###################################################### # #TA6 Internal flows AC34a Axial Compressor Casacade # #File contains experimaental data of surface pressure #distribution from static tappings # #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 = distance x/l (fraction of chord) %Column1Units = m/m (non-dimensional) %Column1Type = Real %Column2Name = Cp (pressure surface to suction surface) %Column2Units = non-dimensional %Column2Type = Real %End of Metadata 0.050 0.146 0.100 0.196 0.150 0.225 0.200 0.254 0.250 0.281 0.300 0.310 0.350 0.337 0.400 0.363 0.450 0.374 0.500 0.387 0.550 0.405 0.600 0.422 0.650 0.437 0.700 0.448 0.750 0.456 0.800 0.460 0.850 0.456 0.900 0.439 0.950 0.406 0.950 0.301 0.900 0.262 0.850 0.214 0.800 0.134 0.750 0.083 0.700 0.011 0.650 -.041 0.600 -.096 0.550 -.134 0.500 -.169 0.450 -.252 0.400 -.308 0.350 -.354 0.300 -.398 0.250 -.433 0.200 -.476 0.150 -.490 0.100 -.457 0.050 -.390