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Volumn 45, Issue 4, 1999, Pages 255-270

A study of fastener pull-through failure of composite laminates. Part 2: Failure prediction

Author keywords

[No Author keywords available]

Indexed keywords

FASTENER PULL THROUGH FAILURE; FLEXURAL FAILURES; INTERPLY DELAMINATION; PROGRESSIVE DAMAGE MODEL; TENSILE IN PLANE STRESSES;

EID: 0033169427     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(99)00010-0     Document Type: Article
Times cited : (33)

References (24)
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  • 2
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    • A study of fastener pull-through failure of composite laminates. Part 1: Experimental
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  • 3
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    • ASTM STP 1128, Masters JE, editor Philadelphia
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    • (1992) American Society for Testing and Materials , pp. 200-212
    • Chester, R.J.1    Clark, G.2
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  • 6
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    • Prediction of delamination in composite laminates subjected to low velocity impact
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    • Jih, C.J.1    Sun, C.T.2
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    • A new approach toward understanding damage mechanisms and mechanics of laminated composites due to low-velocity impact: Part II - Analysis
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    • (1991) Journal of Composite Materials , vol.25 , pp. 1012-1037
    • Choi, H.Y.1    Wu, H.Y.T.2    Chang, F.K.3
  • 10
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    • A model for predicting damage in graphite/ epoxy laminated composites resulting from low-velocity point impact
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.