###################################################### # #TA6 Internal flows AC34a Axial Compressor Casacade # #File contains CFD data of surface pressure #distribution # #Reynolds number : 5E5 #Inlet turbulence intensity : 0.05 (5%) #Inlet Mach number : 0.8 #Inlet flow angle : 52.5 deg #Axial Velocity Density Ratio : 1.12 # ###################################################### %AC = 6-10 %Column1Name = distance x/l (fraction of chord) %Column1Units = m/m (non-dimensional) %Column1Type = Real %Column2Name = Cp (suction surface) %Column2Units = non-dimensional %Column2Type = Real %Column3Name = distance x/l (fraction of chord) %Column3Units = m/m (non-dimensional) %Column3Type = Real %Column4Name = Cp (pressure surface) %Column4Units = non-dimensional %Column4Type = Real %End of Metadata 0.160981E-04 0.360808 1.00019 0.484876 -0.136111E-03 -0.210824 0.999731 0.465409 0.258915E-03 -0.740385 0.998891 0.367951 0.207714E-02 -1.04667 0.997404 0.267925 0.531812E-02 -1.03890 0.995149 0.300027 0.966740E-02 -0.941160 0.991619 0.385613 0.148375E-01 -0.842216 0.985076 0.433350 0.207280E-01 -0.771807 0.978164 0.469489 0.271566E-01 -0.725213 0.968862 0.498176 0.343338E-01 -0.673264 0.958452 0.514948 0.421450E-01 -0.594239 0.946684 0.530979 0.504477E-01 -0.496701 0.933734 0.545729 0.593882E-01 -0.412509 0.919326 0.557248 0.687047E-01 -0.362238 0.903839 0.565745 0.782885E-01 -0.343075 0.887645 0.572653 0.883376E-01 -0.340547 0.870439 0.578906 0.987416E-01 -0.336186 0.852786 0.584570 0.109384 -0.319340 0.834129 0.589487 0.120302 -0.290126 0.815224 0.593298 0.131530 -0.254998 0.795703 0.595942 0.142945 -0.221817 0.776060 0.597667 0.154449 -0.194176 0.755888 0.598736 0.165961 -0.170399 0.735859 0.599049 0.177752 -0.147542 0.715532 0.598234 0.189577 -0.124616 0.695114 0.596571 0.201371 -0.102240 0.674795 0.595243 0.213447 -0.810257E-01 0.654545 0.594345 0.225418 -0.613941E-01 0.634157 0.592612 0.237454 -0.432289E-01 0.613672 0.589809 0.249563 -0.260971E-01 0.593386 0.586674 0.261953 -0.971226E-02 0.573237 0.583417 0.274081 0.586732E-02 0.553045 0.579641 0.286536 0.207488E-01 0.533180 0.575080 0.299138 0.348952E-01 0.513062 0.570612 0.311673 0.481916E-01 0.493287 0.567037 0.324269 0.607156E-01 0.473530 0.562747 0.337193 0.727656E-01 0.453812 0.556792 0.350037 0.846780E-01 0.434376 0.550995 0.363074 0.967703E-01 0.415477 0.546055 0.376258 0.108862 0.396365 0.540836 0.389621 0.120476 0.377472 0.535079 0.403080 0.131534 0.359119 0.529286 0.416660 0.142577 0.340902 0.523735 0.430513 0.154001 0.322712 0.517906 0.444541 0.165406 0.304933 0.510820 0.458441 0.176215 0.287435 0.503144 0.472601 0.186582 0.270350 0.496735 0.486651 0.197043 0.253364 0.491470 0.500967 0.207873 0.236924 0.485979 0.515409 0.218708 0.220654 0.479951 0.529756 0.229214 0.204914 0.473847 0.544344 0.239642 0.189293 0.467868 0.558971 0.250345 0.174150 0.462015 0.573516 0.261367 0.159469 0.456073 0.588575 0.272524 0.145248 0.449845 0.603486 0.283510 0.131313 0.443494 0.618263 0.294363 0.117691 0.437715 0.633595 0.305281 0.104781 0.433453 0.648632 0.316202 0.920976E-01 0.431502 0.663832 0.327127 0.804266E-01 0.431198 0.678757 0.337950 0.689753E-01 0.430126 0.693613 0.348673 0.580403E-01 0.427356 0.708808 0.359360 0.484146E-01 0.426906 0.723844 0.369928 0.391219E-01 0.433232 0.739091 0.380352 0.311159E-01 0.439246 0.754009 0.390531 0.232498E-01 0.435344 0.768930 0.400484 0.176757E-01 0.418631 0.783951 0.410164 0.119180E-01 0.365787 0.799152 0.419351 0.850580E-02 0.386583 0.813719 0.427842 0.632998E-02 0.597188 0.828594 0.435776 0.000000 0.000000 0.843384 0.443171 0.000000 0.000000 0.857686 0.449926 0.000000 0.000000 0.871537 0.456022 0.000000 0.000000 0.885188 0.461517 0.000000 0.000000 0.898666 0.466432 0.000000 0.000000 0.911777 0.470726 0.000000 0.000000 0.923889 0.474397 0.000000 0.000000 0.935671 0.477566 0.000000 0.000000 0.946695 0.480289 0.000000 0.000000 0.956754 0.482590 0.000000 0.000000 0.965865 0.484541 0.000000 0.000000 0.974483 0.486216 0.000000 0.000000 0.981987 0.487644 0.000000 0.000000 0.988389 0.488861 0.000000 0.000000 0.993445 0.489756 0.000000 0.000000 0.996959 0.489941 0.000000 0.000000 0.998642 0.489046 0.000000 0.000000 0.999739 0.487386 0.000000 0.000000 1.00021 0.485478 0.000000 0.000000