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Volumn 52, Issue 2, 2001, Pages 199-204

Estimation of compressive strength of delaminated composites

Author keywords

Damage tolerance; Delamination; Experiment; Prediction; Sublaminate

Indexed keywords

BUCKLING; COMPRESSIVE STRENGTH; DELAMINATION; NUMERICAL ANALYSIS; STRESS ANALYSIS;

EID: 0035340190     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(00)00168-9     Document Type: Article
Times cited : (23)

References (30)
  • 12
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    • Modelling compression failure after low velocity impact on laminated composites using interface elements
    • (1997) J Compos Mater , vol.31 , pp. 1462-1479
    • Moura, M.F.S.F.D.1
  • 15
  • 17
    • 0026714175 scopus 로고
    • Modelling compression failure of laminated composites containing multiple through-the-width delaminations
    • (1992) J Compos Mater , vol.26 , pp. 350-387
    • Kutlu, Z.1    Chang, F.K.2
  • 20
    • 0003770163 scopus 로고
    • The effect of stacking sequence and layer thickness on the compressive behaviour of carbon composite materials: Impact damage and compression after impact
    • Defence Research Agency, Farnborough
    • (1994) Technical Report 94003
    • Hitchen, S.A.1    Kemp, R.M.2
  • 24
    • 0031354048 scopus 로고    scopus 로고
    • Post-impact behaviour of aerospace composites for high-temperature applications: Experiments and simulations
    • (1997) Compos , vol.28 B , Issue.PART B , pp. 651-665
    • Giuseppe, S.1
  • 29
    • 0014583266 scopus 로고
    • A finite element method for the plastic buckling analysis of plates
    • (1969) AIAA J , vol.7 , pp. 1950-1957
    • Pifko, A.1    Isakson, G.2
  • 30
    • 0021819328 scopus 로고
    • NASA/aircraft industry standard specification for graphite fiber toughened thermoset resin composite materials
    • (1985) NASA Reference Publication , pp. 1142


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.