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NACA 0010-66 (naca001066-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 0010-66 (naca001066-il)
Reynolds number: 500,000
Max Cl/Cd: 47.13 at α=10.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca001066-il-500000-n5.txt
Download as CSV file: xf-naca001066-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0010-66                                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -1.0721   0.06953   0.06668  -0.0526   1.0000   0.0078
 -15.500  -1.1280   0.05560   0.05244  -0.0612   1.0000   0.0076
 -15.250  -1.1577   0.05056   0.04721  -0.0601   1.0000   0.0076
 -15.000  -1.1765   0.04654   0.04298  -0.0586   0.9995   0.0076
 -14.750  -1.1878   0.04324   0.03948  -0.0568   0.9986   0.0077
 -14.500  -1.1948   0.04051   0.03652  -0.0546   0.9975   0.0078
 -14.250  -1.1977   0.03817   0.03397  -0.0523   0.9964   0.0079
 -14.000  -1.1973   0.03618   0.03177  -0.0498   0.9955   0.0080
 -13.750  -1.1975   0.03422   0.02962  -0.0471   0.9947   0.0082
 -13.500  -1.1968   0.03261   0.02785  -0.0438   0.9934   0.0084
 -13.250  -1.1925   0.03128   0.02638  -0.0408   0.9919   0.0087
 -13.000  -1.1848   0.03010   0.02504  -0.0382   0.9905   0.0090
 -12.750  -1.1739   0.02902   0.02382  -0.0360   0.9891   0.0093
 -12.500  -1.1609   0.02798   0.02263  -0.0342   0.9879   0.0096
 -12.250  -1.1466   0.02701   0.02151  -0.0325   0.9870   0.0100
 -12.000  -1.1308   0.02609   0.02043  -0.0310   0.9862   0.0105
 -11.750  -1.1130   0.02524   0.01942  -0.0298   0.9855   0.0109
 -11.500  -1.1073   0.02449   0.01857  -0.0258   0.9830   0.0115
 -11.250  -1.0925   0.02387   0.01789  -0.0238   0.9813   0.0122
 -11.000  -1.0735   0.02330   0.01723  -0.0226   0.9800   0.0129
 -10.750  -1.0526   0.02268   0.01651  -0.0217   0.9789   0.0137
 -10.500  -1.0311   0.02204   0.01574  -0.0210   0.9780   0.0146
 -10.250  -1.0092   0.02142   0.01504  -0.0203   0.9772   0.0155
 -10.000  -0.9851   0.02107   0.01466  -0.0201   0.9765   0.0166
  -9.750  -0.9600   0.02076   0.01430  -0.0200   0.9760   0.0178
  -9.500  -0.9349   0.02039   0.01383  -0.0199   0.9755   0.0191
  -9.250  -0.9231   0.02011   0.01346  -0.0166   0.9730   0.0199
  -9.000  -0.9064   0.01964   0.01292  -0.0146   0.9712   0.0208
  -8.750  -0.8852   0.01927   0.01253  -0.0136   0.9698   0.0219
  -8.500  -0.8614   0.01900   0.01223  -0.0131   0.9686   0.0231
  -8.250  -0.8372   0.01872   0.01189  -0.0127   0.9676   0.0244
  -8.000  -0.8127   0.01840   0.01148  -0.0123   0.9668   0.0256
  -7.750  -0.7874   0.01811   0.01112  -0.0121   0.9662   0.0264
  -7.500  -0.7618   0.01782   0.01076  -0.0119   0.9656   0.0271
  -7.250  -0.7381   0.01712   0.01002  -0.0115   0.9650   0.0287
  -7.000  -0.7124   0.01674   0.00961  -0.0114   0.9646   0.0300
  -6.750  -0.6860   0.01642   0.00925  -0.0114   0.9642   0.0311
  -6.500  -0.6797   0.01625   0.00904  -0.0067   0.9604   0.0319
  -6.250  -0.6594   0.01598   0.00872  -0.0053   0.9586   0.0329
  -6.000  -0.6370   0.01570   0.00840  -0.0043   0.9574   0.0339
  -5.750  -0.6135   0.01542   0.00807  -0.0035   0.9563   0.0346
  -5.500  -0.5891   0.01516   0.00776  -0.0030   0.9554   0.0351
  -5.250  -0.5645   0.01484   0.00740  -0.0025   0.9546   0.0364
  -5.000  -0.5393   0.01453   0.00708  -0.0022   0.9539   0.0382
  -4.750  -0.5134   0.01428   0.00681  -0.0020   0.9533   0.0397
  -4.500  -0.4868   0.01406   0.00659  -0.0019   0.9528   0.0415
  -4.250  -0.4594   0.01386   0.00638  -0.0020   0.9523   0.0434
  -4.000  -0.4315   0.01368   0.00618  -0.0022   0.9518   0.0457
  -3.750  -0.4236   0.01360   0.00611   0.0022   0.9483   0.0501
  -3.500  -0.4063   0.01348   0.00601   0.0044   0.9461   0.0572
  -3.250  -0.3848   0.01328   0.00590   0.0056   0.9447   0.0731
  -3.000  -0.3618   0.01309   0.00580   0.0065   0.9435   0.0934
  -2.750  -0.3375   0.01290   0.00570   0.0071   0.9424   0.1137
  -2.500  -0.3123   0.01269   0.00560   0.0074   0.9415   0.1383
  -2.250  -0.2871   0.01248   0.00551   0.0078   0.9406   0.1681
  -2.000  -0.2623   0.01224   0.00544   0.0082   0.9399   0.2073
  -1.750  -0.2384   0.01193   0.00538   0.0088   0.9393   0.2680
  -1.500  -0.2156   0.01155   0.00531   0.0096   0.9386   0.3451
  -1.000  -0.2069   0.01067   0.00523   0.0197   0.9317   0.5491
  -0.500  -0.1241   0.01009   0.00606   0.0143   0.9309   0.9098
  -0.250  -0.0682   0.01026   0.00622   0.0083   0.9289   0.9166
   0.000   0.0000   0.01008   0.00603   0.0000   0.9253   0.9253
   0.250   0.0681   0.01026   0.00622  -0.0083   0.9166   0.9289
   0.500   0.1258   0.01007   0.00603  -0.0146   0.9096   0.9307
   1.000   0.1723   0.00969   0.00561  -0.0120   0.8639   0.9383
   1.500   0.2155   0.01156   0.00531  -0.0096   0.3439   0.9386
   1.750   0.2384   0.01193   0.00538  -0.0088   0.2685   0.9393
   2.000   0.2623   0.01224   0.00544  -0.0082   0.2070   0.9399
   2.250   0.2871   0.01248   0.00551  -0.0078   0.1676   0.9406
   2.500   0.3122   0.01269   0.00560  -0.0074   0.1381   0.9415
   2.750   0.3374   0.01290   0.00570  -0.0070   0.1139   0.9424
   3.000   0.3617   0.01308   0.00580  -0.0065   0.0935   0.9435
   3.250   0.3848   0.01328   0.00590  -0.0056   0.0731   0.9447
   3.500   0.4062   0.01347   0.00601  -0.0044   0.0573   0.9461
   3.750   0.4234   0.01360   0.00611  -0.0022   0.0501   0.9484
   4.000   0.4316   0.01368   0.00618   0.0022   0.0457   0.9518
   4.250   0.4596   0.01386   0.00638   0.0020   0.0434   0.9523
   4.500   0.4869   0.01406   0.00659   0.0019   0.0414   0.9528
   4.750   0.5134   0.01428   0.00681   0.0019   0.0397   0.9533
   5.000   0.5393   0.01453   0.00708   0.0021   0.0382   0.9539
   5.250   0.5645   0.01484   0.00740   0.0025   0.0364   0.9546
   5.500   0.5891   0.01516   0.00776   0.0030   0.0351   0.9554
   5.750   0.6135   0.01541   0.00806   0.0035   0.0345   0.9563
   6.000   0.6370   0.01570   0.00839   0.0043   0.0339   0.9574
   6.250   0.6594   0.01597   0.00872   0.0053   0.0329   0.9587
   6.500   0.6796   0.01624   0.00903   0.0067   0.0319   0.9605
   6.750   0.6860   0.01642   0.00925   0.0114   0.0311   0.9642
   7.000   0.7124   0.01674   0.00961   0.0113   0.0300   0.9646
   7.250   0.7382   0.01712   0.01001   0.0114   0.0287   0.9651
   7.500   0.7619   0.01782   0.01076   0.0119   0.0271   0.9656
   7.750   0.7876   0.01810   0.01111   0.0120   0.0264   0.9662
   8.000   0.8128   0.01840   0.01148   0.0123   0.0256   0.9669
   8.250   0.8373   0.01872   0.01189   0.0127   0.0244   0.9677
   8.500   0.8614   0.01900   0.01223   0.0131   0.0231   0.9686
   8.750   0.8852   0.01927   0.01253   0.0136   0.0219   0.9698
   9.000   0.9065   0.01963   0.01292   0.0146   0.0208   0.9712
   9.250   0.9230   0.02010   0.01345   0.0167   0.0199   0.9731
   9.500   0.9351   0.02038   0.01383   0.0198   0.0191   0.9755
   9.750   0.9604   0.02074   0.01428   0.0199   0.0178   0.9760
  10.000   0.9854   0.02106   0.01466   0.0200   0.0166   0.9766
  10.250   1.0096   0.02142   0.01503   0.0202   0.0154   0.9772
  10.500   1.0315   0.02204   0.01574   0.0209   0.0145   0.9780
  10.750   1.0531   0.02268   0.01650   0.0216   0.0137   0.9789
  11.000   1.0740   0.02329   0.01721   0.0224   0.0129   0.9801
  11.250   1.0929   0.02387   0.01788   0.0237   0.0122   0.9814
  11.500   1.1077   0.02449   0.01857   0.0258   0.0115   0.9831
  11.750   1.1138   0.02524   0.01941   0.0297   0.0109   0.9855
  12.000   1.1315   0.02609   0.02043   0.0309   0.0105   0.9862
  12.250   1.1474   0.02701   0.02151   0.0324   0.0100   0.9870
  12.500   1.1616   0.02799   0.02264   0.0341   0.0096   0.9880
  12.750   1.1748   0.02902   0.02382   0.0359   0.0093   0.9892
  13.000   1.1856   0.03010   0.02505   0.0380   0.0090   0.9905
  13.250   1.1933   0.03128   0.02638   0.0406   0.0087   0.9920
  13.500   1.1976   0.03261   0.02785   0.0436   0.0084   0.9935
  13.750   1.1984   0.03424   0.02964   0.0469   0.0082   0.9947
  14.000   1.1985   0.03619   0.03178   0.0496   0.0080   0.9956
  14.250   1.1988   0.03818   0.03398   0.0520   0.0079   0.9965
  14.500   1.1961   0.04051   0.03653   0.0543   0.0078   0.9976
  14.750   1.1892   0.04325   0.03949   0.0565   0.0077   0.9986
  15.000   1.1779   0.04656   0.04301   0.0583   0.0076   0.9995
  15.250   1.1586   0.05049   0.04715   0.0600   0.0075   1.0000
  15.500   1.1290   0.05551   0.05235   0.0612   0.0076   1.0000
  15.750   1.0733   0.06933   0.06648   0.0527   0.0078   1.0000
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