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Volumn 36, Issue 2, 2009, Pages 243-253

Damage tolerance of impacted curved panels

Author keywords

Composite curved panels; Experimental design; Impact; Residual tensile strength

Indexed keywords

DAMAGE DETECTION; DAMAGE TOLERANCE; EXPERIMENTS; FATIGUE CRACK PROPAGATION; MACHINE DESIGN; OPTICAL MICROSCOPY; STATISTICS; STRENGTH OF MATERIALS; STRUCTURAL PANELS; TENSILE STRENGTH;

EID: 57649124404     PISSN: 0734743X     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijimpeng.2008.03.004     Document Type: Article
Times cited : (33)

References (17)
  • 2
    • 0036170652 scopus 로고    scopus 로고
    • Prediction of the residual tensile strengths of carbon-fiber/epoxy laminates with and without interleaves after solid particle erosion
    • Barkoula N.-M., Papanicolaou G., and Karger-Kocsis J. Prediction of the residual tensile strengths of carbon-fiber/epoxy laminates with and without interleaves after solid particle erosion. Composites Science and Technology 62 (2002) 121-130
    • (2002) Composites Science and Technology , vol.62 , pp. 121-130
    • Barkoula, N.-M.1    Papanicolaou, G.2    Karger-Kocsis, J.3
  • 4
    • 0022440894 scopus 로고
    • An assessment of the impact performance of CFRP with high strain carbon fibres
    • Cantwell W., Curtis P., and Morton J. An assessment of the impact performance of CFRP with high strain carbon fibres. Composites Science and Technology 25 (1986) 133-148
    • (1986) Composites Science and Technology , vol.25 , pp. 133-148
    • Cantwell, W.1    Curtis, P.2    Morton, J.3
  • 5
    • 57649119058 scopus 로고    scopus 로고
    • Poe CC Jr., Harris CE, Morris D. Surface crack analysis applied to impact damage in a thick graphite/epoxy composite. Technical Report TM-100600, NASA; 1988.
    • Poe CC Jr., Harris CE, Morris D. Surface crack analysis applied to impact damage in a thick graphite/epoxy composite. Technical Report TM-100600, NASA; 1988.
  • 6
    • 0033712517 scopus 로고    scopus 로고
    • Damage, deformation and residual burst strength of filament-wound composite tubes subjected to impact or quasi-static indentation
    • Curtis J., Hinton M., Li S., Reid S., and Soden P. Damage, deformation and residual burst strength of filament-wound composite tubes subjected to impact or quasi-static indentation. Composites: Part B 31 (2000) 419-433
    • (2000) Composites: Part B , vol.31 , pp. 419-433
    • Curtis, J.1    Hinton, M.2    Li, S.3    Reid, S.4    Soden, P.5
  • 7
    • 0000495517 scopus 로고
    • Uniform shell designs
    • Doelhert D. Uniform shell designs. Applied Statistics 19 3 (1970) 231-239
    • (1970) Applied Statistics , vol.19 , Issue.3 , pp. 231-239
    • Doelhert, D.1
  • 8
    • 0000553334 scopus 로고
    • Experimental designs through level reduction of the d-dimensional cuboctahedron
    • Doelhert D., and Klee V. Experimental designs through level reduction of the d-dimensional cuboctahedron. Discrete Mathematics 2 (1972) 309-334
    • (1972) Discrete Mathematics , vol.2 , pp. 309-334
    • Doelhert, D.1    Klee, V.2
  • 9
    • 0025480976 scopus 로고
    • On the prediction of tensile strength after impact of composite laminates
    • El-Zein M., and Reifsnider K. On the prediction of tensile strength after impact of composite laminates. Journal of Composites Technology and Research 12 3 (1990) 147-154
    • (1990) Journal of Composites Technology and Research , vol.12 , Issue.3 , pp. 147-154
    • El-Zein, M.1    Reifsnider, K.2
  • 10
    • 13844254310 scopus 로고    scopus 로고
    • Damage development in thick composite tubes under impact loading and influence on implosion pressure: experimental observations
    • Gning P., Tarfaoui M., Collombet F., Riou L., and Davies P. Damage development in thick composite tubes under impact loading and influence on implosion pressure: experimental observations. Composites: Part B 36 (2005) 306-318
    • (2005) Composites: Part B , vol.36 , pp. 306-318
    • Gning, P.1    Tarfaoui, M.2    Collombet, F.3    Riou, L.4    Davies, P.5
  • 13
    • 0035045805 scopus 로고    scopus 로고
    • The onset of delamination at stress-free edges in angle-ply laminates - analysis of two criteria
    • Leguillon D., Marion G., Harry R., and Lecuyer F. The onset of delamination at stress-free edges in angle-ply laminates - analysis of two criteria. Composites Science and Technology 61 (1999) 377-382
    • (1999) Composites Science and Technology , vol.61 , pp. 377-382
    • Leguillon, D.1    Marion, G.2    Harry, R.3    Lecuyer, F.4
  • 14
    • 33747375704 scopus 로고    scopus 로고
    • The influence of impactor shape on the damage to composite laminates
    • Mitrevski T., Marshall I., and Thomson R. The influence of impactor shape on the damage to composite laminates. Composite Structures 76 (2006) 116-122
    • (2006) Composite Structures , vol.76 , pp. 116-122
    • Mitrevski, T.1    Marshall, I.2    Thomson, R.3
  • 15
    • 57649116574 scopus 로고    scopus 로고
    • Nettles A. Instumented impact and residual tensile strength testing of eight-ply carbon/epoxy specimens. Technical Report 2981, NASA; 1990.
    • Nettles A. Instumented impact and residual tensile strength testing of eight-ply carbon/epoxy specimens. Technical Report 2981, NASA; 1990.
  • 16
    • 0035447863 scopus 로고    scopus 로고
    • Experimental determination of elastic properties of impact damage in carbon fibre/epoxy laminates
    • Sjögren A., Krasnikovs A., and Varna J. Experimental determination of elastic properties of impact damage in carbon fibre/epoxy laminates. Composites: Part A 32 (2001) 1237-1242
    • (2001) Composites: Part A , vol.32 , pp. 1237-1242
    • Sjögren, A.1    Krasnikovs, A.2    Varna, J.3
  • 17
    • 0030153214 scopus 로고    scopus 로고
    • Effect of impact damage on residual compressive strength of glass-fibre reinforced polyester (GFRP) laminates
    • Zhou G. Effect of impact damage on residual compressive strength of glass-fibre reinforced polyester (GFRP) laminates. Composite Structures 35 (1996) 171-181
    • (1996) Composite Structures , vol.35 , pp. 171-181
    • Zhou, G.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.