###################################################### # #TA6 Internal flows AC34a Axial Compressor Casacade # #File contains CFD data of pressure loss from #a wake traverse, 30% chord downstream of t.e. # #Reynolds number : 5E5 #Inlet turbulence intensity : 0.05 (5%) #Inlet Mach number : 0.8 #Inlet flow angle : 52.5 deg #Axial Velocity Density Ratio : 1.3 # ###################################################### %AC = 6-10 %Column1Name = distance y/t (fraction of pitch from ss to ps) %Column1Units = m/m (non-dimensional) %Column1Type = Real %Column2Name = w, pressure loss coefficient %Column2Units = non-dimensional %Column2Type = Real %End of Metadata 0.000000 0.000000 0.101010E-01 0.700574E-03 0.202020E-01 0.626888E-03 0.303030E-01 0.553208E-03 0.404041E-01 0.479533E-03 0.505051E-01 0.385684E-03 0.606061E-01 0.287734E-03 0.707071E-01 0.189737E-03 0.808081E-01 0.916947E-04 0.909091E-01 -0.311451E-03 0.101010 -0.838679E-03 0.111111 -0.136597E-02 0.121212 -0.189332E-02 0.131313 -0.248651E-02 0.141414 -0.312557E-02 0.151515 -0.376468E-02 0.161616 -0.440384E-02 0.171717 -0.492183E-02 0.181818 -0.530185E-02 0.191919 -0.568175E-02 0.202020 -0.606152E-02 0.212121 -0.624311E-02 0.222222 -0.605058E-02 0.232323 -0.585768E-02 0.242424 -0.566440E-02 0.252525 -0.537735E-02 0.262626 -0.476778E-02 0.272727 -0.415786E-02 0.282828 -0.354761E-02 0.292929 -0.297224E-02 0.303030 -0.270292E-02 0.313131 -0.243385E-02 0.323232 -0.216502E-02 0.333333 -0.189643E-02 0.343434 -0.164370E-02 0.353535 -0.139179E-02 0.363636 -0.114043E-02 0.373737 -0.889613E-03 0.383838 0.230856E-02 0.393939 0.598609E-02 0.404040 0.966351E-02 0.414141 0.133383E-01 0.424242 0.295861E-01 0.434343 0.502835E-01 0.444444 0.709798E-01 0.454545 0.916751E-01 0.464647 0.123534 0.474747 0.162324 0.484849 0.201114 0.494949 0.239904 0.505051 0.270395 0.515152 0.292432 0.525253 0.314471 0.535354 0.336511 0.545455 0.345540 0.555556 0.332775 0.565657 0.320010 0.575758 0.307245 0.585859 0.289893 0.595960 0.258940 0.606061 0.227987 0.616162 0.197034 0.626263 0.166536 0.636364 0.139065 0.646465 0.111594 0.656566 0.841233E-01 0.666667 0.567924E-01 0.676768 0.447218E-01 0.686869 0.326514E-01 0.696970 0.205809E-01 0.707071 0.851052E-02 0.717172 0.505396E-02 0.727273 0.268976E-02 0.737374 0.325568E-03 0.747475 -0.203867E-02 0.757576 -0.260748E-02 0.767677 -0.262745E-02 0.777778 -0.264748E-02 0.787879 -0.266757E-02 0.797980 -0.242085E-02 0.808081 -0.202676E-02 0.818182 -0.163269E-02 0.828283 -0.123861E-02 0.838384 -0.797049E-03 0.848485 -0.312052E-03 0.858586 0.172990E-03 0.868687 0.658071E-03 0.878788 0.103389E-02 0.888889 0.124642E-02 0.898990 0.145899E-02 0.909091 0.167162E-02 0.919192 0.180198E-02 0.929293 0.171998E-02 0.939394 0.163800E-02 0.949495 0.155604E-02 0.959596 0.144760E-02 0.969697 0.119765E-02 0.979798 0.947895E-03 0.989899 0.698354E-03 1.00000 0.000000