################################################################## # # TA6 GAS TURBINE NOZZLE CASCADE # # The file contains the static pressure (bar) measured # by each tap on suction and pressure side # for different total inlet pressure (P0) # and Isentropic Mach number at Outlet (Mis) ################################################################## %AC = 6-06 %Column1Name = Number of the Pressure tap %Column1Units = Non-dimensional %Column1Type = Integer %Column2Name = Curvilinear Abscissa on Suction or Pressure Side[S] %Column2Units = mm %Column2Type = Real %Column3Name = MUR 43 - P0 =1.435(bar) - Mis = 0.84 - Re = 1.00E+06 %Column3Units = bar %Column3Type = Real %Column4Name = MUR 44 - P0 =1.433(bar) - Mis = 0.84 - Re = 1.00E+06 %Column4Units = bar %Column4Type = Real %Column5Name = MUR 45 - P0 =1.475(bar) - Mis = 0.875 - Re = 1.00E+06 %Column5Units = bar %Column5Type = Real %Column6Name = MUR 46 - P0 =1.478(bar) - Mis = 0.875 - Re = 1.00E+06 %Column6Units = bar %Column6Type = Real %Column7Name = MUR 47 - P0 =1.596(bar) - Mis = 1.020 - Re = 1.00E+06 %Column7Units = bar %Column7Type = Real %Column8Name = MUR 48 - P0 =1.605(bar) - Mis = 1.020 - Re = 1.00E+06 %Column8Units = bar %Column8Type = Real %Column9Name = MUR 49 - P0 =1.608(bar) - Mis = 1.020 - Re = 1.00E+061 %Column9Units = bar %Column9Type = Real %End Of Metadata 1 0.000 1.435 1.437 1.487 1.487 1.604 1.613 1.612 2 2.100 1.417 1.418 1.469 1.469 1.587 1.597 1.592 3 4.060 1.401 1.401 1.451 1.450 1.565 1.573 1.570 4 10.170 1.261 1.262 1.302 1.302 1.398 1.404 1.403 5 16.904 1.046 1.048 1.074 1.075 1.146 1.151 1.147 6 20.298 0.933 0.933 0.947 0.948 1.001 1.007 1.004 7 23.691 0.894 0.895 0.908 0.909 0.951 0.956 0.954 8 27.046 0.882 0.882 0.898 0.899 0.937 0.941 0.937 9 33.817 0.837 0.837 0.834 0.835 0.837 0.837 0.837 10 39.232 0.811 0.811 0.804 0.804 0.799 0.795 0.799 11 42.600 0.799 0.799 0.782 0.783 0.779 0.779 0.780 12 46.000 0.790 0.789 0.764 0.765 0.743 0.742 0.745 13 50.747 0.807 0.807 0.760 0.755 0.710 0.708 0.712 14 54.118 0.808 0.808 0.777 0.779 0.672 0.669 0.671 15 57.493 0.816 0.816 0.793 0.794 0.644 0.639 0.642 16 64.260 0.845 0.844 0.833 0.832 0.655 0.642 0.648 17 71.012 0.866 0.866 0.858 0.859 0.774 0.715 0.806 18 77.780 0.874 0.874 0.875 0.876 0.882 0.887 0.886 19 82.781 0.857 0.857 0.856 0.858 0.844 0.850 0.847 20 86.463 0.936 0.935 0.949 0.950 0.969 0.973 0.970 21 2.027 1.427 1.428 1.479 1.478 1.594 1.602 1.603 22 4.057 1.424 1.424 1.474 1.474 1.593 1.601 1.600 23 10.138 1.414 1.413 1.467 1.466 1.583 1.591 1.589 24 20.274 1.407 1.405 1.457 1.456 1.572 1.580 1.581 25 33.833 1.386 1.387 1.436 1.435 1.548 1.556 1.556 26 47.362 1.299 1.301 1.344 1.344 1.446 1.453 1.451