%0 Conference Proceedings
%T Dynamic delamination of aeronautic structural composites by using cohesive finite elements
%+ Institut Clément Ader (ICA)
%A Ilyas, Muhammad
%A Lachaud, Frederic
%A Espinosa, Christine
%A Salaün, Michel
%< avec comité de lecture
%Z MS2M
%Z MSC
%( 7th International Conference on Composite Materials (ICCM-17)
%B 17th International Conference on Composite Materials (ICCM-17)
%C Edinburgh, United Kingdom
%P 0
%8 2009-07-27
%D 2009
%K Rapid dynamics
%K Carbon/epoxy composites
%K Cohesive elements
%K Impact
%Z Engineering Sciences [physics]/Mechanics [physics.med-ph]/Mechanics of materials [physics.class-ph]
%Z Engineering Sciences [physics]/Mechanics [physics.med-ph]/Mechanics of the structures [physics.class-ph]Conference papers
%X Cohesive finite elements are used to model impact induced delamination prediction of T800/21M unidirectional laminated composite. DCB, ELS and MMB tests are used to identify cohesive element parameters. Results from experiments and numerical prediction of impact induced delamination by commercially available code LS-DYNA are compared.
%G English
%2 https://hal.archives-ouvertes.fr/hal-01851843/document
%2 https://hal.archives-ouvertes.fr/hal-01851843/file/Ilyas_3537.pdf
%L hal-01851843
%U https://hal.archives-ouvertes.fr/hal-01851843
%~ CNRS
%~ INSA-TOULOUSE
%~ ICA
%~ INSA-GROUPE
%~ UNIV-TLSE3
%~ INSTITUTS-TELECOM
%~ INSTITUT-TELECOM