##################################################################### # # TA6 Low Speed Centrifugal Compressor (LSCC) # File contains NUMECA-results of: # Inlet spanwise distributions : station 1 # ##################################################################### %AC = 6-02 %Column1Name = z %Column1Units = m %Column1Type = Real %Column2Name = P/pstd %Column2Units = non-dimensional %Column2Type = Real %Column3Name = p/pstd %Column3Units = non-dimensional %Column3Type = Real %Column4Name = absolute flow angle %Column4Units = deg %Column4Type = Real %Column5Name = pitch angle %Column5Units = deg %Column5Type = Real %End Of Metadata 0.43334 0.99367 0.98503 -1.10000 3.90000 0.43216 0.99449 0.98503 -1.00000 3.60000 0.42920 0.99585 0.98510 -1.00000 2.70000 0.42624 0.99680 0.98503 -0.60000 2.50000 0.42032 0.99803 0.98517 -0.80000 2.70000 0.41440 0.99891 0.98510 -0.60000 1.80000 0.40847 0.99925 0.98510 -0.60000 1.50000 0.40255 0.99952 0.98517 -0.60000 1.30000 0.39663 0.99966 0.98517 -0.60000 1.40000 0.39071 0.99973 0.98523 -0.70000 1.20000 0.37591 0.99986 0.98523 -0.70000 2.00000 0.34630 0.99986 0.98557 -1.10000 3.30000 0.31669 0.99993 0.98591 -1.00000 4.80000 0.28708 0.99993 0.98625 -0.90000 6.30000 0.25748 0.99986 0.98680 -1.00000 8.10000 0.22787 0.99986 0.98734 -1.00000 10.20000 0.19826 0.99980 0.98830 -1.40000 12.50000 0.18346 0.99973 0.98911 -1.40000 13.90000 0.16866 0.99966 0.98979 -1.60000 15.60000 0.15977 0.99966 0.99020 -1.60000 16.80000 0.15681 0.99966 0.99047 -1.60000 17.20000 0.15385 0.99959 0.99061 -1.60000 17.70000 0.15089 0.99959 0.99095 -1.60000 18.20000 0.14793 0.99952 0.99122 -1.60000 18.80000 0.14497 0.99952 0.99170 -1.70000 19.50000 0.14349 0.99932 0.99170 -1.70000 19.80000