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Volumn 36, Issue 1-2, 1996, Pages 161-169

Compression behaviour of flat stiffened panels made of composite material

Author keywords

[No Author keywords available]

Indexed keywords

COMPOSITE STRUCTURES; COMPRESSION TESTING; COMPUTER AIDED ANALYSIS; COMPUTER SOFTWARE; STIFFNESS;

EID: 0030230512     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(96)00075-X     Document Type: Article
Times cited : (11)

References (11)
  • 2
    • 13544253676 scopus 로고
    • Qualification of primary composite aircraft structures
    • New Materials and Fatigue Resistant Aircraft Structures, ed. D. L. Simpson. EMAS, Warley
    • Whitehead, R. S., Qualification of primary composite aircraft structures. In New Materials and Fatigue Resistant Aircraft Structures, ed. D. L. Simpson. Proceedings of the 14th ICAF Symposium, EMAS, Warley, 1987, pp. 585-617.
    • (1987) Proceedings of the 14th ICAF Symposium , pp. 585-617
    • Whitehead, R.S.1
  • 3
    • 0008461901 scopus 로고    scopus 로고
    • Certification of large airplane composite structures: Recent progress and new trends in compliance philosophy
    • Paper ICAS-90-1.8.1. AIAA
    • Rouchon, J., Certification of large airplane composite structures: recent progress and new trends in compliance philosophy. Paper ICAS-90-1.8.1. Proceedings of the 17th ICAS Congress, AIAA, pp. 1439-47.
    • Proceedings of the 17th ICAS Congress , pp. 1439-1447
    • Rouchon, J.1
  • 4
    • 0019279773 scopus 로고
    • A preliminary design procedure for composite panels with open-section stiffeners loaded in the post-buckling range
    • eds A. R. Bunsell et al. ICCM3, Pergamon Press
    • Dickson, J. N., Biggers, S. B. and Wang, J. T. S., A preliminary design procedure for composite panels with open-section stiffeners loaded in the post-buckling range. In Advances in Composite Materials, eds A. R. Bunsell et al. ICCM3, Pergamon Press, 1980, pp. 812-25.
    • (1980) Advances in Composite Materials , pp. 812-825
    • Dickson, J.N.1    Biggers, S.B.2    Wang, J.T.S.3
  • 5
    • 0037832986 scopus 로고
    • Design of stiffened composite panels in the post-buckling range
    • eds M. Edward et al. Plenum Press
    • Dickson, J. N., Cole, R. T. and Wang J. T. S., Design of stiffened composite panels in the post-buckling range. In Fibrous Composites in Structural Design, eds M. Edward et al. Plenum Press, 1980, pp. 313-27.
    • (1980) Fibrous Composites in Structural Design , pp. 313-327
    • Dickson, J.N.1    Cole, R.T.2    Wang, J.T.S.3
  • 7
    • 0022107662 scopus 로고
    • Postbuckling behaviour of selected flat stiffened graphite-epoxy panels loaded in compression
    • Starnes, J H. Jr., Knight, N. F. Jr. and Rouse, M., Postbuckling behaviour of selected flat stiffened graphite-epoxy panels loaded in compression. AIAA Jnl., 1985, 23(8), 1236-1246.
    • (1985) AIAA Jnl. , vol.23 , Issue.8 , pp. 1236-1246
    • Starnes J.H., Jr.1    Knight N.F., Jr.2    Rouse, M.3
  • 8
    • 0023167129 scopus 로고
    • PANDA-2 program for minimum weight design of stiffened, composite locally buckled panels
    • Bushnell, D., PANDA-2 program for minimum weight design of stiffened, composite locally buckled panels. Comput. Struct., 1987, 25(4), 469-605.
    • (1987) Comput. Struct. , vol.25 , Issue.4 , pp. 469-605
    • Bushnell, D.1
  • 10
    • 30244458736 scopus 로고
    • Damage tolerance of composites
    • London
    • McCarty, J. E. and Norton, R. E., Damage tolerance of composites. Paper presented at the 15th ICAS Congress, London, 1986.
    • (1986) 15th ICAS Congress
    • McCarty, J.E.1    Norton, R.E.2
  • 11
    • 1942518650 scopus 로고
    • A, B, C, D, Rev. K. 5. MARC Analysis Research Corporation
    • MARC Reference Library. Vols A, B, C, D, Rev. K. 5. MARC Analysis Research Corporation, 1992.
    • (1992) MARC Reference Library


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.