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EH 3.0/12 (eh3012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: EH 3.0/12 (eh3012-il)
Reynolds number: 1,000,000
Max Cl/Cd: 74.08 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-eh3012-il-1000000-n5.txt
Download as CSV file: xf-eh3012-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EH 3.0/12                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -1.1260   0.04185   0.03879  -0.0443   1.0000   0.0021
 -14.500  -1.1485   0.03788   0.03460  -0.0419   1.0000   0.0021
 -14.250  -1.1630   0.03500   0.03152  -0.0386   1.0000   0.0021
 -14.000  -1.1696   0.03295   0.02931  -0.0350   1.0000   0.0021
 -13.750  -1.1699   0.03123   0.02745  -0.0319   1.0000   0.0021
 -13.500  -1.1641   0.02955   0.02562  -0.0297   1.0000   0.0021
 -13.250  -1.1550   0.02807   0.02400  -0.0277   1.0000   0.0021
 -13.000  -1.1433   0.02673   0.02253  -0.0259   1.0000   0.0021
 -12.750  -1.1296   0.02553   0.02120  -0.0242   1.0000   0.0021
 -12.500  -1.1144   0.02440   0.01996  -0.0227   1.0000   0.0021
 -12.250  -1.0978   0.02338   0.01883  -0.0213   1.0000   0.0021
 -12.000  -1.0801   0.02244   0.01779  -0.0200   1.0000   0.0020
 -11.750  -1.0614   0.02155   0.01681  -0.0188   1.0000   0.0020
 -11.500  -1.0419   0.02074   0.01591  -0.0177   1.0000   0.0020
 -11.250  -1.0218   0.01997   0.01506  -0.0166   1.0000   0.0020
 -11.000  -1.0010   0.01925   0.01426  -0.0156   1.0000   0.0020
 -10.500  -0.9428   0.01794   0.01263  -0.0168   0.8843   0.0020
 -10.250  -0.9234   0.01753   0.01199  -0.0152   0.8352   0.0019
 -10.000  -0.9019   0.01708   0.01136  -0.0141   0.7994   0.0019
  -9.750  -0.8794   0.01666   0.01078  -0.0132   0.7673   0.0019
  -9.500  -0.8563   0.01624   0.01023  -0.0124   0.7492   0.0019
  -9.250  -0.8323   0.01581   0.00970  -0.0117   0.7296   0.0019
  -9.000  -0.8083   0.01542   0.00920  -0.0110   0.7143   0.0019
  -8.750  -0.7838   0.01503   0.00873  -0.0104   0.6986   0.0018
  -8.500  -0.7590   0.01467   0.00828  -0.0099   0.6838   0.0018
  -8.250  -0.7341   0.01432   0.00784  -0.0093   0.6693   0.0018
  -8.000  -0.7087   0.01403   0.00750  -0.0088   0.6555   0.0017
  -7.500  -0.6582   0.01339   0.00666  -0.0079   0.6266   0.0002
  -7.250  -0.6327   0.01308   0.00624  -0.0074   0.6121   0.0002
  -7.000  -0.6070   0.01281   0.00591  -0.0069   0.6006   0.0002
  -6.750  -0.5810   0.01255   0.00559  -0.0065   0.5903   0.0003
  -6.500  -0.5549   0.01229   0.00528  -0.0062   0.5813   0.0003
  -6.000  -0.5025   0.01183   0.00471  -0.0054   0.5642   0.0004
  -5.500  -0.4497   0.01141   0.00419  -0.0047   0.5469   0.0004
  -5.250  -0.4233   0.01122   0.00395  -0.0044   0.5377   0.0004
  -5.000  -0.3967   0.01104   0.00373  -0.0041   0.5289   0.0005
  -4.750  -0.3700   0.01087   0.00351  -0.0038   0.5211   0.0005
  -4.500  -0.3413   0.01109   0.00379  -0.0040   0.5128   0.0008
  -4.250  -0.3168   0.01050   0.00305  -0.0032   0.5052   0.0008
  -4.000  -0.2900   0.01036   0.00288  -0.0029   0.4969   0.0008
  -3.750  -0.2628   0.01026   0.00279  -0.0027   0.4902   0.0009
  -3.500  -0.2360   0.01011   0.00262  -0.0024   0.4834   0.0020
  -2.750  -0.1548   0.00979   0.00222  -0.0017   0.4623   0.0030
  -2.500  -0.1283   0.00959   0.00205  -0.0014   0.4565   0.0100
  -2.250  -0.1011   0.00950   0.00195  -0.0012   0.4493   0.0114
  -2.000  -0.0739   0.00943   0.00185  -0.0010   0.4429   0.0122
  -1.750  -0.0465   0.00935   0.00177  -0.0008   0.4369   0.0135
  -1.500  -0.0193   0.00928   0.00169  -0.0007   0.4307   0.0168
  -1.250   0.0079   0.00919   0.00161  -0.0005   0.4251   0.0229
  -1.000   0.0344   0.00904   0.00153  -0.0002   0.4185   0.0420
  -0.750   0.0616   0.00897   0.00148   0.0000   0.4129   0.0532
  -0.500   0.0891   0.00892   0.00144   0.0001   0.4075   0.0594
  -0.250   0.1167   0.00891   0.00141   0.0002   0.4013   0.0609
   0.000   0.1440   0.00886   0.00138   0.0003   0.3960   0.0707
   0.250   0.1684   0.00848   0.00137   0.0009   0.3911   0.1776
   0.500   0.1760   0.00675   0.00119   0.0042   0.3865   0.6663
   0.750   0.1984   0.00650   0.00121   0.0055   0.3814   0.7562
   1.000   0.2237   0.00652   0.00124   0.0061   0.3627   0.7929
   1.250   0.2497   0.00655   0.00128   0.0065   0.3497   0.8177
   1.500   0.2758   0.00656   0.00132   0.0070   0.3418   0.8438
   1.750   0.3020   0.00662   0.00138   0.0074   0.3284   0.8640
   2.000   0.3273   0.00685   0.00147   0.0079   0.2943   0.8804
   2.250   0.3535   0.00702   0.00156   0.0082   0.2734   0.8934
   2.500   0.3789   0.00729   0.00169   0.0087   0.2423   0.9060
   2.750   0.4050   0.00751   0.00183   0.0090   0.2206   0.9177
   3.000   0.4318   0.00774   0.00197   0.0091   0.2008   0.9273
   3.250   0.4470   0.00928   0.00282   0.0107   0.0206   0.9368
   3.500   0.4759   0.00945   0.00297   0.0104   0.0089   0.9417
   3.750   0.5043   0.00962   0.00311   0.0102   0.0052   0.9473
   4.000   0.5322   0.00977   0.00324   0.0101   0.0056   0.9527
   4.250   0.5631   0.00996   0.00342   0.0093   0.0038   0.9565
   4.500   0.5934   0.01013   0.00356   0.0086   0.0034   0.9606
   4.750   0.6223   0.01031   0.00372   0.0082   0.0033   0.9652
   5.000   0.6529   0.01050   0.00390   0.0074   0.0033   0.9683
   5.250   0.6851   0.01071   0.00408   0.0062   0.0032   0.9706
   5.500   0.7167   0.01098   0.00428   0.0052   0.0026   0.9731
   6.000   0.7771   0.01140   0.00475   0.0036   0.0020   0.9792
   6.250   0.8070   0.01164   0.00501   0.0029   0.0016   0.9815
   6.500   0.8384   0.01189   0.00523   0.0018   0.0020   0.9831
   6.750   0.8692   0.01216   0.00549   0.0008   0.0020   0.9851
   7.000   0.8993   0.01243   0.00576  -0.0001   0.0020   0.9875
   7.250   0.9283   0.01273   0.00608  -0.0007   0.0018   0.9901
   7.500   0.9562   0.01305   0.00640  -0.0012   0.0016   0.9927
   7.750   0.9865   0.01337   0.00673  -0.0022   0.0016   0.9946
   8.000   1.0164   0.01372   0.00711  -0.0031   0.0015   0.9965
   8.250   1.0457   0.01412   0.00754  -0.0040   0.0013   0.9983
   8.500   1.0746   0.01458   0.00804  -0.0049   0.0011   0.9997
   8.750   1.0951   0.01496   0.00844  -0.0040   0.0011   1.0000
   9.000   1.1119   0.01537   0.00889  -0.0023   0.0011   1.0000
   9.250   1.1307   0.01567   0.00917  -0.0010   0.0013   1.0000
   9.500   1.1475   0.01611   0.00964   0.0006   0.0014   1.0000
   9.750   1.1631   0.01661   0.01018   0.0023   0.0013   1.0000
  10.000   1.1757   0.01728   0.01093   0.0044   0.0012   1.0000
  10.250   1.1926   0.01767   0.01132   0.0058   0.0013   1.0000
  10.500   1.2075   0.01815   0.01182   0.0075   0.0014   1.0000
  10.750   1.2193   0.01875   0.01245   0.0096   0.0014   1.0000
  11.000   1.2257   0.01933   0.01307   0.0126   0.0015   1.0000
  11.250   1.2291   0.02016   0.01397   0.0156   0.0015   1.0000
  11.500   1.2356   0.02109   0.01495   0.0176   0.0015   1.0000
  11.750   1.2409   0.02233   0.01626   0.0190   0.0015   1.0000
  12.000   1.2496   0.02355   0.01753   0.0198   0.0016   1.0000
  12.250   1.2543   0.02533   0.01938   0.0202   0.0017   1.0000
  12.500   1.2625   0.02694   0.02104   0.0203   0.0017   1.0000
  12.750   1.2633   0.02943   0.02364   0.0202   0.0017   1.0000
  13.000   1.2688   0.03154   0.02580   0.0198   0.0017   1.0000
  13.250   1.2666   0.03454   0.02890   0.0193   0.0018   1.0000
  13.500   1.2717   0.03678   0.03121   0.0189   0.0017   1.0000
  13.750   1.2690   0.03991   0.03443   0.0183   0.0017   1.0000
  14.000   1.2597   0.04385   0.03847   0.0175   0.0019   1.0000
  14.250   1.2641   0.04619   0.04087   0.0170   0.0017   1.0000
  14.500   1.2571   0.04991   0.04467   0.0161   0.0018   1.0000
  14.750   1.2398   0.05490   0.04978   0.0149   0.0019   1.0000
  15.000   1.2385   0.05809   0.05304   0.0141   0.0018   1.0000
  15.250   1.2248   0.06297   0.05803   0.0127   0.0020   1.0000
  15.500   1.2303   0.06540   0.06049   0.0120   0.0018   1.0000
  15.750   1.2124   0.07106   0.06628   0.0102   0.0019   1.0000
  16.000   1.2117   0.07440   0.06967   0.0092   0.0019   1.0000
  16.250   1.2019   0.07908   0.07443   0.0077   0.0019   1.0000
  16.500   1.2009   0.08257   0.07798   0.0065   0.0018   1.0000
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