###################################################### # #TA6 Internal flows AC34a Axial Compressor Casacade # #File contains overall pressure loss coefficient, exit #flow angle and exit Mach number. # #Reynolds number : 5E5 #Inlet turbulence intensity : 0.05 (5%) #Inlet Mach number : 0.6 #Inlet flow angle : 49.5 deg #Axial Velocity Density Ratio : 1.2 # ###################################################### %AC = 6-10 %Column1Name = pressure loss coefficient %Column1Units = non-dimensional %Column1Type = Real %Column2Name = M2 (exit Mach number) %Column2Units = non-dimensional %Column2Type = Real %Column3Name = a2 (exit flow angle) %Column3Units = degrees %Column3Type = Real %End of Metadata 0.0327 0.431 0.656