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PSU-90-125WL (psu-90-125wl-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: PSU-90-125WL (psu-90-125wl-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.7 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-psu-90-125wl-il-1000000.txt
Download as CSV file: xf-psu-90-125wl-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.7718   0.03842   0.03565  -0.0784   1.0000   0.0103
 -11.500  -0.7962   0.03620   0.03328  -0.0748   1.0000   0.0102
 -11.250  -0.8163   0.03479   0.03179  -0.0697   0.9995   0.0103
 -11.000  -0.7990   0.03132   0.02805  -0.0730   0.9956   0.0104
 -10.750  -0.7751   0.02963   0.02626  -0.0751   0.9925   0.0106
 -10.500  -0.7523   0.02766   0.02412  -0.0768   0.9884   0.0108
 -10.250  -0.7265   0.02566   0.02193  -0.0788   0.9855   0.0110
 -10.000  -0.6963   0.02442   0.02059  -0.0809   0.9836   0.0113
  -9.750  -0.6733   0.02307   0.01908  -0.0813   0.9770   0.0117
  -9.500  -0.6447   0.02155   0.01737  -0.0828   0.9728   0.0121
  -9.250  -0.6203   0.02012   0.01576  -0.0832   0.9640   0.0122
  -9.000  -0.5914   0.01887   0.01434  -0.0842   0.9564   0.0124
  -8.750  -0.5650   0.01776   0.01308  -0.0846   0.9444   0.0126
  -8.500  -0.5385   0.01708   0.01227  -0.0848   0.9308   0.0128
  -8.250  -0.5141   0.01639   0.01143  -0.0844   0.9163   0.0129
  -8.000  -0.4912   0.01565   0.01055  -0.0838   0.9024   0.0130
  -7.750  -0.4733   0.01405   0.00879  -0.0824   0.8892   0.0134
  -7.500  -0.4524   0.01319   0.00783  -0.0815   0.8784   0.0137
  -7.250  -0.4296   0.01261   0.00717  -0.0808   0.8689   0.0141
  -7.000  -0.4054   0.01219   0.00670  -0.0803   0.8603   0.0147
  -6.750  -0.3811   0.01177   0.00619  -0.0798   0.8526   0.0151
  -6.500  -0.3565   0.01134   0.00570  -0.0793   0.8451   0.0155
  -6.000  -0.3060   0.01062   0.00484  -0.0785   0.8317   0.0163
  -5.750  -0.2803   0.01032   0.00446  -0.0782   0.8254   0.0167
  -5.500  -0.2542   0.01001   0.00409  -0.0779   0.8197   0.0170
  -5.250  -0.2288   0.00957   0.00358  -0.0775   0.8138   0.0179
  -5.000  -0.2026   0.00929   0.00324  -0.0773   0.8084   0.0192
  -4.750  -0.1757   0.00906   0.00298  -0.0771   0.8032   0.0206
  -4.500  -0.1486   0.00886   0.00273  -0.0770   0.7978   0.0224
  -4.250  -0.1221   0.00860   0.00248  -0.0767   0.7927   0.0310
  -4.000  -0.0970   0.00806   0.00220  -0.0765   0.7878   0.0857
  -3.750  -0.0708   0.00772   0.00202  -0.0764   0.7827   0.1305
  -3.500  -0.0445   0.00743   0.00186  -0.0762   0.7779   0.1781
  -3.250  -0.0179   0.00712   0.00174  -0.0762   0.7732   0.2284
  -3.000   0.0088   0.00683   0.00162  -0.0761   0.7684   0.2819
  -2.750   0.0355   0.00658   0.00152  -0.0761   0.7637   0.3374
  -2.500   0.0624   0.00632   0.00144  -0.0760   0.7590   0.3962
  -2.250   0.0896   0.00611   0.00137  -0.0760   0.7540   0.4449
  -2.000   0.1162   0.00587   0.00131  -0.0758   0.7490   0.5120
  -1.750   0.1433   0.00571   0.00131  -0.0757   0.7440   0.5693
  -1.500   0.1712   0.00564   0.00129  -0.0757   0.7387   0.5971
  -1.250   0.1992   0.00562   0.00128  -0.0757   0.7335   0.6167
  -1.000   0.2275   0.00560   0.00128  -0.0757   0.7284   0.6341
  -0.750   0.2557   0.00558   0.00127  -0.0758   0.7228   0.6494
  -0.500   0.2836   0.00559   0.00126  -0.0757   0.7170   0.6628
  -0.250   0.3119   0.00556   0.00127  -0.0758   0.7110   0.6751
   0.000   0.3399   0.00557   0.00127  -0.0758   0.7043   0.6865
   0.250   0.3680   0.00557   0.00128  -0.0758   0.6977   0.6979
   0.500   0.3959   0.00557   0.00129  -0.0757   0.6903   0.7085
   0.750   0.4239   0.00558   0.00130  -0.0757   0.6828   0.7184
   1.000   0.4517   0.00560   0.00132  -0.0757   0.6741   0.7284
   1.250   0.4795   0.00560   0.00134  -0.0756   0.6650   0.7382
   1.500   0.5069   0.00563   0.00137  -0.0755   0.6545   0.7485
   1.750   0.5341   0.00568   0.00140  -0.0753   0.6418   0.7593
   2.000   0.5610   0.00572   0.00143  -0.0751   0.6271   0.7696
   2.250   0.5877   0.00578   0.00149  -0.0748   0.6107   0.7803
   2.500   0.6141   0.00587   0.00154  -0.0745   0.5919   0.7919
   2.750   0.6397   0.00598   0.00162  -0.0741   0.5707   0.8041
   3.000   0.6650   0.00611   0.00172  -0.0736   0.5494   0.8169
   3.250   0.6901   0.00625   0.00183  -0.0730   0.5273   0.8305
   3.500   0.7147   0.00642   0.00195  -0.0724   0.5045   0.8454
   3.750   0.7391   0.00657   0.00209  -0.0717   0.4821   0.8621
   4.000   0.7627   0.00674   0.00223  -0.0708   0.4601   0.8812
   4.250   0.7855   0.00689   0.00237  -0.0698   0.4381   0.9029
   4.500   0.8068   0.00705   0.00252  -0.0684   0.4173   0.9304
   4.750   0.8324   0.00723   0.00268  -0.0680   0.3942   0.9632
   5.000   0.8689   0.00751   0.00286  -0.0701   0.3694   0.9908
   5.250   0.8956   0.00779   0.00304  -0.0702   0.3460   1.0000
   5.500   0.9191   0.00807   0.00324  -0.0695   0.3244   1.0000
   5.750   0.9425   0.00837   0.00344  -0.0688   0.3024   1.0000
   6.000   0.9653   0.00870   0.00367  -0.0680   0.2791   1.0000
   6.250   0.9874   0.00907   0.00392  -0.0672   0.2540   1.0000
   6.500   1.0097   0.00943   0.00418  -0.0663   0.2301   1.0000
   6.750   1.0312   0.00984   0.00447  -0.0653   0.2058   1.0000
   7.000   1.0525   0.01025   0.00477  -0.0644   0.1839   1.0000
   7.250   1.0740   0.01064   0.00507  -0.0634   0.1652   1.0000
   7.500   1.0947   0.01107   0.00541  -0.0623   0.1453   1.0000
   7.750   1.1145   0.01154   0.00577  -0.0611   0.1261   1.0000
   8.000   1.1350   0.01195   0.00612  -0.0600   0.1118   1.0000
   8.250   1.1544   0.01241   0.00650  -0.0587   0.0962   1.0000
   8.500   1.1730   0.01290   0.00692  -0.0573   0.0816   1.0000
   8.750   1.1908   0.01339   0.00734  -0.0558   0.0689   1.0000
   9.000   1.2063   0.01390   0.00778  -0.0538   0.0571   1.0000
   9.250   1.2206   0.01444   0.00826  -0.0516   0.0465   1.0000
   9.500   1.2329   0.01509   0.00883  -0.0492   0.0349   1.0000
   9.750   1.2420   0.01594   0.00958  -0.0464   0.0208   1.0000
  10.000   1.2507   0.01684   0.01042  -0.0435   0.0115   1.0000
  10.250   1.2645   0.01746   0.01106  -0.0416   0.0102   1.0000
  10.500   1.2773   0.01817   0.01180  -0.0395   0.0090   1.0000
  10.750   1.2907   0.01884   0.01254  -0.0377   0.0084   1.0000
  11.000   1.3036   0.01956   0.01331  -0.0358   0.0081   1.0000
  11.250   1.3145   0.02042   0.01422  -0.0338   0.0075   1.0000
  11.500   1.3230   0.02147   0.01534  -0.0316   0.0071   1.0000
  11.750   1.3298   0.02267   0.01663  -0.0294   0.0069   1.0000
  12.000   1.3404   0.02363   0.01766  -0.0277   0.0068   1.0000
  12.250   1.3504   0.02468   0.01877  -0.0261   0.0066   1.0000
  12.500   1.3590   0.02586   0.02002  -0.0245   0.0064   1.0000
  12.750   1.3662   0.02718   0.02142  -0.0228   0.0062   1.0000
  13.000   1.3736   0.02853   0.02284  -0.0214   0.0060   1.0000
  13.250   1.3795   0.03004   0.02443  -0.0199   0.0059   1.0000
  13.500   1.3857   0.03158   0.02604  -0.0187   0.0056   1.0000
  13.750   1.3885   0.03346   0.02800  -0.0174   0.0055   1.0000
  14.000   1.3899   0.03553   0.03016  -0.0162   0.0054   1.0000
  14.250   1.3903   0.03780   0.03252  -0.0151   0.0054   1.0000
  14.500   1.3892   0.04029   0.03511  -0.0143   0.0053   1.0000
  14.750   1.3841   0.04331   0.03824  -0.0136   0.0052   1.0000
  15.000   1.3792   0.04649   0.04153  -0.0132   0.0051   1.0000
  15.250   1.3764   0.04958   0.04472  -0.0131   0.0051   1.0000
  15.500   1.3532   0.05535   0.05067  -0.0135   0.0050   1.0000
  15.750   1.3515   0.05874   0.05415  -0.0141   0.0050   1.0000
  16.000   1.3491   0.06236   0.05787  -0.0149   0.0050   1.0000
  16.250   1.3359   0.06765   0.06330  -0.0163   0.0049   1.0000
  16.500   1.3301   0.07210   0.06785  -0.0178   0.0049   1.0000
  16.750   1.3261   0.07644   0.07230  -0.0194   0.0049   1.0000
  17.000   1.3184   0.08146   0.07744  -0.0213   0.0048   1.0000
  17.250   1.3088   0.08691   0.08300  -0.0236   0.0049   1.0000
  17.500   1.3026   0.09199   0.08820  -0.0259   0.0049   1.0000
  17.750   1.2924   0.09784   0.09416  -0.0285   0.0048   1.0000
  18.000   1.2870   0.10304   0.09947  -0.0311   0.0048   1.0000
  18.250   1.2761   0.10922   0.10576  -0.0342   0.0048   1.0000
  18.500   1.2663   0.11529   0.11195  -0.0373   0.0048   1.0000
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