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Volumn 26, Issue 1, 2000, Pages 75-89

Modelling delaminations in postbuckling stiffened composite shear panels

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING; COMPUTER SIMULATION; DELAMINATION; DIFFERENTIAL EQUATIONS; FINITE ELEMENT METHOD; INTEGRAL EQUATIONS; LAMINATED COMPOSITES; SHEAR STRENGTH; STIFFNESS; STRAIN RATE; STRUCTURAL PANELS;

EID: 0034228616     PISSN: 01787675     EISSN: None     Source Type: Journal    
DOI: 10.1007/s004660000154     Document Type: Article
Times cited : (16)

References (21)
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  • 10
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    • Robinson, P.1    Song, D.Q.2
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    • Scott ML (ed.) Gold Coast, July
    • Shyprykevich P (1997) Damage Tolerance of Composite Aircraft Structures: Analysis and Certification. In: Scott ML (ed.) Proc. 11th International Conference on Composite Materials, vol I, Gold Coast, July, pp. 552-562
    • (1997) Proc. 11th International Conference on Composite Materials , vol.1 , pp. 552-562
    • Shyprykevich, P.1
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    • (1995) Composites Sci. Technol. , vol.55 , pp. 319-327
    • Singh, S.1    Partridge, I.K.2
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    • Tao, J.1    Sun, C.T.2
  • 15
    • 0010742230 scopus 로고    scopus 로고
    • Durability of postbuckling fibre composite shear panels
    • Proc. Scott ML (ed.) Gold Coast, July
    • Thomson RS, Scott ML (1997) Durability of Postbuckling Fibre Composite Shear Panels. In: Proc. Scott ML (ed.) 11th International Conference on Composite Materials, Gold Coast, July, vol. VI, pp. 677-686
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.