01 - Aircraft and Systems Integration
DETAILED AERO-STRUCTURAL DESIGN OF WINGLET FOR BUSINESS JET
N.R. El Haddad¹, L. Gonzalez¹; ¹EMBRY RIDDLE AERONAUTICAL UNIVERSITY, United States
First stage in the design and certification of a winglet for Dassault Falcon 10. The Vortex Lattice Method was used to screen configurations. For the final one, RANS CFD calculations were performed. An FE model of the wingbox was also constructed to estimate weight penalties. Both models were calibrated vs wind tunnel and stress reports data. Finally, impact on range and fuel burn is presented.