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PSU-90-125WL (psu-90-125wl-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: PSU-90-125WL (psu-90-125wl-il)
Reynolds number: 500,000
Max Cl/Cd: 102.51 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-psu-90-125wl-il-500000.txt
Download as CSV file: xf-psu-90-125wl-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: PSU-90-125WL                                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.4260   0.10750   0.10512  -0.0439   1.0000   0.0275
 -11.500  -0.4308   0.10164   0.09929  -0.0468   1.0000   0.0277
 -11.250  -0.4481   0.09461   0.09231  -0.0487   1.0000   0.0284
 -11.000  -0.4478   0.09138   0.08910  -0.0494   1.0000   0.0287
 -10.750  -0.4410   0.09015   0.08788  -0.0489   1.0000   0.0294
 -10.500  -0.4425   0.08661   0.08437  -0.0500   1.0000   0.0299
 -10.250  -0.4500   0.08168   0.07947  -0.0520   1.0000   0.0303
 -10.000  -0.4618   0.07585   0.07368  -0.0548   1.0000   0.0307
  -9.000  -0.5972   0.03274   0.02852  -0.0793   0.9745   0.0220
  -8.750  -0.5757   0.02687   0.02234  -0.0813   0.9715   0.0196
  -8.500  -0.5540   0.02396   0.01905  -0.0816   0.9634   0.0194
  -8.250  -0.5252   0.02156   0.01632  -0.0828   0.9589   0.0192
  -8.000  -0.4988   0.01995   0.01450  -0.0832   0.9513   0.0193
  -7.750  -0.4693   0.01857   0.01296  -0.0840   0.9452   0.0197
  -7.500  -0.4418   0.01756   0.01182  -0.0842   0.9372   0.0203
  -7.250  -0.4134   0.01656   0.01069  -0.0846   0.9300   0.0208
  -7.000  -0.3884   0.01567   0.00969  -0.0843   0.9206   0.0211
  -6.750  -0.3620   0.01490   0.00880  -0.0841   0.9131   0.0214
  -6.500  -0.3380   0.01432   0.00812  -0.0835   0.9037   0.0217
  -6.250  -0.3165   0.01325   0.00696  -0.0826   0.8955   0.0224
  -6.000  -0.2936   0.01260   0.00624  -0.0819   0.8873   0.0232
  -5.750  -0.2689   0.01213   0.00569  -0.0814   0.8803   0.0242
  -5.500  -0.2440   0.01175   0.00526  -0.0809   0.8730   0.0255
  -5.250  -0.2180   0.01144   0.00486  -0.0806   0.8669   0.0271
  -5.000  -0.1933   0.01100   0.00436  -0.0800   0.8600   0.0297
  -4.750  -0.1672   0.01068   0.00399  -0.0797   0.8543   0.0343
  -4.500  -0.1433   0.01006   0.00357  -0.0792   0.8482   0.0738
  -4.250  -0.1190   0.00952   0.00328  -0.0788   0.8422   0.1375
  -4.000  -0.0935   0.00913   0.00307  -0.0786   0.8371   0.1950
  -3.750  -0.0685   0.00874   0.00290  -0.0783   0.8311   0.2549
  -3.500  -0.0429   0.00839   0.00274  -0.0781   0.8257   0.3177
  -3.250  -0.0168   0.00810   0.00261  -0.0779   0.8207   0.3767
  -3.000   0.0085   0.00777   0.00251  -0.0776   0.8149   0.4449
  -2.750   0.0345   0.00752   0.00244  -0.0773   0.8098   0.5096
  -2.500   0.0607   0.00737   0.00244  -0.0769   0.8048   0.5674
  -2.250   0.0875   0.00730   0.00244  -0.0766   0.7992   0.6075
  -2.000   0.1150   0.00727   0.00242  -0.0765   0.7942   0.6324
  -1.750   0.1427   0.00727   0.00241  -0.0763   0.7890   0.6516
  -1.500   0.1702   0.00725   0.00239  -0.0761   0.7832   0.6686
  -1.250   0.1980   0.00725   0.00237  -0.0760   0.7781   0.6843
  -1.000   0.2254   0.00725   0.00237  -0.0758   0.7721   0.6989
  -0.750   0.2529   0.00723   0.00236  -0.0756   0.7661   0.7121
  -0.500   0.2806   0.00724   0.00236  -0.0755   0.7607   0.7245
  -0.250   0.3078   0.00722   0.00237  -0.0752   0.7542   0.7365
   0.000   0.3356   0.00723   0.00235  -0.0751   0.7483   0.7480
   0.250   0.3629   0.00723   0.00237  -0.0749   0.7417   0.7594
   0.500   0.3901   0.00721   0.00236  -0.0746   0.7348   0.7699
   0.750   0.4173   0.00721   0.00238  -0.0744   0.7277   0.7808
   1.000   0.4444   0.00721   0.00238  -0.0741   0.7200   0.7924
   1.250   0.4713   0.00721   0.00240  -0.0738   0.7123   0.8038
   1.500   0.4979   0.00719   0.00241  -0.0735   0.7039   0.8148
   1.750   0.5244   0.00719   0.00244  -0.0731   0.6949   0.8266
   2.000   0.5507   0.00720   0.00245  -0.0726   0.6857   0.8392
   2.250   0.5766   0.00719   0.00248  -0.0721   0.6746   0.8525
   2.500   0.6019   0.00718   0.00252  -0.0714   0.6628   0.8664
   2.750   0.6266   0.00719   0.00255  -0.0706   0.6498   0.8813
   3.000   0.6506   0.00720   0.00260  -0.0697   0.6355   0.8980
   3.250   0.6735   0.00722   0.00264  -0.0684   0.6193   0.9169
   3.500   0.6969   0.00728   0.00268  -0.0673   0.6006   0.9393
   3.750   0.7266   0.00739   0.00275  -0.0676   0.5793   0.9611
   4.000   0.7624   0.00758   0.00286  -0.0695   0.5541   0.9801
   4.250   0.8006   0.00781   0.00299  -0.0720   0.5274   0.9971
   4.500   0.8237   0.00805   0.00313  -0.0713   0.5041   1.0000
   4.750   0.8453   0.00831   0.00330  -0.0702   0.4809   1.0000
   5.000   0.8674   0.00859   0.00348  -0.0693   0.4571   1.0000
   5.500   0.9119   0.00919   0.00392  -0.0674   0.4099   1.0000
   5.750   0.9337   0.00953   0.00416  -0.0664   0.3868   1.0000
   6.000   0.9556   0.00987   0.00441  -0.0655   0.3621   1.0000
   6.250   0.9771   0.01024   0.00469  -0.0645   0.3386   1.0000
   6.500   0.9980   0.01064   0.00499  -0.0634   0.3143   1.0000
   6.750   1.0192   0.01103   0.00530  -0.0623   0.2910   1.0000
   7.000   1.0393   0.01146   0.00564  -0.0612   0.2682   1.0000
   7.250   1.0593   0.01191   0.00599  -0.0600   0.2438   1.0000
   7.500   1.0783   0.01241   0.00638  -0.0586   0.2189   1.0000
   7.750   1.0965   0.01294   0.00680  -0.0572   0.1962   1.0000
   8.000   1.1152   0.01342   0.00721  -0.0558   0.1753   1.0000
   8.250   1.1319   0.01400   0.00767  -0.0542   0.1544   1.0000
   8.500   1.1481   0.01452   0.00813  -0.0524   0.1361   1.0000
   8.750   1.1626   0.01510   0.00862  -0.0503   0.1182   1.0000
   9.000   1.1771   0.01568   0.00914  -0.0483   0.1037   1.0000
   9.250   1.1917   0.01627   0.00969  -0.0463   0.0910   1.0000
   9.500   1.2056   0.01691   0.01028  -0.0443   0.0787   1.0000
   9.750   1.2188   0.01760   0.01092  -0.0423   0.0667   1.0000
  10.000   1.2309   0.01837   0.01165  -0.0403   0.0548   1.0000
  10.250   1.2411   0.01926   0.01248  -0.0380   0.0427   1.0000
  10.500   1.2472   0.02045   0.01356  -0.0354   0.0276   1.0000
  10.750   1.2520   0.02177   0.01483  -0.0327   0.0182   1.0000
  11.000   1.2593   0.02298   0.01607  -0.0304   0.0156   1.0000
  11.250   1.2693   0.02403   0.01719  -0.0286   0.0140   1.0000
  11.500   1.2760   0.02534   0.01856  -0.0266   0.0129   1.0000
  11.750   1.2793   0.02695   0.02026  -0.0245   0.0122   1.0000
  12.000   1.2874   0.02826   0.02167  -0.0229   0.0118   1.0000
  12.250   1.2938   0.02973   0.02324  -0.0214   0.0114   1.0000
  12.500   1.2988   0.03138   0.02497  -0.0199   0.0109   1.0000
  12.750   1.3027   0.03316   0.02685  -0.0185   0.0106   1.0000
  13.000   1.3057   0.03510   0.02887  -0.0172   0.0103   1.0000
  13.250   1.3076   0.03719   0.03106  -0.0161   0.0101   1.0000
  13.500   1.3059   0.03971   0.03367  -0.0150   0.0098   1.0000
  13.750   1.3020   0.04256   0.03662  -0.0141   0.0096   1.0000
  14.000   1.2957   0.04578   0.03995  -0.0134   0.0094   1.0000
  14.250   1.2909   0.04901   0.04329  -0.0130   0.0094   1.0000
  14.500   1.2845   0.05258   0.04699  -0.0129   0.0092   1.0000
  14.750   1.2845   0.05558   0.05010  -0.0130   0.0092   1.0000
  15.000   1.2842   0.05874   0.05337  -0.0133   0.0091   1.0000
  15.250   1.2814   0.06229   0.05704  -0.0138   0.0091   1.0000
  15.500   1.2794   0.06593   0.06082  -0.0146   0.0088   1.0000
  15.750   1.2771   0.06969   0.06469  -0.0155   0.0088   1.0000
  16.000   1.2741   0.07365   0.06878  -0.0166   0.0087   1.0000
  16.250   1.2702   0.07791   0.07317  -0.0180   0.0085   1.0000
  16.500   1.2666   0.08221   0.07758  -0.0196   0.0085   1.0000
  16.750   1.2616   0.08685   0.08235  -0.0214   0.0083   1.0000
  17.000   1.2559   0.09169   0.08732  -0.0233   0.0083   1.0000
  17.250   1.2501   0.09664   0.09240  -0.0254   0.0083   1.0000
  17.500   1.2440   0.10179   0.09768  -0.0278   0.0082   1.0000
  17.750   1.2359   0.10736   0.10339  -0.0304   0.0082   1.0000
  18.000   1.2293   0.11282   0.10897  -0.0332   0.0081   1.0000
  18.250   1.2204   0.11881   0.11511  -0.0363   0.0081   1.0000
  18.500   1.2110   0.12503   0.12148  -0.0397   0.0081   1.0000
  18.750   1.2026   0.13120   0.12778  -0.0432   0.0081   1.0000
  19.000   1.1915   0.13804   0.13476  -0.0472   0.0081   1.0000
  19.250   1.1803   0.14507   0.14195  -0.0515   0.0081   1.0000
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