03.1 - Aerodynamics - CFD Methods and Validation
SHIP-HELICOPTER OPERATIONAL LIMITATION ENVELOPE DEFINITION WITH CFD RESULTS AND WIND TUNNEL DATA
C.F. Rafaelš, G.A.L. da Silvaš, M.J.M. Guedes, Brazilian Navy, Brazil; šAerothermal Solutions and Software Distributor, Brazil
The present paper presents a SHOL envelope definition based on a CFD study and from a wind tunnel campaign. The results from wind tunnel were used to validate de CFD study. As only one procedure of landing was tested in wind tunnel, the CFD simulation was used to build envelopes for the others procedures of landings.