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AQFlow Inc. |
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return to project menu Subsonic Flow around a Wing-Fuselage Configuration under Incidence
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A three dimensional numerical analysis was carried out to assess the performance of turbulence models in the subsonic/transonic flow regime around a wing/fuselage configuration, at various incident angle range. The top figures show the wing-fuselage configuration and the distribution of a coarse grid around the geometry studied. The bottom figures show in subsonic regime (Mach=0.6), the mean pressure and the mean velocity distribution at fifteen degrees angle of attack where strong separation takes place.
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