############################################################################## # # TA1 External Aerodynamics AC1-02 RAE M2155 Wing # # File contains the CFD DOAP parameters # # Mach number : 0.854 # Reynolds number : 4.1 x 10^6 # Angle of incidence : 1.50 (deg) ############################################################################## %AC = 1-02 %Column1Name = Lift coefficient %Column1Units = %Column1Type = Real %Column2Name = Pressure drag Coefficient %Column2Units = %Column2Type = Real %Column3Name = Friction drag coefficient %Column3Units = %Column3Type = Real %End of Metadata 0.40443 0.0295 0.005342