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E209 (13.72%) (e209-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E209 (13.72%) (e209-il)
Reynolds number: 1,000,000
Max Cl/Cd: 103.66 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e209-il-1000000-n5.txt
Download as CSV file: xf-e209-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E209  (13.72%)                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.8478   0.11135   0.10890  -0.0284   1.0000   0.0039
 -17.250  -0.8802   0.10124   0.09868  -0.0335   1.0000   0.0039
 -17.000  -0.9185   0.09026   0.08754  -0.0393   1.0000   0.0038
 -16.750  -0.9454   0.08160   0.07875  -0.0439   1.0000   0.0037
 -16.500  -0.9749   0.07270   0.06970  -0.0488   1.0000   0.0038
 -16.250  -1.0052   0.06421   0.06106  -0.0537   1.0000   0.0038
 -16.000  -1.0083   0.06035   0.05710  -0.0556   1.0000   0.0036
 -15.750  -1.0339   0.05335   0.04995  -0.0595   1.0000   0.0037
 -15.500  -1.0431   0.04892   0.04541  -0.0618   1.0000   0.0037
 -15.250  -1.0605   0.04356   0.03991  -0.0646   1.0000   0.0038
 -15.000  -1.0689   0.03954   0.03576  -0.0665   1.0000   0.0038
 -14.750  -1.0722   0.03631   0.03243  -0.0678   1.0000   0.0038
 -14.500  -1.0752   0.03331   0.02931  -0.0688   1.0000   0.0038
 -14.250  -1.0779   0.03060   0.02649  -0.0692   1.0000   0.0039
 -14.000  -1.0777   0.02850   0.02429  -0.0691   1.0000   0.0040
 -13.750  -1.0788   0.02661   0.02230  -0.0681   1.0000   0.0040
 -13.500  -1.0791   0.02514   0.02074  -0.0663   1.0000   0.0041
 -13.250  -1.0781   0.02408   0.01961  -0.0638   1.0000   0.0042
 -13.000  -1.0809   0.02321   0.01868  -0.0599   1.0000   0.0043
 -12.750  -1.0820   0.02245   0.01785  -0.0558   1.0000   0.0043
 -12.500  -1.0753   0.02170   0.01703  -0.0530   1.0000   0.0044
 -12.250  -1.0678   0.02094   0.01621  -0.0502   1.0000   0.0045
 -12.000  -1.0425   0.02015   0.01534  -0.0508   0.9985   0.0047
 -11.750  -1.0162   0.01931   0.01442  -0.0517   0.9964   0.0048
 -11.500  -0.9884   0.01861   0.01366  -0.0526   0.9944   0.0051
 -11.250  -0.9631   0.01786   0.01283  -0.0530   0.9918   0.0052
 -11.000  -0.9365   0.01721   0.01211  -0.0535   0.9890   0.0053
 -10.750  -0.9079   0.01661   0.01146  -0.0544   0.9864   0.0055
 -10.500  -0.8781   0.01592   0.01069  -0.0555   0.9842   0.0057
 -10.250  -0.8500   0.01529   0.01001  -0.0562   0.9813   0.0061
 -10.000  -0.8242   0.01477   0.00946  -0.0563   0.9762   0.0064
  -9.750  -0.7944   0.01430   0.00897  -0.0572   0.9718   0.0070
  -9.500  -0.7675   0.01386   0.00849  -0.0574   0.9653   0.0075
  -9.000  -0.7088   0.01296   0.00749  -0.0587   0.9433   0.0085
  -8.750  -0.6782   0.01254   0.00702  -0.0595   0.9196   0.0094
  -8.500  -0.6522   0.01228   0.00661  -0.0593   0.8842   0.0102
  -8.250  -0.6290   0.01209   0.00627  -0.0584   0.8507   0.0108
  -8.000  -0.6060   0.01189   0.00592  -0.0575   0.8221   0.0114
  -7.750  -0.5827   0.01164   0.00557  -0.0568   0.7963   0.0124
  -7.500  -0.5587   0.01145   0.00527  -0.0561   0.7732   0.0133
  -7.250  -0.5339   0.01128   0.00500  -0.0556   0.7532   0.0143
  -7.000  -0.5088   0.01112   0.00475  -0.0552   0.7351   0.0151
  -6.750  -0.4841   0.01088   0.00442  -0.0546   0.7180   0.0165
  -6.500  -0.4588   0.01068   0.00415  -0.0542   0.7029   0.0178
  -6.250  -0.4329   0.01050   0.00390  -0.0539   0.6889   0.0189
  -6.000  -0.4070   0.01032   0.00366  -0.0536   0.6754   0.0209
  -5.750  -0.3812   0.01011   0.00342  -0.0533   0.6633   0.0245
  -5.500  -0.3554   0.00989   0.00318  -0.0530   0.6523   0.0313
  -5.250  -0.3295   0.00967   0.00296  -0.0527   0.6418   0.0427
  -5.000  -0.3034   0.00945   0.00276  -0.0524   0.6316   0.0555
  -4.750  -0.2771   0.00924   0.00257  -0.0522   0.6232   0.0687
  -4.500  -0.2507   0.00906   0.00240  -0.0520   0.6142   0.0832
  -4.250  -0.2240   0.00887   0.00224  -0.0519   0.6063   0.1008
  -3.750  -0.1710   0.00845   0.00193  -0.0515   0.5914   0.1496
  -3.500  -0.1448   0.00820   0.00179  -0.0513   0.5840   0.1852
  -3.250  -0.1182   0.00797   0.00166  -0.0512   0.5776   0.2207
  -3.000  -0.0916   0.00777   0.00154  -0.0510   0.5710   0.2545
  -2.750  -0.0654   0.00749   0.00142  -0.0509   0.5650   0.3057
  -2.500  -0.0388   0.00727   0.00133  -0.0507   0.5586   0.3518
  -2.250  -0.0118   0.00715   0.00128  -0.0506   0.5528   0.3862
  -2.000   0.0160   0.00706   0.00125  -0.0506   0.5473   0.4140
  -1.750   0.0438   0.00703   0.00122  -0.0506   0.5410   0.4291
  -1.500   0.0720   0.00702   0.00120  -0.0506   0.5358   0.4403
  -1.250   0.1001   0.00699   0.00118  -0.0506   0.5304   0.4512
  -1.000   0.1280   0.00699   0.00117  -0.0506   0.5246   0.4613
  -0.500   0.1843   0.00698   0.00116  -0.0507   0.5141   0.4808
  -0.250   0.2123   0.00699   0.00116  -0.0507   0.5088   0.4890
   0.000   0.2405   0.00699   0.00117  -0.0508   0.5037   0.4982
   0.250   0.2686   0.00699   0.00118  -0.0508   0.4982   0.5072
   0.750   0.3246   0.00701   0.00121  -0.0508   0.4880   0.5261
   1.000   0.3526   0.00702   0.00124  -0.0508   0.4825   0.5352
   1.250   0.3805   0.00705   0.00127  -0.0508   0.4777   0.5446
   1.500   0.4086   0.00706   0.00130  -0.0509   0.4725   0.5532
   2.000   0.4643   0.00712   0.00139  -0.0509   0.4615   0.5711
   2.250   0.4922   0.00714   0.00144  -0.0509   0.4553   0.5810
   2.750   0.5473   0.00723   0.00156  -0.0508   0.4399   0.6037
   3.000   0.5746   0.00728   0.00163  -0.0507   0.4316   0.6157
   3.250   0.6019   0.00733   0.00171  -0.0506   0.4229   0.6293
   3.500   0.6291   0.00738   0.00179  -0.0505   0.4147   0.6452
   4.000   0.6829   0.00750   0.00198  -0.0502   0.3957   0.6806
   4.250   0.7095   0.00757   0.00209  -0.0500   0.3850   0.6999
   4.500   0.7357   0.00765   0.00221  -0.0498   0.3738   0.7226
   4.750   0.7615   0.00774   0.00235  -0.0494   0.3613   0.7484
   5.250   0.8114   0.00794   0.00265  -0.0484   0.3306   0.8094
   5.500   0.8349   0.00809   0.00284  -0.0476   0.3101   0.8454
   5.750   0.8562   0.00828   0.00307  -0.0463   0.2858   0.8904
   6.000   0.8801   0.00849   0.00332  -0.0455   0.2636   0.9451
   6.250   0.9130   0.00895   0.00364  -0.0470   0.2303   0.9760
   6.500   0.9442   0.00949   0.00401  -0.0482   0.1942   0.9917
   6.750   0.9689   0.01007   0.00441  -0.0481   0.1609   1.0000
   7.000   0.9878   0.01059   0.00478  -0.0466   0.1320   1.0000
   7.250   1.0089   0.01098   0.00510  -0.0456   0.1153   1.0000
   7.500   1.0301   0.01137   0.00542  -0.0445   0.1008   1.0000
   7.750   1.0505   0.01179   0.00578  -0.0434   0.0862   1.0000
   8.000   1.0707   0.01223   0.00615  -0.0422   0.0728   1.0000
   8.250   1.0897   0.01273   0.00657  -0.0409   0.0590   1.0000
   8.500   1.1104   0.01310   0.00692  -0.0398   0.0517   1.0000
   8.750   1.1290   0.01359   0.00736  -0.0384   0.0420   1.0000
   9.000   1.1472   0.01407   0.00781  -0.0369   0.0340   1.0000
   9.250   1.1654   0.01453   0.00824  -0.0355   0.0290   1.0000
   9.500   1.1832   0.01498   0.00869  -0.0340   0.0248   1.0000
   9.750   1.1988   0.01545   0.00915  -0.0321   0.0209   1.0000
  10.000   1.2125   0.01591   0.00962  -0.0299   0.0185   1.0000
  10.250   1.2257   0.01640   0.01012  -0.0276   0.0163   1.0000
  10.500   1.2392   0.01690   0.01065  -0.0255   0.0148   1.0000
  10.750   1.2510   0.01750   0.01126  -0.0232   0.0130   1.0000
  11.000   1.2640   0.01806   0.01186  -0.0212   0.0119   1.0000
  11.250   1.2761   0.01869   0.01252  -0.0192   0.0110   1.0000
  11.500   1.2862   0.01945   0.01330  -0.0171   0.0098   1.0000
  11.750   1.2973   0.02020   0.01409  -0.0152   0.0089   1.0000
  12.000   1.3069   0.02106   0.01500  -0.0134   0.0079   1.0000
  12.250   1.3151   0.02207   0.01604  -0.0115   0.0070   1.0000
  12.500   1.3238   0.02312   0.01715  -0.0099   0.0063   1.0000
  12.750   1.3317   0.02430   0.01837  -0.0085   0.0057   1.0000
  13.000   1.3380   0.02567   0.01979  -0.0071   0.0051   1.0000
  13.250   1.3444   0.02712   0.02130  -0.0059   0.0048   1.0000
  13.500   1.3517   0.02858   0.02282  -0.0050   0.0046   1.0000
  13.750   1.3580   0.03019   0.02450  -0.0042   0.0043   1.0000
  14.000   1.3633   0.03198   0.02635  -0.0035   0.0041   1.0000
  14.250   1.3675   0.03392   0.02835  -0.0029   0.0039   1.0000
  14.500   1.3707   0.03603   0.03053  -0.0024   0.0037   1.0000
  14.750   1.3749   0.03810   0.03267  -0.0021   0.0037   1.0000
  15.000   1.3753   0.04060   0.03526  -0.0019   0.0035   1.0000
  15.250   1.3757   0.04318   0.03792  -0.0018   0.0033   1.0000
  15.500   1.3753   0.04590   0.04072  -0.0018   0.0032   1.0000
  15.750   1.3764   0.04854   0.04343  -0.0020   0.0031   1.0000
  16.000   1.3762   0.05140   0.04639  -0.0022   0.0030   1.0000
  16.250   1.3753   0.05441   0.04949  -0.0027   0.0030   1.0000
  16.500   1.3733   0.05765   0.05281  -0.0032   0.0030   1.0000
  16.750   1.3727   0.06080   0.05605  -0.0039   0.0030   1.0000
  17.000   1.3697   0.06436   0.05970  -0.0048   0.0029   1.0000
  17.250   1.3672   0.06792   0.06334  -0.0058   0.0028   1.0000
  17.500   1.3637   0.07172   0.06724  -0.0069   0.0027   1.0000
  17.750   1.3589   0.07581   0.07142  -0.0083   0.0027   1.0000
  18.000   1.3539   0.08002   0.07573  -0.0098   0.0026   1.0000
  18.250   1.3459   0.08480   0.08061  -0.0116   0.0027   1.0000
  18.500   1.3405   0.08926   0.08517  -0.0134   0.0026   1.0000
  18.750   1.3338   0.09405   0.09006  -0.0154   0.0025   1.0000
  19.000   1.3247   0.09933   0.09545  -0.0177   0.0026   1.0000
  19.250   1.3139   0.10502   0.10126  -0.0204   0.0025   1.0000
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