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Volumn 60, Issue 15, 2000, Pages 2849-2856

Modelling of splitting and delamination in notched cross-ply laminates

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CRACKS; DELAMINATION; FAILURE (MECHANICAL); FINITE ELEMENT METHOD; INTERFACES (MATERIALS); MATHEMATICAL MODELS; TENSILE STRESS;

EID: 0034322950     PISSN: 02663538     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0266-3538(00)00170-6     Document Type: Article
Times cited : (112)

References (17)
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    • (1985) Journal of Reinforced Plastics and Composites , vol.4 , pp. 3-159
    • Awerbuch, J1    Madhukar, M.S2
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    • F.K Chang K.Y Chang A progressive damage model for laminated composites containing stress concentrations Journal of Composite Materials 21 1987 834 855
    • (1987) Journal of Composite Materials , vol.21 , pp. 834-855
    • Chang, F.K1    Chang, K.Y2
  • 4
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    • Damage tolerance of laminated composites containing an open hole and subjected to tensile loadings
    • K.Y Chang S Liu F.K Chang Damage tolerance of laminated composites containing an open hole and subjected to tensile loadings Journal of Composite Materials 25 1991 274 301
    • (1991) Journal of Composite Materials , vol.25 , pp. 274-301
    • Chang, K.Y1    Liu, S2    Chang, F.K3
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    • Experimental study on clamping effects on the tensile strength of composite plates with a bolt-filled hole
    • Y Yan W.D Wen F.K Chang P Shyprykevich Experimental study on clamping effects on the tensile strength of composite plates with a bolt-filled hole Composites 30A 1999 1215 1229
    • (1999) Composites , vol.30A , pp. 1215-1229
    • Yan, Y1    Wen, W.D2    Chang, F.K3    Shyprykevich, P4
  • 6
    • 85119557916 scopus 로고    scopus 로고
    • Chang FK, Qing X, Sun H-T, Yan YM. Damage tolerance-based design of bolted composite joints, Final report to Boeing Commercial Airplane Group under contract No. TZ-370444-07LHN and to FAA Technical Center under contract No. DEPT/95-G-012-0001, Stanford University, Department of Aeronautics and Astronautics, 1999.
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    • 0025684079 scopus 로고
    • Damage mechanics of composite materials. I: Measurements of damage and strength
    • M.T Kortschot P.W.R Beaumont Damage mechanics of composite materials. I: Measurements of damage and strength Composites Science and Technology 39 1990 289 301
    • (1990) Composites Science and Technology , vol.39 , pp. 289-301
    • Kortschot, M.T1    Beaumont, P.W.R2
  • 8
    • 0026754953 scopus 로고
    • Fatigue damage mechanics of composite materials. I: Experimental measurement of damage and post-fatigue properties
    • S.M Spearing P.W.R Beaumont Fatigue damage mechanics of composite materials. I: Experimental measurement of damage and post-fatigue properties Composites Science and Technology 44 1992 159 168
    • (1992) Composites Science and Technology , vol.44 , pp. 159-168
    • Spearing, S.M1    Beaumont, P.W.R2
  • 10
    • 85119563570 scopus 로고    scopus 로고
    • Johnson P, Chang FK. Characterization of matrix crack-induced laminate failure, part II: analysis and verifications, Journal of Composite Materials, in press, 2000.
  • 11
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    • A combined stress based and fracture mechanics based model for predicting delamination in composites
    • W Cui M.R Wisnom A combined stress based and fracture mechanics based model for predicting delamination in composites Composites 24 1993 467 474
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    • Cui, W1    Wisnom, M.R2
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    • A nonlinear finite-element approach for the analysis of mode-I free edge delamination in composites
    • J.C.J Schellekens R de Borst A nonlinear finite-element approach for the analysis of mode-I free edge delamination in composites Int. J. Solids and Structures 30 1993 1239 1253
    • (1993) Int. J. Solids and Structures , vol.30 , pp. 1239-1253
    • Schellekens, J.C.J1    de Borst, R2
  • 13
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.