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NREL's S830 Airfoil (s830-nr) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NREL's S830 Airfoil (s830-nr)
Reynolds number: 1,000,000
Max Cl/Cd: 115.28 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s830-nr-1000000-n5.txt
Download as CSV file: xf-s830-nr-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NREL's S830 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
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.3612   0.05144   0.04878  -0.1589   0.9697   0.0035
 -13.750  -0.3786   0.04679   0.04390  -0.1591   0.9667   0.0035
 -13.500  -0.3853   0.04259   0.03945  -0.1605   0.9648   0.0035
 -13.250  -0.3804   0.03936   0.03599  -0.1624   0.9633   0.0035
 -13.000  -0.3734   0.03626   0.03262  -0.1640   0.9619   0.0035
 -12.750  -0.3587   0.03411   0.03027  -0.1656   0.9606   0.0035
 -12.500  -0.3535   0.03269   0.02871  -0.1640   0.9565   0.0035
 -12.250  -0.3415   0.03183   0.02781  -0.1633   0.9515   0.0036
 -12.000  -0.3230   0.03049   0.02632  -0.1640   0.9483   0.0036
 -11.750  -0.3056   0.02953   0.02526  -0.1640   0.9440   0.0036
 -11.500  -0.2939   0.02881   0.02448  -0.1626   0.9363   0.0036
 -11.250  -0.2733   0.02795   0.02351  -0.1629   0.9288   0.0037
 -11.000  -0.2480   0.02715   0.02258  -0.1639   0.9180   0.0037
 -10.750  -0.2178   0.02642   0.02175  -0.1662   0.9042   0.0037
 -10.500  -0.1887   0.02580   0.02093  -0.1678   0.8808   0.0038
 -10.250  -0.1703   0.02536   0.02033  -0.1672   0.8615   0.0038
 -10.000  -0.1548   0.02500   0.01984  -0.1662   0.8423   0.0039
  -9.750  -0.1418   0.02464   0.01936  -0.1646   0.8260   0.0039
  -9.500  -0.1321   0.02422   0.01883  -0.1624   0.8116   0.0040
  -9.250  -0.1204   0.02381   0.01833  -0.1608   0.7997   0.0040
  -9.000  -0.1102   0.02335   0.01779  -0.1589   0.7878   0.0041
  -8.750  -0.0986   0.02292   0.01730  -0.1573   0.7762   0.0041
  -8.500  -0.0890   0.02243   0.01675  -0.1555   0.7664   0.0042
  -8.250  -0.0800   0.02192   0.01617  -0.1535   0.7562   0.0042
  -8.000  -0.0708   0.02140   0.01561  -0.1517   0.7477   0.0042
  -7.500  -0.0578   0.02030   0.01441  -0.1471   0.7300   0.0044
  -7.250  -0.0531   0.01977   0.01382  -0.1444   0.7217   0.0044
  -7.000  -0.0518   0.01914   0.01316  -0.1412   0.7134   0.0045
  -6.750  -0.0615   0.01852   0.01249  -0.1360   0.7055   0.0046
  -6.500  -0.0583   0.01783   0.01178  -0.1333   0.6987   0.0046
  -6.000  -0.0408   0.01630   0.01016  -0.1305   0.6853   0.0049
  -5.750  -0.0251   0.01551   0.00932  -0.1303   0.6788   0.0050
  -5.500  -0.0051   0.01471   0.00846  -0.1310   0.6730   0.0053
  -5.250   0.0196   0.01388   0.00758  -0.1326   0.6667   0.0059
  -5.000   0.0461   0.01306   0.00670  -0.1346   0.6604   0.0073
  -4.750   0.0779   0.01223   0.00584  -0.1376   0.6545   0.0116
  -4.500   0.1079   0.01169   0.00526  -0.1396   0.6480   0.0158
  -4.250   0.1364   0.01132   0.00485  -0.1409   0.6424   0.0213
  -4.000   0.1663   0.01097   0.00451  -0.1423   0.6370   0.0293
  -3.750   0.1953   0.01067   0.00421  -0.1436   0.6314   0.0425
  -3.500   0.2250   0.01035   0.00391  -0.1449   0.6264   0.0637
  -3.250   0.2866   0.00773   0.00233  -0.1568   0.6211   0.4454
  -3.000   0.3142   0.00771   0.00230  -0.1571   0.6157   0.4619
  -2.750   0.3411   0.00773   0.00230  -0.1573   0.6109   0.4732
  -2.500   0.3687   0.00775   0.00230  -0.1575   0.6059   0.4799
  -2.250   0.3950   0.00780   0.00231  -0.1575   0.6004   0.4842
  -2.000   0.4210   0.00786   0.00231  -0.1574   0.5953   0.4874
  -1.750   0.4482   0.00790   0.00231  -0.1576   0.5904   0.4900
  -1.500   0.4747   0.00795   0.00233  -0.1577   0.5853   0.4929
  -1.250   0.5006   0.00801   0.00235  -0.1576   0.5808   0.4940
  -1.000   0.5281   0.00804   0.00236  -0.1578   0.5768   0.4950
  -0.750   0.5550   0.00809   0.00238  -0.1580   0.5723   0.4961
  -0.500   0.5811   0.00816   0.00241  -0.1579   0.5679   0.4972
  -0.250   0.6074   0.00823   0.00245  -0.1580   0.5639   0.4983
   0.000   0.6345   0.00828   0.00249  -0.1582   0.5601   0.4994
   0.250   0.6612   0.00835   0.00253  -0.1582   0.5559   0.5005
   0.500   0.6871   0.00844   0.00259  -0.1582   0.5517   0.5017
   0.750   0.7134   0.00853   0.00265  -0.1582   0.5480   0.5028
   1.000   0.7403   0.00860   0.00271  -0.1584   0.5441   0.5038
   1.250   0.7667   0.00868   0.00279  -0.1585   0.5400   0.5050
   1.500   0.7926   0.00877   0.00287  -0.1584   0.5363   0.5065
   1.750   0.8185   0.00887   0.00297  -0.1584   0.5330   0.5077
   2.000   0.8452   0.00894   0.00305  -0.1586   0.5300   0.5090
   2.250   0.8715   0.00903   0.00315  -0.1586   0.5267   0.5103
   2.500   0.8972   0.00913   0.00325  -0.1585   0.5234   0.5116
   2.750   0.9223   0.00925   0.00337  -0.1584   0.5202   0.5130
   3.000   0.9479   0.00936   0.00348  -0.1583   0.5173   0.5143
   3.250   0.9742   0.00945   0.00359  -0.1584   0.5144   0.5156
   3.500   1.0001   0.00955   0.00370  -0.1584   0.5112   0.5168
   3.750   1.0254   0.00967   0.00383  -0.1583   0.5081   0.5178
   4.000   1.0501   0.00980   0.00397  -0.1581   0.5052   0.5188
   4.250   1.0746   0.00994   0.00412  -0.1578   0.5025   0.5201
   4.500   1.1005   0.01003   0.00426  -0.1578   0.5004   0.5216
   4.750   1.1260   0.01014   0.00441  -0.1578   0.4980   0.5230
   5.000   1.1510   0.01026   0.00457  -0.1577   0.4954   0.5243
   5.250   1.1755   0.01040   0.00475  -0.1574   0.4926   0.5257
   5.500   1.1993   0.01057   0.00493  -0.1571   0.4898   0.5272
   5.750   1.2228   0.01075   0.00513  -0.1566   0.4872   0.5287
   6.000   1.2482   0.01087   0.00530  -0.1566   0.4851   0.5303
   6.250   1.2715   0.01103   0.00550  -0.1562   0.4787   0.5316
   6.500   1.2902   0.01133   0.00576  -0.1549   0.4674   0.5328
   6.750   1.3078   0.01167   0.00606  -0.1534   0.4536   0.5338
   7.000   1.3263   0.01201   0.00638  -0.1521   0.4413   0.5351
   7.250   1.3479   0.01225   0.00665  -0.1515   0.4321   0.5365
   7.500   1.3644   0.01266   0.00704  -0.1499   0.4169   0.5379
   7.750   1.3807   0.01311   0.00746  -0.1483   0.4012   0.5391
   8.000   1.3932   0.01373   0.00800  -0.1461   0.3789   0.5405
   8.250   1.3930   0.01491   0.00897  -0.1420   0.3353   0.5416
   8.500   1.3861   0.01649   0.01029  -0.1369   0.2879   0.5427
   8.750   1.3851   0.01789   0.01152  -0.1330   0.2527   0.5438
   9.000   1.3841   0.01935   0.01283  -0.1293   0.2206   0.5450
   9.250   1.3848   0.02081   0.01417  -0.1261   0.1937   0.5460
   9.500   1.3847   0.02239   0.01564  -0.1229   0.1681   0.5470
   9.750   1.3824   0.02421   0.01733  -0.1196   0.1415   0.5480
  10.000   1.3784   0.02624   0.01924  -0.1164   0.1150   0.5488
  10.250   1.3808   0.02797   0.02091  -0.1141   0.0980   0.5498
  10.500   1.3816   0.02989   0.02278  -0.1119   0.0811   0.5512
  10.750   1.3833   0.03184   0.02469  -0.1099   0.0674   0.5525
  11.000   1.3865   0.03374   0.02657  -0.1081   0.0566   0.5536
  11.250   1.3906   0.03565   0.02847  -0.1066   0.0476   0.5548
  11.500   1.3932   0.03775   0.03056  -0.1051   0.0387   0.5559
  11.750   1.3951   0.03999   0.03279  -0.1036   0.0305   0.5570
  12.000   1.4023   0.04181   0.03464  -0.1026   0.0272   0.5582
  12.250   1.4093   0.04368   0.03655  -0.1017   0.0245   0.5594
  12.500   1.4154   0.04570   0.03859  -0.1009   0.0215   0.5605
  12.750   1.4201   0.04790   0.04082  -0.1000   0.0183   0.5615
  13.000   1.4266   0.04995   0.04290  -0.0993   0.0159   0.5626
  13.250   1.4319   0.05217   0.04515  -0.0986   0.0139   0.5637
  13.500   1.4368   0.05446   0.04749  -0.0980   0.0117   0.5646
  13.750   1.4433   0.05664   0.04971  -0.0975   0.0104   0.5657
  14.000   1.4483   0.05902   0.05214  -0.0970   0.0089   0.5671
  14.250   1.4543   0.06133   0.05451  -0.0967   0.0079   0.5684
  14.500   1.4599   0.06371   0.05695  -0.0964   0.0069   0.5696
  14.750   1.4647   0.06622   0.05951  -0.0961   0.0061   0.5707
  15.000   1.4706   0.06861   0.06196  -0.0959   0.0054   0.5719
  15.250   1.4756   0.07117   0.06458  -0.0958   0.0049   0.5731
  15.500   1.4807   0.07373   0.06720  -0.0957   0.0044   0.5744
  15.750   1.4859   0.07632   0.06986  -0.0957   0.0041   0.5757
  16.000   1.4911   0.07890   0.07250  -0.0957   0.0036   0.5770
  16.250   1.4944   0.08176   0.07542  -0.0958   0.0032   0.5782
  16.500   1.4993   0.08442   0.07814  -0.0959   0.0029   0.5793
  16.750   1.5034   0.08723   0.08102  -0.0961   0.0026   0.5802
  17.000   1.5078   0.09001   0.08386  -0.0963   0.0022   0.5811
  17.250   1.5106   0.09306   0.08698  -0.0967   0.0020   0.5824
  17.500   1.5151   0.09588   0.08987  -0.0971   0.0017   0.5837
  17.750   1.5180   0.09892   0.09300  -0.0975   0.0015   0.5850
  18.000   1.5213   0.10191   0.09606  -0.0980   0.0013   0.5863
  18.250   1.5229   0.10516   0.09939  -0.0986   0.0011   0.5878
  18.500   1.5259   0.10823   0.10253  -0.0993   0.0009   0.5893
  18.750   1.5282   0.11143   0.10581  -0.1000   0.0008   0.5907
  19.000   1.5302   0.11463   0.10909  -0.1008   0.0007   0.5920
  19.250   1.5316   0.11795   0.11248  -0.1017   0.0006   0.5933
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