FN Archimer Export Format
PT J
TI Delamination behaviour of very high modulus carbon/epoxy marine composites
BT 
AF BARAL, N
   DAVIES, Peter
   BALEY, C
   BIGOURDAN, Benoit
AS 1:2;2:1;3:3;4:1;
FF 1:;2:PDG-DOP-DCB-ERT-MS;3:;4:PDG-DOP-DCB-ERT-MS;
C1 IFREMER, Ctr Brest, Mat & Struct Grp, F-29280 Plouzane, France.
   Trimaran Groupama, F-56100 Lorient, France.
   Univ Bretagne Sud, L2PIC, F-56321 Lorient, France.
C2 IFREMER, FRANCE
   TRIMARAN GROUPAMA, FRANCE
   UBS, FRANCE
SI BREST
SE PDG-DOP-DCB-ERT-MS
IN WOS Ifremer jusqu'en 2018
   copubli-france
   copubli-univ-france
IF 2.533
TC 17
UR https://archimer.ifremer.fr/doc/2008/publication-3772.pdf
LA English
DT Article
DE ;Mixed mode;Fracture toughness;Polymers;Carbon fibres;Delamination
AB This paper presents a study of the delamination resistance Of unidirectional carbon fibre reinforced epoxy composites manufactured from prepreg for racing yacht mast applications. Fibre modulus has been varied from 290 to 640 GPa. Two manufacturing methods, oven cure under vacuum and autoclave, were used to produce samples. Results show that delamination resistance tinder mode I and mixed mode loading decreases as fibre modulus increases. The manufacturing route affects G, values by modifying interlaminar layer geometry but does not change the trend of lower toughness with increasing fibre modulus. For the pitch composites crack propagation is observed within the fibres, in addition to more usual matrix and interface cracking. For the very high modulus fibre composites it is no longer possible to measure the Gill,, fracture envelope with the MMB specimen, compression failure occurs before delamination. FE analysis and instrumented specimens have been used to define the limits to the current standard test method for these materials. (c) 2007 Elsevier Ltd. All rights reserved.
PY 2008
PD MAR
SO Composites Science and Technology
SN 0266-3538
PU Elsevier
VL 68
IS 3-4
UT 000253621700047
BP 995
EP 1007
DI 10.1016/j.compscitech.2007.07.022
ID 3772
ER

EF