RT Journal Article
T1 Machining FEM model of long fiber composites for aeronautical components
A1 Santiuste Romero, Carlos
A1 Soldani, Xavier
A1 Miguélez Garrido, María Henar
AB This work is focused on the study of orthogonal cutting of long fiber composites. A model based in finite element was developed. The mechanisms of chip formation of Glass and Carbon Fiber Reinforced Polymer (FRP) composites were analyzed. Significant differences were observed when comparing machining induced damage predicted with the model for both materials. While damage extended widely ahead the interface and beneath the tool tip in the case of GFRP, damage was located in a much smaller zone in the case CFRP. The fiber orientation influences both the mechanism of chip formation and the induced subsurface damage.
PB Elsevier
SN 0263-8223
YR 2010
FD 2010-02
LK https://hdl.handle.net/10016/15359
UL https://hdl.handle.net/10016/15359
LA eng
NO The authors are indebted for the financial support of this work,to the Ministry of Science and Education of Spain (under ProjectDPI2008-06746). The authors also acknowledge to the CAMUC3M for the financial support obtained for this work with theProject CCG08-UC3 M/DPI-4494.
DS e-Archivo
RD 1 sept. 2024