite/epoxy plates in compression. In: AIAA Paper No. 80-0686. In: Proceedings of the AIAA/ASME/ASCE/AHS 21st Structures, Structural Dynamics and Materials Conference; 1980. p. 187-93
    • (1980) AIAA Paper No. 80-068 , pp. 187-193
    • Spier, E.E.1
  • 14
    • 0026896543 scopus 로고
    • Efficient stress solutions at skin stiffener interfaces of composite stiffened panels
    • Kassapoglou C. DiNicola A.J. Efficient stress solutions at skin stiffener interfaces of composite stiffened panels AIAA J. 30 1992 1833-1839
    • (1992) AIAA J. , vol.30 , pp. 1833-1839
    • Kassapoglou, C.1    DiNicola, A.J.2
  • 15
    • 0032026526 scopus 로고    scopus 로고
    • Australian developments in the analysis of composite structures with material and geometric nonlinearities
    • Jones R. Alesi H. Mileshkin N. Australian developments in the analysis of composite structures with material and geometric nonlinearities Compos. Struct. 41 1998 197-214
    • (1998) Compos. Struct. , vol.41 , pp. 197-214
    • Jones, R.1    Alesi, H.2    Mileshkin, N.3
  • 19
    • 1542390505 scopus 로고    scopus 로고
    • High fidelity failure analysis for a composite fuselage section
    • American Helicopter Society, Washington, USA, 9-11 May
    • Li J, Davila CG, Chen T-K. High fidelity failure analysis for a composite fuselage section. In: Proceedings of the 57th Annual Forum, American Helicopter Society, Washington, USA, 9-11 May 2001
    • (2001) Proceedings of the 57th Annual Forum
    • Li, J.1    Davila, C.G.2    Chen, T.-K.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.