25th Congress of International Council of the Aeronautical Sciences, 3 - 8 September 2006, Hamburg, Germany
Paper ICAS 2006-3.6.2

EXPERIMENTAL STUDY AND NUMERICAL SIMULATION OF FLOW AROUND WING CONTROL SURFACE

G. Fillola, G. Carrier*, J.- B. Dor*
Airbus, France; *ONERA, France

Keywords: Spoiler and aileron, CFD, Unsteady transonic flow, HTP and VTP

Wind tunnel testing has been conducted in the ONERA-T2 facility, on an extruded profile equipped with both an aileron and a spoiler. A numerical validation completes these tests, in order to evaluate CFD capability to predict control surfaces effectiveness. This study has been finalized with CFD industrial applications.

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