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NREL's S810 Airfoil (s810-nr) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NREL's S810 Airfoil (s810-nr)
Reynolds number: 1,000,000
Max Cl/Cd: 92.5 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s810-nr-1000000-n5.txt
Download as CSV file: xf-s810-nr-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NREL's S810 Airfoil                             
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.4944   0.08262   0.07961  -0.0768   0.7068   0.0029
 -12.250  -0.5166   0.07749   0.07440  -0.0782   0.7059   0.0031
 -12.000  -0.5419   0.07248   0.06929  -0.0786   0.7050   0.0028
 -11.750  -0.5613   0.06861   0.06533  -0.0783   0.7040   0.0028
 -11.500  -0.5855   0.06451   0.06112  -0.0771   0.7030   0.0028
 -11.000  -0.6190   0.05847   0.05487  -0.0736   0.7011   0.0028
 -10.750  -0.6333   0.05588   0.05219  -0.0711   0.7003   0.0029
 -10.500  -0.6467   0.05345   0.04965  -0.0681   0.6994   0.0030
 -10.250  -0.6646   0.05068   0.04674  -0.0636   0.6984   0.0028
 -10.000  -0.6697   0.04886   0.04481  -0.0604   0.6975   0.0031
  -9.750  -0.6737   0.04609   0.04188  -0.0573   0.6966   0.0031
  -9.500  -0.6721   0.04343   0.03905  -0.0546   0.6957   0.0032
  -9.250  -0.6681   0.04049   0.03592  -0.0519   0.6948   0.0035
  -9.000  -0.6593   0.03741   0.03262  -0.0496   0.6940   0.0038
  -8.750  -0.6482   0.03434   0.02932  -0.0475   0.6932   0.0038
  -8.500  -0.6311   0.03142   0.02618  -0.0460   0.6924   0.0040
  -8.250  -0.6090   0.02823   0.02276  -0.0452   0.6917   0.0040
  -8.000  -0.5728   0.02495   0.01924  -0.0462   0.6911   0.0043
  -7.750  -0.4901   0.02140   0.01537  -0.0537   0.6909   0.0044
  -7.250  -0.4188   0.01944   0.01313  -0.0534   0.6898   0.0047
  -7.000  -0.4014   0.01891   0.01255  -0.0524   0.6889   0.0046
  -6.750  -0.3931   0.01797   0.01154  -0.0501   0.6881   0.0049
  -6.500  -0.3817   0.01720   0.01074  -0.0484   0.6873   0.0051
  -6.250  -0.3653   0.01666   0.01019  -0.0475   0.6867   0.0054
  -6.000  -0.3513   0.01602   0.00952  -0.0462   0.6860   0.0056
  -5.750  -0.3392   0.01529   0.00877  -0.0447   0.6852   0.0059
  -5.500  -0.3271   0.01459   0.00804  -0.0431   0.6844   0.0061
  -5.250  -0.3155   0.01393   0.00735  -0.0414   0.6837   0.0065
  -5.000  -0.3120   0.01327   0.00666  -0.0383   0.6829   0.0066
  -4.750  -0.2988   0.01275   0.00608  -0.0366   0.6822   0.0067
  -4.500  -0.2810   0.01233   0.00561  -0.0355   0.6815   0.0071
  -4.250  -0.2610   0.01195   0.00519  -0.0348   0.6808   0.0073
  -4.000  -0.2382   0.01168   0.00490  -0.0345   0.6802   0.0076
  -3.750  -0.2171   0.01128   0.00445  -0.0339   0.6795   0.0083
  -3.500  -0.1936   0.01098   0.00413  -0.0336   0.6789   0.0093
  -3.250  -0.1685   0.01075   0.00389  -0.0337   0.6783   0.0104
  -3.000  -0.1426   0.01056   0.00368  -0.0338   0.6777   0.0119
  -2.750  -0.1168   0.01035   0.00347  -0.0340   0.6771   0.0152
  -2.500  -0.0899   0.01021   0.00332  -0.0343   0.6765   0.0189
  -2.250  -0.0631   0.01006   0.00317  -0.0346   0.6759   0.0251
  -2.000  -0.0371   0.00982   0.00300  -0.0348   0.6752   0.0598
  -1.750  -0.0337   0.00685   0.00171  -0.0330   0.6743   0.5630
  -1.500  -0.0047   0.00686   0.00176  -0.0336   0.6736   0.5897
  -1.250   0.0248   0.00689   0.00180  -0.0343   0.6732   0.5994
  -1.000   0.0544   0.00690   0.00180  -0.0350   0.6727   0.6030
  -0.750   0.0841   0.00693   0.00180  -0.0357   0.6723   0.6059
  -0.500   0.1136   0.00694   0.00180  -0.0365   0.6718   0.6083
  -0.250   0.1430   0.00697   0.00186  -0.0371   0.6713   0.6132
   0.000   0.1726   0.00700   0.00190  -0.0378   0.6707   0.6165
   0.250   0.2022   0.00701   0.00191  -0.0385   0.6700   0.6175
   0.500   0.2317   0.00702   0.00192  -0.0393   0.6693   0.6185
   0.750   0.2613   0.00704   0.00194  -0.0400   0.6686   0.6194
   1.000   0.2908   0.00706   0.00196  -0.0407   0.6679   0.6204
   1.250   0.3203   0.00708   0.00198  -0.0414   0.6671   0.6212
   1.500   0.3497   0.00708   0.00201  -0.0421   0.6661   0.6223
   1.750   0.3791   0.00708   0.00204  -0.0428   0.6650   0.6233
   2.000   0.4084   0.00707   0.00205  -0.0435   0.6633   0.6242
   2.250   0.4376   0.00706   0.00205  -0.0441   0.6607   0.6251
   2.500   0.4665   0.00703   0.00206  -0.0446   0.6569   0.6261
   2.750   0.4953   0.00696   0.00203  -0.0452   0.6515   0.6271
   3.000   0.5240   0.00693   0.00199  -0.0456   0.6459   0.6281
   3.250   0.5530   0.00690   0.00203  -0.0462   0.6397   0.6292
   3.500   0.5816   0.00688   0.00203  -0.0467   0.6329   0.6304
   3.750   0.6102   0.00687   0.00205  -0.0472   0.6222   0.6315
   4.000   0.6373   0.00689   0.00203  -0.0474   0.5963   0.6324
   4.250   0.6519   0.00757   0.00229  -0.0453   0.5005   0.6334
   4.500   0.6628   0.00851   0.00282  -0.0428   0.4077   0.6342
   4.750   0.6770   0.00922   0.00324  -0.0408   0.3417   0.6350
   5.000   0.6920   0.00980   0.00361  -0.0390   0.2891   0.6360
   5.250   0.7046   0.01043   0.00402  -0.0368   0.2363   0.6371
   5.500   0.7162   0.01103   0.00442  -0.0343   0.1895   0.6383
   5.750   0.7280   0.01153   0.00480  -0.0319   0.1563   0.6395
   6.000   0.7343   0.01202   0.00517  -0.0284   0.1253   0.6407
   6.250   0.7409   0.01265   0.00567  -0.0252   0.0941   0.6418
   6.500   0.7520   0.01322   0.00616  -0.0229   0.0744   0.6429
   6.750   0.7668   0.01369   0.00660  -0.0212   0.0640   0.6440
   7.000   0.7801   0.01425   0.00711  -0.0195   0.0507   0.6451
   7.250   0.7938   0.01482   0.00764  -0.0179   0.0400   0.6461
   7.750   0.8244   0.01594   0.00874  -0.0154   0.0276   0.6482
   8.000   0.8389   0.01658   0.00935  -0.0141   0.0211   0.6491
   8.250   0.8566   0.01706   0.00987  -0.0133   0.0202   0.6504
   8.500   0.8719   0.01768   0.01050  -0.0122   0.0162   0.6517
   8.750   0.8867   0.01835   0.01117  -0.0111   0.0116   0.6529
   9.000   0.8985   0.01921   0.01200  -0.0096   0.0057   0.6541
   9.250   0.9146   0.01985   0.01267  -0.0087   0.0051   0.6552
   9.500   0.9291   0.02060   0.01347  -0.0077   0.0037   0.6564
   9.750   0.9448   0.02128   0.01420  -0.0068   0.0035   0.6577
  10.000   0.9606   0.02197   0.01494  -0.0060   0.0034   0.6589
  10.250   0.9745   0.02280   0.01582  -0.0049   0.0030   0.6600
  10.500   0.9902   0.02351   0.01659  -0.0042   0.0030   0.6612
  10.750   1.0045   0.02434   0.01745  -0.0033   0.0027   0.6622
  11.250   1.0306   0.02618   0.01942  -0.0013   0.0024   0.6649
  11.500   1.0445   0.02705   0.02037  -0.0005   0.0023   0.6664
  11.750   1.0539   0.02828   0.02170   0.0008   0.0021   0.6677
  12.000   1.0642   0.02947   0.02298   0.0019   0.0021   0.6691
  12.250   1.0741   0.03071   0.02431   0.0029   0.0020   0.6704
  12.500   1.0858   0.03182   0.02550   0.0037   0.0020   0.6718
  12.750   1.0965   0.03304   0.02680   0.0046   0.0020   0.6732
  13.000   1.1084   0.03418   0.02801   0.0052   0.0020   0.6746
  13.250   1.1185   0.03551   0.02941   0.0060   0.0019   0.6759
  13.500   1.1294   0.03677   0.03074   0.0066   0.0019   0.6770
  13.750   1.1355   0.03849   0.03258   0.0075   0.0019   0.6784
  14.000   1.1442   0.04000   0.03418   0.0082   0.0019   0.6800
  14.250   1.1535   0.04151   0.03580   0.0087   0.0018   0.6816
  14.500   1.1608   0.04322   0.03761   0.0092   0.0018   0.6832
  14.750   1.1650   0.04528   0.03979   0.0099   0.0018   0.6849
  15.000   1.1691   0.04741   0.04203   0.0104   0.0017   0.6866
  15.250   1.1755   0.04936   0.04408   0.0106   0.0017   0.6886
  15.500   1.1802   0.05155   0.04637   0.0108   0.0017   0.6902
  16.000   1.1815   0.05700   0.05208   0.0111   0.0016   0.6934
  16.250   1.1808   0.06004   0.05525   0.0110   0.0016   0.6951
  16.500   1.1820   0.06296   0.05828   0.0106   0.0015   0.6969
  16.750   1.1775   0.06669   0.06216   0.0101   0.0016   0.6986
  17.000   1.1711   0.07085   0.06648   0.0092   0.0016   0.7003
  17.250   1.1639   0.07534   0.07111   0.0080   0.0016   0.7019
  17.500   1.1613   0.07933   0.07521   0.0066   0.0015   0.7036
  17.750   1.1598   0.08327   0.07927   0.0050   0.0014   0.7052
  18.000   1.1465   0.08927   0.08544   0.0026   0.0014   0.7066
  18.250   1.1377   0.09479   0.09109   0.0001   0.0014   0.7082
  18.500   1.1208   0.10198   0.09846  -0.0034   0.0014   0.7095
  18.750   1.1106   0.10821   0.10482  -0.0068   0.0013   0.7112
  19.000   1.0850   0.11775   0.11455  -0.0120   0.0014   0.7119
  19.250   1.0705   0.12541   0.12234  -0.0164   0.0014   0.7133
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