############################################################################## # # TA1 External Aerodynamics AC1-02 RAE M2155 Wing # # File contains the Experimental friction coefficients at y/b = 0.60 # # Mach number : 0.854 # Reynolds number : 4.1 x 10^6 # Angle of incidence : 1.50 (deg) ############################################################################## %AC = 1-02 %Column1Name = x/c (upper surface) %Column1Units = %Column1Type = Real %Column2Name = Cf (upper surface) %Column2Units = %Column2Type = Real %Column3Name = x/c (lower surface) %Column3Units = %Column3Type = Real %Column4Name = -Cf (lower surface) %Column4Units = %Column4Type = Real %End of Metadata 0.4500 0.00175 0.9500 -0.00158 0.5500 0.00226 0.9000 -0.00118 0.7500 0.00174 0.8500 -0.00100 0.8500 0.00161 0.7500 -0.00081 0.9000 0.00118 0.6750 -0.00107 0.9500 0.00071 0.5500 -0.00196