############################################################################## # # TA1 External Aerodynamics AC1-02 RAE M2155 Wing # # File contains the Experimental friction coefficients at y/b = 0.20 # # Mach number : 0.806 # Reynolds number : 4.1 x 10^6 # Angle of incidence : 2.50 (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 0.450 0.00227 0.950 -0.00198 0.550 0.00207 0.900 -0.00169 0.750 0.00186 0.850 -0.00153 0.850 0.00165 0.750 -0.00152 0.900 0.00128 0.675 -0.00197 0.950 0.00104 0.550 -0.00281