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Volumn 18, Issue 1, 2011, Pages 85-100

Analysis and compression testing of laminates optimised for damage tolerance

Author keywords

Compression; Damage tolerance; Delamination; Impact; Static strength

Indexed keywords

BARELY VISIBLE IMPACT DAMAGES; BASELINE CONFIGURATIONS; CAI STRENGTH; COMPRESSION; COMPRESSION TESTS; COMPRESSION-AFTER-IMPACT STRENGTHS; DAMAGE GROWTH; DAMAGE MORPHOLOGY; IMPACT; IMPACT LOADS; MODELLING METHODOLOGY; OUT-OF-PLANE; REDUCTION IN COMPRESSIVE STRENGTH; SEMI-ANALYTICAL; STACKING SEQUENCE; STATIC STRENGTH;

EID: 79951674465     PISSN: 0929189X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s10443-010-9153-z     Document Type: Conference Paper
Times cited : (32)

References (11)
  • 1
    • 0024144104 scopus 로고
    • Two-dimensional delamination growth in composite laminates under compression loading
    • Whitcomb JD (ed) ASTM STP 972. ASTM, Philadelphia, Ch. 8
    • Flanagan, G.: Two-dimensional delamination growth in composite laminates under compression loading. In Composite Materials: Testing and Design. In: Whitcomb JD (ed) ASTM STP 972. ASTM, Philadelphia, Ch. 8, 180-190 (1988)
    • (1988) Composite Materials: Testing and Design , pp. 180-190
    • Flanagan, G.1
  • 2
    • 0021785142 scopus 로고
    • Two-dimensional modelling of compressive failure in delaminated laminates
    • H Chai CD Babcock 1985 Two-dimensional modelling of compressive failure in delaminated laminates J. Comp. Mats. 19 67 98 10.1177/002199838501900105 (Pubitemid 15489995)
    • (1985) Journal of Composite Materials , vol.19 , Issue.1 , pp. 67-98
    • Chai, H.1    Babcock, C.D.2
  • 3
    • 44549087154 scopus 로고    scopus 로고
    • Post-buckled propagation model for compressive fatigue of impact damaged laminates
    • 10.1016/j.ijsolstr.2008.03.014
    • AT Rhead R Butler GW Hunt 2008 Post-buckled propagation model for compressive fatigue of impact damaged laminates Int. J. Sol. Struct. 45 16 4349 4361 10.1016/j.ijsolstr.2008.03.014
    • (2008) Int. J. Sol. Struct. , vol.45 , Issue.16 , pp. 4349-4361
    • Rhead, A.T.1    Butler, R.2    Hunt, G.W.3
  • 4
    • 70349415473 scopus 로고    scopus 로고
    • Compressive static strength model for impact damaged laminates
    • 1:CAS:528:DC%2BD1MXht1agtb%2FE 10.1016/j.compscitech.2009.01.010
    • AT Rhead R Butler 2009 Compressive static strength model for impact damaged laminates Compos. Sci. Technol. 69 14 2301 2307 1:CAS:528: DC%2BD1MXht1agtb%2FE 10.1016/j.compscitech.2009.01.010
    • (2009) Compos. Sci. Technol. , vol.69 , Issue.14 , pp. 2301-2307
    • Rhead, A.T.1    Butler, R.2
  • 5
    • 77955429877 scopus 로고    scopus 로고
    • Compressive strength of laminates following free edge impact
    • doi: 10.10.16/j.compositesa.2009.10.024articleinpress
    • Rhead, A.T.; Butler, R.; Marchant, D.: Compressive strength of laminates following free edge impact. Comp. Part A. (2009). doi: 10.10.16/j.compositesa. 2009.10.024 article in press.
    • (2009) Comp. Part A.
    • Rhead A., .T.1    Butler, R.2    Marchant, D.3
  • 6
    • 0019707231 scopus 로고
    • One dimensional modelling of failure in laminated plates by delamination buckling
    • H Chai CD Babcock WG Knauss 1981 One dimensional modelling of failure in laminated plates by delamination buckling Int. J. Struct. 7 11 1069 1083 10.1016/0020-7683(81)90014-7 (Pubitemid 12433563)
    • (1981) International Journal of Solids and Structures , vol.17 , Issue.11 , pp. 1069-1083
    • Chai, H.1    Babcock, C.D.2    Knauss, W.G.3
  • 7
    • 0026253658 scopus 로고
    • VICONOPT. Program for exact vibration and buckling analysis or design of prismatic plate assemblies
    • FW Williams D Kennedy R Butler MS Anderson 1991 VICONOPT-Program for exact vibration and buckling analysis or design of prismatic plate assemblies AIAA 29 11 1927 1928 10.2514/3.10820 (Pubitemid 21717955)
    • (1991) AIAA journal , vol.29 , Issue.11 , pp. 1927-1928
    • Williams, F.W.1    Kennedy, D.2    Butler, R.3    Anderson, M.S.4
  • 8
    • 0035426389 scopus 로고    scopus 로고
    • Buckling behavior of composite laminates with multiple delaminations under uniaxial compression
    • DOI 10.1016/S0263-8223(01)00007-1, PII S0263822301000071
    • S-F Hwang G-H Liu 2001 Buckling behaviour of composite laminates with multiple delaminations under uniaxial compression Compos. Struct. 53 235 243 10.1016/S0263-8223(01)00007-1 (Pubitemid 32632942)
    • (2001) Composite Structures , vol.53 , Issue.2 , pp. 235-243
    • Hwang, S.-F.1    Liu, G.-H.2
  • 9
    • 0029277246 scopus 로고
    • The effect of stacking sequence on impact damage in a carbon fibre/epoxy composite
    • 1:CAS:528:DyaK2MXlsFamurw%3D 10.1016/0010-4361(95)91384-H
    • SA Hitchen RMJ Kemp 1995 The effect of stacking sequence on impact damage in a carbon fibre/epoxy composite Composites 26 207 214 1:CAS:528: DyaK2MXlsFamurw%3D 10.1016/0010-4361(95)91384-H
    • (1995) Composites , vol.26 , pp. 207-214
    • Hitchen, S.A.1    Kemp, R.M.J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.