Several configuration of a one-bay component of a typical wing leading edge was prepared and tested at Alenia plant. Various materials, lay-up distribution and boundary conditions were investigated. Analysis of the suitable sensor distribution was also additionally performed for the best possible numerical correlation approach. The numerical finite element simulations were performed using the commercial explicit integration code MSc/Dytran.
Analysis of bird strike on a wing leading edge made of fibre metal laminates / Guida, Michele; Marulo, Francesco; M., Meo; M., Riccio; S., Russo. - ELETTRONICO. - Proceedings of ICCST/6:(2007), pp. 1-12. (Intervento presentato al convegno Sixteen International Conference on Composite Science and Technology (ICCST/6), tenutosi a Durban, South Africa nel January 22–24, 2007).
Analysis of bird strike on a wing leading edge made of fibre metal laminates
MARULO, FRANCESCO;
2007
Abstract
Several configuration of a one-bay component of a typical wing leading edge was prepared and tested at Alenia plant. Various materials, lay-up distribution and boundary conditions were investigated. Analysis of the suitable sensor distribution was also additionally performed for the best possible numerical correlation approach. The numerical finite element simulations were performed using the commercial explicit integration code MSc/Dytran.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
