Yayın: Unsteady Navier Stokes Solutions of Low Aspect Ratio Rectangular Flat Wings in Compressible Flow
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Transonic, Aspect ratio (aeronautics), Vortex, Delta wing, Mechanics, Leading edge, Suction, Flow (mathematics), Enhanced Data Rates for GSM Evolution, Wind tunnel, Bubble, Angle of attack, Compressibility, Physics, Geometry, Mathematics, Engineering, Aerodynamics, Meteorology
