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FAUVEL 14% AIRFOIL (fauvel-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FAUVEL 14% AIRFOIL (fauvel-il)
Reynolds number: 1,000,000
Max Cl/Cd: 106.27 at α=9°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fauvel-il-1000000.txt
Download as CSV file: xf-fauvel-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FAUVEL 14% 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -1.0214   0.06221   0.05975  -0.0221   1.0000   0.0183
 -14.750  -1.0788   0.05088   0.04806  -0.0291   1.0000   0.0183
 -14.500  -1.0868   0.04757   0.04465  -0.0297   1.0000   0.0185
 -14.250  -1.0810   0.04441   0.04065  -0.0332   0.6985   0.0187
 -14.000  -1.0972   0.04134   0.03733  -0.0316   0.6774   0.0188
 -13.750  -1.1064   0.03903   0.03484  -0.0294   0.6659   0.0189
 -13.500  -1.1139   0.03701   0.03262  -0.0268   0.6569   0.0191
 -13.250  -1.1195   0.03517   0.03060  -0.0238   0.6504   0.0193
 -13.000  -1.1199   0.03384   0.02911  -0.0207   0.6443   0.0195
 -12.750  -1.1207   0.03248   0.02757  -0.0173   0.6394   0.0197
 -12.500  -1.1170   0.03152   0.02648  -0.0140   0.6357   0.0198
 -12.250  -1.1098   0.03108   0.02594  -0.0108   0.6320   0.0200
 -12.000  -1.1133   0.02882   0.02344  -0.0069   0.6287   0.0203
 -11.750  -1.1009   0.02782   0.02238  -0.0048   0.6250   0.0206
 -11.500  -1.0850   0.02725   0.02175  -0.0030   0.6210   0.0208
 -11.250  -1.0680   0.02668   0.02113  -0.0013   0.6183   0.0210
 -11.000  -1.0504   0.02607   0.02047   0.0003   0.6152   0.0212
 -10.750  -1.0320   0.02551   0.01985   0.0018   0.6118   0.0215
 -10.500  -1.0131   0.02491   0.01917   0.0033   0.6085   0.0217
 -10.250  -0.9939   0.02427   0.01843   0.0047   0.6049   0.0220
 -10.000  -0.9742   0.02355   0.01762   0.0061   0.6022   0.0224
  -9.750  -0.9538   0.02287   0.01684   0.0074   0.5993   0.0228
  -9.500  -0.9330   0.02218   0.01602   0.0087   0.5959   0.0231
  -9.250  -0.9113   0.02170   0.01543   0.0100   0.5926   0.0234
  -9.000  -0.8890   0.02143   0.01504   0.0111   0.5892   0.0236
  -8.750  -0.8685   0.01973   0.01326   0.0121   0.5861   0.0242
  -8.500  -0.8451   0.01918   0.01270   0.0130   0.5829   0.0246
  -8.250  -0.8213   0.01876   0.01226   0.0139   0.5795   0.0250
  -8.000  -0.7972   0.01829   0.01174   0.0147   0.5761   0.0253
  -7.750  -0.7730   0.01783   0.01122   0.0155   0.5723   0.0257
  -7.500  -0.7483   0.01736   0.01070   0.0163   0.5689   0.0262
  -7.250  -0.7234   0.01686   0.01015   0.0171   0.5649   0.0266
  -7.000  -0.6982   0.01642   0.00965   0.0178   0.5608   0.0269
  -6.750  -0.6729   0.01608   0.00924   0.0186   0.5566   0.0273
  -6.500  -0.6470   0.01592   0.00902   0.0192   0.5526   0.0276
  -6.250  -0.6237   0.01471   0.00781   0.0201   0.5482   0.0283
  -6.000  -0.5987   0.01423   0.00733   0.0208   0.5429   0.0288
  -5.750  -0.5735   0.01385   0.00692   0.0216   0.5375   0.0292
  -5.500  -0.5477   0.01349   0.00655   0.0222   0.5320   0.0297
  -5.250  -0.5221   0.01314   0.00617   0.0229   0.5257   0.0301
  -5.000  -0.4964   0.01282   0.00582   0.0236   0.5195   0.0306
  -4.750  -0.4704   0.01252   0.00549   0.0242   0.5119   0.0311
  -4.500  -0.4441   0.01230   0.00522   0.0248   0.5035   0.0316
  -4.250  -0.4177   0.01208   0.00497   0.0254   0.4943   0.0319
  -4.000  -0.3938   0.01159   0.00442   0.0264   0.4849   0.0325
  -3.750  -0.3687   0.01124   0.00405   0.0272   0.4753   0.0332
  -3.500  -0.3428   0.01101   0.00379   0.0278   0.4662   0.0338
  -3.250  -0.3166   0.01082   0.00357   0.0284   0.4567   0.0345
  -3.000  -0.2902   0.01065   0.00336   0.0290   0.4479   0.0353
  -2.750  -0.2636   0.01051   0.00318   0.0295   0.4392   0.0361
  -2.500  -0.2367   0.01040   0.00303   0.0300   0.4316   0.0368
  -2.250  -0.2106   0.01019   0.00279   0.0306   0.4247   0.0379
  -2.000  -0.1842   0.01005   0.00263   0.0312   0.4174   0.0393
  -1.750  -0.1572   0.00992   0.00250   0.0316   0.4120   0.0408
  -1.500  -0.1301   0.00983   0.00238   0.0320   0.4057   0.0423
  -1.250  -0.1036   0.00973   0.00226   0.0326   0.3988   0.0465
  -1.000  -0.0775   0.00950   0.00216   0.0332   0.3946   0.0682
  -0.750  -0.0536   0.00913   0.00202   0.0341   0.3898   0.1307
  -0.500  -0.0308   0.00872   0.00195   0.0351   0.3847   0.2324
  -0.250  -0.0046   0.00859   0.00191   0.0356   0.3798   0.2671
   0.000   0.0208   0.00836   0.00186   0.0363   0.3757   0.3200
   0.250   0.0388   0.00760   0.00169   0.0381   0.3715   0.4947
   0.500   0.0522   0.00683   0.00162   0.0411   0.3674   0.7018
   0.750   0.0748   0.00667   0.00165   0.0426   0.3629   0.7653
   1.000   0.0994   0.00655   0.00170   0.0436   0.3600   0.8098
   1.250   0.1261   0.00653   0.00174   0.0443   0.3563   0.8345
   1.500   0.1534   0.00656   0.00178   0.0447   0.3521   0.8515
   1.750   0.1800   0.00663   0.00186   0.0453   0.3471   0.8719
   2.000   0.2078   0.00666   0.00193   0.0457   0.3442   0.8860
   2.250   0.2355   0.00670   0.00200   0.0461   0.3413   0.9006
   2.500   0.2624   0.00677   0.00207   0.0466   0.3379   0.9140
   2.750   0.2915   0.00686   0.00215   0.0466   0.3342   0.9222
   3.000   0.3183   0.00699   0.00224   0.0471   0.3297   0.9303
   3.250   0.3487   0.00706   0.00233   0.0469   0.3270   0.9359
   3.500   0.3763   0.00712   0.00240   0.0471   0.3243   0.9421
   3.750   0.4066   0.00721   0.00248   0.0468   0.3210   0.9465
   4.000   0.4372   0.00732   0.00257   0.0464   0.3169   0.9503
   4.250   0.4653   0.00749   0.00269   0.0465   0.3120   0.9552
   4.500   0.4956   0.00755   0.00277   0.0462   0.3095   0.9590
   4.750   0.5299   0.00765   0.00288   0.0450   0.3058   0.9617
   5.000   0.5632   0.00778   0.00299   0.0440   0.3018   0.9645
   5.250   0.5934   0.00796   0.00312   0.0436   0.2968   0.9677
   5.500   0.6229   0.00805   0.00323   0.0434   0.2936   0.9710
   5.750   0.6595   0.00816   0.00334   0.0416   0.2902   0.9720
   6.000   0.6972   0.00830   0.00347   0.0396   0.2861   0.9729
   6.250   0.7331   0.00849   0.00363   0.0379   0.2814   0.9741
   6.500   0.7673   0.00862   0.00377   0.0366   0.2780   0.9754
   6.750   0.8009   0.00872   0.00388   0.0354   0.2743   0.9770
   7.000   0.8327   0.00885   0.00400   0.0345   0.2689   0.9792
   7.250   0.8604   0.00906   0.00418   0.0345   0.2636   0.9824
   7.500   0.8956   0.00914   0.00428   0.0329   0.2595   0.9832
   7.750   0.9300   0.00928   0.00441   0.0315   0.2533   0.9840
   8.000   0.9640   0.00947   0.00458   0.0300   0.2471   0.9851
   8.250   0.9975   0.00960   0.00472   0.0287   0.2406   0.9864
   8.500   1.0299   0.00984   0.00492   0.0276   0.2324   0.9879
   8.750   1.0620   0.01002   0.00510   0.0265   0.2243   0.9897
   9.000   1.0924   0.01028   0.00534   0.0257   0.2161   0.9917
   9.250   1.1225   0.01058   0.00560   0.0249   0.2054   0.9934
   9.500   1.1554   0.01088   0.00586   0.0235   0.1934   0.9944
   9.750   1.1869   0.01131   0.00622   0.0221   0.1781   0.9958
  10.000   1.2175   0.01184   0.00666   0.0209   0.1616   0.9973
  10.250   1.2477   0.01240   0.00715   0.0197   0.1461   0.9988
  10.500   1.2773   0.01298   0.00766   0.0185   0.1339   1.0000
  10.750   1.2938   0.01346   0.00813   0.0201   0.1263   1.0000
  11.000   1.3102   0.01392   0.00858   0.0217   0.1202   1.0000
  11.250   1.3259   0.01441   0.00906   0.0234   0.1148   1.0000
  11.500   1.3408   0.01492   0.00957   0.0252   0.1097   1.0000
  11.750   1.3564   0.01536   0.01004   0.0269   0.1056   1.0000
  12.000   1.3692   0.01597   0.01063   0.0288   0.1008   1.0000
  12.250   1.3833   0.01648   0.01117   0.0306   0.0969   1.0000
  12.500   1.3955   0.01709   0.01179   0.0326   0.0922   1.0000
  12.750   1.4050   0.01784   0.01254   0.0347   0.0873   1.0000
  13.000   1.4136   0.01862   0.01332   0.0368   0.0824   1.0000
  13.250   1.4135   0.01973   0.01444   0.0397   0.0772   1.0000
  13.500   1.4044   0.02147   0.01624   0.0422   0.0737   1.0000
  13.750   1.3970   0.02498   0.01980   0.0407   0.0689   1.0000
  14.000   1.3916   0.02794   0.02281   0.0402   0.0647   1.0000
  14.250   1.3809   0.03133   0.02622   0.0398   0.0610   1.0000
  14.500   1.3730   0.03446   0.02940   0.0395   0.0581   1.0000
  14.750   1.3604   0.03813   0.03311   0.0389   0.0556   1.0000
  15.000   1.3495   0.04173   0.03678   0.0383   0.0534   1.0000
  15.250   1.3402   0.04528   0.04039   0.0376   0.0517   1.0000
  15.500   1.3294   0.04911   0.04428   0.0366   0.0503   1.0000
  15.750   1.3156   0.05349   0.04871   0.0354   0.0486   1.0000
  16.000   1.3055   0.05757   0.05286   0.0342   0.0475   1.0000
  16.250   1.3004   0.06109   0.05644   0.0331   0.0467   1.0000
  16.500   1.2935   0.06491   0.06034   0.0319   0.0460   1.0000
  16.750   1.2850   0.06897   0.06447   0.0305   0.0452   1.0000
  17.000   1.2781   0.07286   0.06842   0.0292   0.0445   1.0000
  17.250   1.2688   0.07715   0.07276   0.0277   0.0438   1.0000
  17.500   1.2596   0.08148   0.07714   0.0261   0.0431   1.0000
  17.750   1.2513   0.08573   0.08144   0.0246   0.0423   1.0000
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