############################################################ # TA6 Turbomachinery Internal Flows # AC22 Annular compressor cascade with tip-clearance # # File contains the computed circumferential mass average # span-wise distributions of flow quantities at Station 2 # # Tip-clearance size : 2.0% # Hub rotational speed : 0.0rpm # Mass flow-rate : 13.2kg/s # Reynolds number : 1.1E6 ############################################################ %AC = 6-05 %Column1Name = Spanwise position %Column1Units = % %Column1Type = Real %Column2Name = Static pressure %Column2Units = Pa %Column2Type = Real %Column3Name = Total pressure %Column3Units = Pa %Column3Type = Real %Column4Name = Axial component of velocity vector %Column4Units = Non-dimensional with respect to the peripheral velocity at hub %Column4Type = Real %Column5Name = Peripheral component of velocity vector %Column5Units = Non-dimensional with respect to the peripheral velocity at hub %Column5Type = Real %Column6Name = Span-wise component of velocity vector %Column6Units = Non-dimensional with respect to the peripheral velocity at hub %Column6Type = Real %Column7Name = Flow angle in the peripheral direction %Column7Units = Degrees %Column7Type = Real %Column8Name = Mach number %Column8Units = Non-dimensional %Column8Type = Real %Column9Name = Pressure loss coefficient %Column9Units = Non-dimensional %Column9Type = Real %End of Metadata .228506 73223.870000 77766.400000 .270989 .529577 .003374 62.900820 .294493 .000000 .478488 73255.570000 78865.580000 .304263 .583509 -.000033 62.460850 .326396 .000000 .728471 73267.610000 79676.500000 .328498 .619293 .001080 62.056730 .348197 .000000 .978453 73278.100000 80311.430000 .347146 .644987 .001783 61.709890 .364222 .000000 1.228436 73289.880000 80855.320000 .362874 .665487 .002215 61.397460 .377265 .000000 1.478418 73302.170000 81345.230000 .376883 .682899 .002719 61.106270 .388543 .000000 1.728400 73315.090000 81799.610000 .389751 .698223 .003223 60.829560 .398635 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