TY - JOUR
T1 - On the benefit of thin plies on flexural response of CFRP composites aged at elevated temperature
AU - Basha, Muhammad
AU - Wagih, A.
AU - Khan, T.
AU - Lubineau, G.
AU - Sebaey, T. A.
N1 - Funding Information:
This research work was funded by the Institutional Fund Project under grant no. (IFPIP: 769-135-1443). The authors gratefully acknowledge technical and financial support provided by the Ministry of Education and King Abdulaziz University, DSR, Jeddah, Saudi Arabia.
Publisher Copyright:
© 2022 Elsevier Ltd
PY - 2023/3
Y1 - 2023/3
N2 - This paper demonstrated the benefits of thin plies for enhancing the flexural response of conventional composites at elevated temperatures. Two types of carbon fabrics i.e., traditional ply (320 um thick) and thin ply (80 um thick), and general purpose epoxy was used to fabricate composites using autoclave manufacturing process. Three configurations of laminates were made, with the first one having all traditional plies, second one with the core made of all thin plies surrounded by traditional plies and the third one with each traditional ply sandwiched by a set of thin plies. Three-point bending test was conducted after thermal aging for 24 h at of 140 °C, 160 °C, 180 °C, 200 °C and 220 °C. The results demonstrated that the laminates containing thin plies have higher flexural strength and modulus at all the considered ageing temperatures, due to the existence of thin plies that delayed the compressive fiber damage at the plies in contact with the indenter. Moreover, the existence of these plies interrupted the heat flow to the laminate core, which reduced the propagation of delamination and matrix cracks inside the laminate core. The laminate with conventional plies surrounded by thin plies, showed the highest flexural strength improvement of 20 % at 220 °C.
AB - This paper demonstrated the benefits of thin plies for enhancing the flexural response of conventional composites at elevated temperatures. Two types of carbon fabrics i.e., traditional ply (320 um thick) and thin ply (80 um thick), and general purpose epoxy was used to fabricate composites using autoclave manufacturing process. Three configurations of laminates were made, with the first one having all traditional plies, second one with the core made of all thin plies surrounded by traditional plies and the third one with each traditional ply sandwiched by a set of thin plies. Three-point bending test was conducted after thermal aging for 24 h at of 140 °C, 160 °C, 180 °C, 200 °C and 220 °C. The results demonstrated that the laminates containing thin plies have higher flexural strength and modulus at all the considered ageing temperatures, due to the existence of thin plies that delayed the compressive fiber damage at the plies in contact with the indenter. Moreover, the existence of these plies interrupted the heat flow to the laminate core, which reduced the propagation of delamination and matrix cracks inside the laminate core. The laminate with conventional plies surrounded by thin plies, showed the highest flexural strength improvement of 20 % at 220 °C.
KW - A. Polymer-matrix composites (PMCs)
KW - B. High-temperature properties
KW - D. CT analysis
KW - Thin plies
UR - http://www.scopus.com/inward/record.url?scp=85144601083&partnerID=8YFLogxK
U2 - 10.1016/j.compositesa.2022.107393
DO - 10.1016/j.compositesa.2022.107393
M3 - Article
AN - SCOPUS:85144601083
SN - 1359-835X
VL - 166
JO - Composites Part A: Applied Science and Manufacturing
JF - Composites Part A: Applied Science and Manufacturing
M1 - 107393
ER -