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NREL's S810 Airfoil (s810-nr) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NREL's S810 Airfoil (s810-nr)
Reynolds number: 1,000,000
Max Cl/Cd: 105.36 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s810-nr-1000000.txt
Download as CSV file: xf-s810-nr-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.4875   0.07625   0.07319  -0.0796   0.7331   0.0074
 -11.500  -0.5027   0.07258   0.06943  -0.0796   0.7319   0.0074
 -11.000  -0.5312   0.06621   0.06287  -0.0781   0.7295   0.0075
 -10.750  -0.5451   0.06328   0.05985  -0.0766   0.7286   0.0075
 -10.500  -0.5582   0.06064   0.05711  -0.0747   0.7276   0.0075
 -10.250  -0.5696   0.05828   0.05467  -0.0726   0.7265   0.0075
 -10.000  -0.5827   0.05586   0.05212  -0.0693   0.7254   0.0076
  -9.750  -0.5940   0.05382   0.04999  -0.0656   0.7242   0.0076
  -9.500  -0.6005   0.05173   0.04777  -0.0623   0.7231   0.0076
  -9.250  -0.6030   0.04923   0.04512  -0.0594   0.7221   0.0076
  -9.000  -0.6025   0.04663   0.04235  -0.0567   0.7211   0.0076
  -8.750  -0.5980   0.04426   0.03983  -0.0545   0.7202   0.0076
  -8.500  -0.5928   0.04155   0.03691  -0.0519   0.7193   0.0076
  -8.250  -0.5853   0.02256   0.01784  -0.0458   0.7167   0.0082
  -8.000  -0.5738   0.02096   0.01616  -0.0448   0.7157   0.0085
  -7.750  -0.5595   0.01937   0.01447  -0.0438   0.7151   0.0088
  -7.500  -0.5429   0.01770   0.01268  -0.0429   0.7144   0.0092
  -7.250  -0.5242   0.01627   0.01113  -0.0422   0.7138   0.0100
  -7.000  -0.4986   0.01585   0.01060  -0.0415   0.7131   0.0116
  -6.750  -0.4768   0.01556   0.01018  -0.0406   0.7123   0.0121
  -6.500  -0.4563   0.01420   0.00866  -0.0398   0.7116   0.0121
  -6.250  -0.4350   0.01289   0.00718  -0.0392   0.7109   0.0122
  -6.000  -0.3976   0.00869   0.00281  -0.0411   0.7104   0.0135
  -5.750  -0.3674   0.00766   0.00177  -0.0419   0.7098   0.0140
  -5.500  -0.2782   0.01705   0.01082  -0.0518   0.7107   0.0097
  -5.250  -0.2614   0.01641   0.01017  -0.0502   0.7100   0.0103
  -5.000  -0.2491   0.01569   0.00941  -0.0483   0.7092   0.0105
  -4.750  -0.2405   0.01484   0.00854  -0.0460   0.7084   0.0107
  -4.500  -0.2317   0.01414   0.00781  -0.0437   0.7075   0.0113
  -4.250  -0.2277   0.01355   0.00717  -0.0406   0.7067   0.0115
  -4.000  -0.2128   0.01307   0.00665  -0.0391   0.7060   0.0118
  -3.750  -0.1929   0.01274   0.00628  -0.0383   0.7053   0.0122
  -3.500  -0.1821   0.01189   0.00533  -0.0362   0.7044   0.0131
  -3.250  -0.1616   0.01144   0.00481  -0.0355   0.7035   0.0141
  -3.000  -0.1378   0.01116   0.00450  -0.0353   0.7028   0.0162
  -2.750  -0.1124   0.01099   0.00430  -0.0354   0.7020   0.0186
  -2.500  -0.0877   0.01070   0.00398  -0.0353   0.7014   0.0274
  -2.250  -0.0688   0.00982   0.00354  -0.0347   0.7010   0.1894
  -2.000  -0.0612   0.00739   0.00256  -0.0333   0.7004   0.5909
  -1.750  -0.0317   0.00754   0.00270  -0.0339   0.6999   0.6098
  -1.500  -0.0020   0.00774   0.00289  -0.0345   0.6994   0.6202
  -1.250   0.0273   0.00782   0.00299  -0.0351   0.6987   0.6258
  -1.000   0.0568   0.00788   0.00305  -0.0358   0.6979   0.6283
  -0.750   0.0864   0.00794   0.00310  -0.0365   0.6973   0.6306
  -0.500   0.1160   0.00801   0.00315  -0.0372   0.6967   0.6329
  -0.250   0.1454   0.00809   0.00322  -0.0379   0.6961   0.6366
   0.000   0.1747   0.00813   0.00329  -0.0385   0.6953   0.6391
   0.250   0.2042   0.00814   0.00331  -0.0393   0.6945   0.6401
   0.500   0.2337   0.00816   0.00333  -0.0400   0.6937   0.6410
   0.750   0.2632   0.00818   0.00336  -0.0407   0.6929   0.6420
   1.000   0.2927   0.00820   0.00338  -0.0414   0.6921   0.6430
   1.250   0.3222   0.00823   0.00341  -0.0422   0.6912   0.6441
   1.500   0.3518   0.00825   0.00344  -0.0429   0.6901   0.6451
   1.750   0.3814   0.00831   0.00349  -0.0436   0.6888   0.6463
   2.000   0.4105   0.00839   0.00358  -0.0443   0.6870   0.6473
   2.250   0.4396   0.00832   0.00355  -0.0449   0.6848   0.6482
   2.500   0.4687   0.00824   0.00349  -0.0455   0.6816   0.6490
   2.750   0.4981   0.00807   0.00332  -0.0461   0.6777   0.6501
   3.000   0.5276   0.00802   0.00325  -0.0467   0.6735   0.6513
   3.250   0.5559   0.00787   0.00319  -0.0471   0.6697   0.6523
   3.500   0.5848   0.00776   0.00312  -0.0476   0.6655   0.6533
   3.750   0.6140   0.00766   0.00302  -0.0481   0.6607   0.6543
   4.000   0.6421   0.00755   0.00298  -0.0485   0.6543   0.6555
   4.250   0.6706   0.00744   0.00291  -0.0489   0.6476   0.6567
   4.500   0.6988   0.00738   0.00292  -0.0493   0.6402   0.6579
   4.750   0.7270   0.00734   0.00289  -0.0497   0.6319   0.6590
   5.000   0.7548   0.00729   0.00289  -0.0500   0.6167   0.6601
   5.250   0.7786   0.00739   0.00289  -0.0495   0.5684   0.6611
   5.500   0.7857   0.00840   0.00339  -0.0461   0.4628   0.6621
   5.750   0.7874   0.00962   0.00409  -0.0420   0.3546   0.6629
   6.000   0.7916   0.01054   0.00464  -0.0383   0.2761   0.6642
   6.250   0.7969   0.01127   0.00512  -0.0347   0.2188   0.6656
   6.500   0.7987   0.01187   0.00555  -0.0304   0.1776   0.6670
   6.750   0.8036   0.01250   0.00606  -0.0268   0.1463   0.6682
   7.000   0.8086   0.01326   0.00667  -0.0235   0.1145   0.6694
   7.250   0.8159   0.01402   0.00731  -0.0208   0.0884   0.6707
   7.500   0.8250   0.01477   0.00798  -0.0185   0.0672   0.6719
   7.750   0.8363   0.01548   0.00862  -0.0167   0.0521   0.6732
   8.000   0.8485   0.01620   0.00929  -0.0151   0.0397   0.6744
   8.250   0.8636   0.01680   0.00988  -0.0139   0.0347   0.6755
   8.500   0.8791   0.01742   0.01051  -0.0128   0.0296   0.6766
   8.750   0.8944   0.01806   0.01113  -0.0117   0.0257   0.6777
   9.000   0.9095   0.01869   0.01178  -0.0107   0.0208   0.6796
   9.500   0.9320   0.02049   0.01352  -0.0077   0.0071   0.6823
   9.750   0.9461   0.02127   0.01436  -0.0066   0.0062   0.6837
  10.000   0.9607   0.02203   0.01518  -0.0056   0.0059   0.6851
  10.250   0.9729   0.02297   0.01618  -0.0044   0.0052   0.6864
  10.500   0.9878   0.02374   0.01700  -0.0035   0.0050   0.6878
  10.750   1.0001   0.02470   0.01802  -0.0024   0.0046   0.6892
  11.000   1.0105   0.02582   0.01921  -0.0010   0.0044   0.6904
  11.250   1.0205   0.02700   0.02047   0.0003   0.0042   0.6915
  11.500   1.0314   0.02808   0.02165   0.0014   0.0041   0.6934
  11.750   1.0355   0.02971   0.02343   0.0031   0.0040   0.6951
  12.000   1.0404   0.03135   0.02520   0.0047   0.0039   0.6967
  12.250   1.0489   0.03274   0.02668   0.0058   0.0038   0.6983
  12.500   1.0598   0.03398   0.02800   0.0066   0.0038   0.7000
  12.750   1.0679   0.03548   0.02960   0.0076   0.0038   0.7016
  13.000   1.0794   0.03671   0.03091   0.0082   0.0037   0.7032
  13.250   1.0863   0.03838   0.03268   0.0091   0.0037   0.7047
  13.500   1.0957   0.03986   0.03425   0.0098   0.0035   0.7062
  13.750   1.0985   0.04201   0.03656   0.0108   0.0036   0.7081
  14.000   1.1047   0.04387   0.03854   0.0115   0.0035   0.7100
  14.250   1.1110   0.04577   0.04055   0.0121   0.0033   0.7118
  14.500   1.1146   0.04800   0.04292   0.0126   0.0033   0.7137
  14.750   1.1150   0.05066   0.04574   0.0132   0.0033   0.7155
  15.000   1.1150   0.05343   0.04867   0.0137   0.0032   0.7173
  15.250   1.1158   0.05620   0.05155   0.0138   0.0031   0.7190
  15.500   1.1143   0.05930   0.05481   0.0138   0.0031   0.7210
  15.750   1.1078   0.06318   0.05888   0.0137   0.0031   0.7230
  16.000   1.1011   0.06722   0.06310   0.0132   0.0031   0.7251
  16.250   1.0924   0.07176   0.06781   0.0124   0.0031   0.7271
  16.500   1.0816   0.07684   0.07307   0.0110   0.0030   0.7290
  16.750   1.0703   0.08223   0.07863   0.0092   0.0031   0.7308
  17.000   1.0542   0.08872   0.08531   0.0068   0.0031   0.7324
  17.250   1.0370   0.09582   0.09259   0.0036   0.0031   0.7337
  17.500   1.0208   0.10312   0.10006  -0.0002   0.0031   0.7353
  17.750   1.0057   0.11058   0.10768  -0.0043   0.0030   0.7370
  18.000   0.9833   0.12005   0.11733  -0.0097   0.0031   0.7381
  18.250   0.9626   0.12967   0.12711  -0.0154   0.0031   0.7393
  18.500   0.9405   0.14007   0.13766  -0.0217   0.0032   0.7402
  18.750   0.9096   0.15359   0.15134  -0.0295   0.0032   0.7404
  19.000   0.8676   0.17131   0.16919  -0.0390   0.0034   0.7394
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