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PSU-90-125WL (psu-90-125wl-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: PSU-90-125WL (psu-90-125wl-il)
Reynolds number: 1,000,000
Max Cl/Cd: 97.75 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-psu-90-125wl-il-1000000-n5.txt
Download as CSV file: xf-psu-90-125wl-il-1000000-n5.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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.7452   0.08076   0.07860  -0.0532   1.0000   0.0072
 -14.500  -0.7835   0.06923   0.06692  -0.0603   1.0000   0.0072
 -14.250  -0.8217   0.05813   0.05562  -0.0679   1.0000   0.0071
 -14.000  -0.8419   0.05094   0.04828  -0.0730   1.0000   0.0071
 -13.750  -0.8548   0.04563   0.04282  -0.0765   1.0000   0.0071
 -13.500  -0.8682   0.04096   0.03800  -0.0791   1.0000   0.0072
 -13.250  -0.8755   0.03761   0.03453  -0.0803   1.0000   0.0072
 -13.000  -0.8826   0.03479   0.03159  -0.0806   1.0000   0.0073
 -12.750  -0.8853   0.03283   0.02954  -0.0799   1.0000   0.0073
 -12.500  -0.8956   0.03080   0.02739  -0.0779   1.0000   0.0074
 -12.000  -0.8769   0.02757   0.02391  -0.0783   0.9935   0.0075
 -11.750  -0.8607   0.02591   0.02209  -0.0789   0.9878   0.0076
 -11.250  -0.8159   0.02354   0.01946  -0.0806   0.9779   0.0077
 -11.000  -0.7902   0.02232   0.01811  -0.0819   0.9721   0.0077
 -10.750  -0.7661   0.02110   0.01675  -0.0827   0.9628   0.0078
 -10.500  -0.7439   0.01910   0.01455  -0.0837   0.9497   0.0080
 -10.250  -0.7179   0.01797   0.01328  -0.0845   0.9339   0.0082
 -10.000  -0.6946   0.01719   0.01235  -0.0844   0.9155   0.0083
  -9.750  -0.6738   0.01655   0.01157  -0.0837   0.8982   0.0084
  -9.500  -0.6528   0.01600   0.01091  -0.0828   0.8834   0.0086
  -9.250  -0.6316   0.01545   0.01024  -0.0820   0.8706   0.0087
  -9.000  -0.6094   0.01496   0.00966  -0.0813   0.8601   0.0089
  -8.750  -0.5868   0.01448   0.00909  -0.0807   0.8512   0.0090
  -8.500  -0.5636   0.01404   0.00856  -0.0801   0.8425   0.0092
  -8.250  -0.5398   0.01363   0.00808  -0.0796   0.8348   0.0095
  -8.000  -0.5157   0.01325   0.00762  -0.0791   0.8271   0.0098
  -7.750  -0.4916   0.01283   0.00712  -0.0786   0.8207   0.0100
  -7.500  -0.4671   0.01242   0.00663  -0.0782   0.8143   0.0102
  -7.250  -0.4423   0.01206   0.00619  -0.0778   0.8085   0.0104
  -7.000  -0.4169   0.01171   0.00580  -0.0775   0.8026   0.0106
  -6.750  -0.3914   0.01141   0.00542  -0.0772   0.7970   0.0108
  -6.500  -0.3656   0.01111   0.00508  -0.0770   0.7919   0.0109
  -6.250  -0.3394   0.01085   0.00476  -0.0768   0.7863   0.0110
  -6.000  -0.3144   0.01044   0.00426  -0.0764   0.7808   0.0114
  -5.750  -0.2882   0.01011   0.00389  -0.0761   0.7758   0.0118
  -5.500  -0.2618   0.00984   0.00358  -0.0760   0.7706   0.0122
  -5.250  -0.2352   0.00963   0.00332  -0.0758   0.7658   0.0127
  -5.000  -0.2081   0.00941   0.00308  -0.0757   0.7612   0.0132
  -4.750  -0.1810   0.00923   0.00286  -0.0756   0.7561   0.0138
  -4.500  -0.1539   0.00908   0.00267  -0.0755   0.7513   0.0146
  -4.250  -0.1263   0.00893   0.00250  -0.0755   0.7468   0.0151
  -4.000  -0.0989   0.00876   0.00230  -0.0754   0.7417   0.0169
  -3.750  -0.0717   0.00861   0.00213  -0.0753   0.7369   0.0197
  -3.500  -0.0449   0.00833   0.00195  -0.0752   0.7324   0.0427
  -3.250  -0.0180   0.00807   0.00179  -0.0752   0.7274   0.0704
  -3.000   0.0088   0.00783   0.00165  -0.0751   0.7226   0.1030
  -2.750   0.0358   0.00759   0.00153  -0.0751   0.7180   0.1405
  -2.500   0.0628   0.00733   0.00142  -0.0751   0.7127   0.1837
  -2.250   0.0896   0.00709   0.00132  -0.0750   0.7073   0.2336
  -2.000   0.1170   0.00691   0.00124  -0.0750   0.7018   0.2716
  -1.750   0.1439   0.00667   0.00117  -0.0750   0.6954   0.3260
  -1.500   0.1705   0.00640   0.00111  -0.0750   0.6895   0.3962
  -1.250   0.1977   0.00620   0.00106  -0.0750   0.6829   0.4493
  -1.000   0.2249   0.00607   0.00103  -0.0749   0.6763   0.4932
  -0.750   0.2526   0.00596   0.00102  -0.0749   0.6689   0.5304
  -0.500   0.2801   0.00591   0.00102  -0.0748   0.6607   0.5603
  -0.250   0.3079   0.00588   0.00102  -0.0748   0.6506   0.5832
   0.000   0.3355   0.00588   0.00103  -0.0748   0.6395   0.6025
   0.250   0.3629   0.00590   0.00104  -0.0747   0.6264   0.6189
   0.500   0.3902   0.00594   0.00107  -0.0745   0.6118   0.6326
   0.750   0.4173   0.00601   0.00109  -0.0744   0.5949   0.6446
   1.000   0.4441   0.00610   0.00114  -0.0742   0.5763   0.6558
   1.250   0.4706   0.00620   0.00119  -0.0739   0.5569   0.6662
   1.500   0.4970   0.00633   0.00126  -0.0737   0.5359   0.6768
   1.750   0.5231   0.00647   0.00134  -0.0734   0.5149   0.6876
   2.000   0.5494   0.00660   0.00142  -0.0731   0.4943   0.6978
   2.250   0.5754   0.00676   0.00152  -0.0728   0.4731   0.7074
   2.500   0.6015   0.00691   0.00162  -0.0725   0.4535   0.7175
   2.750   0.6274   0.00705   0.00173  -0.0721   0.4337   0.7279
   3.000   0.6531   0.00722   0.00185  -0.0718   0.4142   0.7383
   3.250   0.6788   0.00739   0.00198  -0.0714   0.3946   0.7488
   3.500   0.7042   0.00757   0.00211  -0.0710   0.3741   0.7598
   3.750   0.7291   0.00777   0.00226  -0.0706   0.3535   0.7712
   4.000   0.7543   0.00795   0.00241  -0.0701   0.3350   0.7833
   4.250   0.7793   0.00814   0.00257  -0.0697   0.3167   0.7959
   4.750   0.8280   0.00856   0.00293  -0.0685   0.2799   0.8223
   5.000   0.8522   0.00876   0.00311  -0.0679   0.2630   0.8369
   5.500   0.8983   0.00919   0.00352  -0.0662   0.2276   0.8726
   5.750   0.9194   0.00946   0.00377  -0.0650   0.2080   0.8963
   6.000   0.9386   0.00972   0.00402  -0.0633   0.1850   0.9299
   6.250   0.9672   0.01013   0.00433  -0.0638   0.1573   0.9794
   6.500   0.9925   0.01049   0.00460  -0.0637   0.1408   1.0000
   6.750   1.0143   0.01087   0.00489  -0.0628   0.1236   1.0000
   7.000   1.0353   0.01130   0.00523  -0.0618   0.1045   1.0000
   7.250   1.0558   0.01174   0.00558  -0.0607   0.0881   1.0000
   7.500   1.0770   0.01213   0.00591  -0.0597   0.0763   1.0000
   7.750   1.0977   0.01252   0.00625  -0.0586   0.0655   1.0000
   8.000   1.1176   0.01295   0.00663  -0.0574   0.0547   1.0000
   8.250   1.1352   0.01350   0.00709  -0.0558   0.0414   1.0000
   8.750   1.1680   0.01449   0.00798  -0.0522   0.0242   1.0000
   9.000   1.1799   0.01516   0.00858  -0.0497   0.0130   1.0000
   9.250   1.1932   0.01579   0.00918  -0.0474   0.0076   1.0000
   9.500   1.2099   0.01624   0.00966  -0.0458   0.0068   1.0000
   9.750   1.2254   0.01676   0.01020  -0.0440   0.0060   1.0000
  10.000   1.2407   0.01730   0.01078  -0.0422   0.0054   1.0000
  10.250   1.2561   0.01785   0.01136  -0.0405   0.0051   1.0000
  10.500   1.2715   0.01839   0.01195  -0.0389   0.0050   1.0000
  10.750   1.2858   0.01901   0.01262  -0.0372   0.0048   1.0000
  11.000   1.2995   0.01968   0.01334  -0.0355   0.0046   1.0000
  11.250   1.3130   0.02038   0.01409  -0.0338   0.0044   1.0000
  11.500   1.3254   0.02116   0.01493  -0.0321   0.0043   1.0000
  11.750   1.3375   0.02198   0.01580  -0.0305   0.0041   1.0000
  12.000   1.3481   0.02294   0.01681  -0.0288   0.0039   1.0000
  12.250   1.3580   0.02396   0.01789  -0.0271   0.0038   1.0000
  12.500   1.3676   0.02505   0.01904  -0.0255   0.0037   1.0000
  12.750   1.3749   0.02634   0.02041  -0.0238   0.0036   1.0000
  13.000   1.3817   0.02770   0.02186  -0.0223   0.0034   1.0000
  13.250   1.3878   0.02917   0.02341  -0.0207   0.0034   1.0000
  13.500   1.3982   0.03034   0.02463  -0.0197   0.0033   1.0000
  13.750   1.4047   0.03186   0.02624  -0.0185   0.0033   1.0000
  14.000   1.4122   0.03334   0.02779  -0.0175   0.0032   1.0000
  14.250   1.4158   0.03521   0.02975  -0.0164   0.0032   1.0000
  14.500   1.4194   0.03716   0.03178  -0.0154   0.0031   1.0000
  14.750   1.4239   0.03907   0.03377  -0.0147   0.0030   1.0000
  15.000   1.4259   0.04130   0.03609  -0.0140   0.0030   1.0000
  15.250   1.4258   0.04385   0.03874  -0.0135   0.0030   1.0000
  15.500   1.4271   0.04636   0.04134  -0.0132   0.0029   1.0000
  15.750   1.4253   0.04933   0.04442  -0.0131   0.0029   1.0000
  16.000   1.4237   0.05241   0.04760  -0.0133   0.0028   1.0000
  16.250   1.4226   0.05559   0.05087  -0.0136   0.0028   1.0000
  16.500   1.4172   0.05947   0.05487  -0.0144   0.0028   1.0000
  16.750   1.4136   0.06325   0.05875  -0.0153   0.0027   1.0000
  17.000   1.4071   0.06763   0.06325  -0.0166   0.0027   1.0000
  17.250   1.3987   0.07248   0.06822  -0.0183   0.0027   1.0000
  17.500   1.3877   0.07790   0.07377  -0.0203   0.0027   1.0000
  17.750   1.3774   0.08342   0.07941  -0.0226   0.0027   1.0000
  18.000   1.3674   0.08907   0.08518  -0.0252   0.0026   1.0000
  18.250   1.3549   0.09528   0.09151  -0.0281   0.0026   1.0000
  18.500   1.3402   0.10207   0.09843  -0.0314   0.0026   1.0000
  18.750   1.3237   0.10939   0.10589  -0.0351   0.0026   1.0000
  19.000   1.3091   0.11647   0.11309  -0.0389   0.0026   1.0000
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