3D viscous flow analysis on wing-body-aileron-spoiler configurations |
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| Institution: | 1. AIRBUS, Aircraft Control, 316 route de Bayonne, 31060 Toulouse Cedex 09, France (+33-561183803;7. University of Bristol. Aerospace department - Queen''s Building. University Walk. Bristol, BS8 1TR. UK;71. Deimos Engenharia, 1998-023 Lisbon, Portugal;77. DEIMOS Space S.L.U, Ronda de Poniente, 19, 28760, Tres Cantos, Madrid, Spain;1. Airbus Defence and Space, rue du Général Niox 33165 St Médard en Jalles (France);2. Airbus Defence and Space, 31 rue des Cosmonautes 31402 Toulouse (France);3. CNES, 18 avenue Edouard Belin 31401 Toulouse Cedex 9 France |
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| Abstract: | The paper presents the configuration requirements and the strategy of mesh generation for wing-body configurations including spoilers and ailerons. Samples of final mesh features are shown, convergence issues are addressed and a number of sample solutions are discussed with respect to varying incidences, spoiler and aileron deflections and Reynolds numbers. The effects are discussed and compared with measurements. |
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