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Volumn 34, Issue 1, 1996, Pages 178-184

Efficient modeling of postbuckling delamination growth in composite laminates using plate elements

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; BUCKLING; COMPOSITE STRUCTURES; DELAMINATION; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; PLATES (STRUCTURAL COMPONENTS); STRAIN RATE;

EID: 0029697977     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13038     Document Type: Article
Times cited : (44)

References (21)
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  • 2
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  • 4
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    • Refined Buckling and Postbuckling Analysis of Two-Dimensional Delaminations - I. Analysis and Validation
    • Yin, W. L., and Jane, K. C., "Refined Buckling and Postbuckling Analysis of Two-Dimensional Delaminations - I. Analysis and Validation," International Journal of Solids and Structures, Vol. 29, No. 5, 1992, pp. 591-610.
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  • 5
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    • Yin, W. L., and Jane, K. C., "Refined Buckling and Postbuckling Analysis of Two-Dimensional Delaminations - II. Results for Anisotropic Laminates and Conclusion," International Journal of Solids and Structures, Vol. 29, No. 5, 1992, pp. 611-639.
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  • 6
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  • 7
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    • Buckling and Post-Buckling Behavior of Elliptical Plates: Part I Analysis
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  • 9
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.