TY - JOUR
T1 - Mechanical properties and damage behavior of bi-directional glass fiber non-crimp fabric laminates
T2 - effects of laminate and nesting configurations
AU - Fikry, M. J.Mohammad
AU - Nakatani, Hayato
AU - Ohtani, Akio
AU - Kobayashi, Satoshi
AU - Ogihara, Shinji
N1 - Publisher Copyright:
© 2025 Japan Society for Composite Materials, Korean Society for Composite Materials and Informa UK Limited, trading as Taylor & Francis Group.
PY - 2025
Y1 - 2025
N2 - This study investigates the mechanical properties, failure behavior, and damage mechanisms of bi-directional glass fiber non-crimp fabric (NCF) laminates, focusing on the effects of nesting conditions and laminate configurations. The laminates were fabricated using the vacuum-assisted resin transfer molding (VaRTM) process and tested under tensile loading at 0° and 30° orientations. The bi-directional NCF materials consist of 0° fiber bundles in the warp direction and 90° fiber bundles in the weft direction. Four distinct laminate configurations were analyzed to understand the influence of fiber alignment and nesting conditions on mechanical performance. The 30° loading direction was chosen to examine the combined effects of tensile and shear stresses. Results demonstrate that nesting conditions and laminate configurations significantly affect crack initiation, propagation, and failure behavior. Laminates with nesting exhibited delayed crack propagation, more uniform crack distribution, and improved load-bearing capacity. In contrast, non-nested laminates displayed void-induced cracking, rapid crack propagation, and reduced structural integrity. This study provides a comprehensive evaluation of the failure behavior and damage mechanisms in bi-directional glass NCF laminates, offering valuable insights for optimizing composite materials in aerospace, automotive, and other structural applications.
AB - This study investigates the mechanical properties, failure behavior, and damage mechanisms of bi-directional glass fiber non-crimp fabric (NCF) laminates, focusing on the effects of nesting conditions and laminate configurations. The laminates were fabricated using the vacuum-assisted resin transfer molding (VaRTM) process and tested under tensile loading at 0° and 30° orientations. The bi-directional NCF materials consist of 0° fiber bundles in the warp direction and 90° fiber bundles in the weft direction. Four distinct laminate configurations were analyzed to understand the influence of fiber alignment and nesting conditions on mechanical performance. The 30° loading direction was chosen to examine the combined effects of tensile and shear stresses. Results demonstrate that nesting conditions and laminate configurations significantly affect crack initiation, propagation, and failure behavior. Laminates with nesting exhibited delayed crack propagation, more uniform crack distribution, and improved load-bearing capacity. In contrast, non-nested laminates displayed void-induced cracking, rapid crack propagation, and reduced structural integrity. This study provides a comprehensive evaluation of the failure behavior and damage mechanisms in bi-directional glass NCF laminates, offering valuable insights for optimizing composite materials in aerospace, automotive, and other structural applications.
KW - failure behavior
KW - glass fiber laminate
KW - material characterization
KW - nesting
KW - Non-crimp fabric
KW - VaRTM
UR - http://www.scopus.com/inward/record.url?scp=105002044319&partnerID=8YFLogxK
U2 - 10.1080/09243046.2025.2485803
DO - 10.1080/09243046.2025.2485803
M3 - Article
AN - SCOPUS:105002044319
SN - 0924-3046
JO - Advanced Composite Materials
JF - Advanced Composite Materials
ER -