-
1
-
-
0024144104
-
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
-
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
-
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
-
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
-
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
-
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
-
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
-
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
-
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
|