Effect of ply thickness and ply level hybridization on the compression after impact strength of thin laminates

There is a lack of research available on how thin laminates respond to impact and post impact loads, even though thin structures are used in present-day aircrafts. This experimental paper employs thick, standard and thin uni-directional plies to investigate the effect ply thickness has on thin lamin...

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Detalles Bibliográficos
Autores: Sasikumar, Aravind, Trias Mansilla, Daniel, Costa i Balanzat, Josep, Blanco Villaverde, Norbert, Orr, Jessica, Linde, Peter
Tipo de recurso: artículo
Estado:Versión aceptada para publicación
Fecha de publicación:2019
País:España
Institución:Varias* (Consorci de Biblioteques Universitáries de Catalunya, Centre de Serveis Científics i Acadèmics de Catalunya)
Repositorio:Recercat. Dipósit de la Recerca de Catalunya
OAI Identifier:oai:recercat.cat:10256/26054
Acceso en línea:http://hdl.handle.net/10256/26054
Access Level:acceso abierto
Palabra clave:Mecànica de fractura
Materials compostos
Materials laminats
Assaigs de materials
Fracture mechanics
Composite materials
Laminated materials
Materials -- Testing
Descripción
Sumario:There is a lack of research available on how thin laminates respond to impact and post impact loads, even though thin structures are used in present-day aircrafts. This experimental paper employs thick, standard and thin uni-directional plies to investigate the effect ply thickness has on thin laminates on their impact and compression after impact (CAI) response. Further, we propose two hybrid laminates where thick or standard plies are mixed with thin plies, respectively, in an effort to improve the CAI strength of thin laminates. Results reveal that, contrary to thick laminates, thin laminates made of only thin plies exhibit extensive fibre failure, leading to a considerably reduced CAI strength. Moreover, the hybrid laminate where thick 0° plies are mixed with thin plies improves the CAI strength by 40% over the thin ply baseline laminate. Thus, hybridization with thin laminates appears to be an economic prospective in terms of improving damage tolerance