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FAUVEL 14% AIRFOIL (fauvel-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FAUVEL 14% AIRFOIL (fauvel-il)
Reynolds number: 500,000
Max Cl/Cd: 89.76 at α=9.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fauvel-il-500000.txt
Download as CSV file: xf-fauvel-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.4549   0.14343   0.14030   0.0328   0.6382   0.0305
 -12.750  -0.5288   0.13697   0.13357   0.0234   0.6535   0.0303
 -12.500  -0.5571   0.12455   0.12119   0.0152   0.6546   0.0322
 -12.250  -0.5480   0.12206   0.11869   0.0148   0.6504   0.0324
 -12.000  -0.5387   0.11974   0.11635   0.0143   0.6458   0.0327
 -11.750  -0.5323   0.11674   0.11331   0.0133   0.6418   0.0330
 -11.500  -0.5267   0.11364   0.11019   0.0121   0.6381   0.0335
 -11.250  -0.6178   0.08401   0.08063  -0.0119   0.6457   0.0369
 -11.000  -0.5899   0.08877   0.08540  -0.0047   0.6392   0.0372
 -10.750  -0.5943   0.08379   0.08044  -0.0075   0.6365   0.0374
 -10.500  -0.5828   0.08339   0.08004  -0.0065   0.6320   0.0377
 -10.250  -0.6471   0.06785   0.06439  -0.0181   0.6334   0.0378
 -10.000  -0.6810   0.06256   0.05897  -0.0180   0.6317   0.0379
  -9.750  -0.8187   0.04594   0.04140  -0.0070   0.6355   0.0314
  -9.500  -0.8199   0.04278   0.03807  -0.0043   0.6321   0.0308
  -9.250  -0.8305   0.03821   0.03308  -0.0003   0.6292   0.0304
  -9.000  -0.8311   0.03456   0.02899   0.0031   0.6259   0.0304
  -8.750  -0.8239   0.03184   0.02587   0.0059   0.6223   0.0307
  -8.500  -0.8114   0.02981   0.02349   0.0082   0.6186   0.0312
  -8.250  -0.7960   0.02874   0.02206   0.0105   0.6145   0.0318
  -8.000  -0.7797   0.02658   0.01960   0.0122   0.6104   0.0322
  -7.750  -0.7581   0.02477   0.01765   0.0131   0.6061   0.0327
  -7.500  -0.7346   0.02373   0.01656   0.0138   0.6016   0.0332
  -7.250  -0.7104   0.02286   0.01565   0.0146   0.5969   0.0337
  -7.000  -0.6862   0.02199   0.01467   0.0154   0.5925   0.0342
  -6.750  -0.6618   0.02122   0.01377   0.0162   0.5880   0.0348
  -6.500  -0.6368   0.02046   0.01292   0.0169   0.5830   0.0356
  -6.250  -0.6115   0.01977   0.01210   0.0177   0.5776   0.0362
  -6.000  -0.5859   0.01915   0.01135   0.0184   0.5728   0.0366
  -5.750  -0.5600   0.01856   0.01066   0.0191   0.5678   0.0370
  -5.500  -0.5333   0.01725   0.00936   0.0194   0.5621   0.0377
  -5.250  -0.5076   0.01657   0.00867   0.0200   0.5567   0.0383
  -5.000  -0.4818   0.01607   0.00817   0.0206   0.5506   0.0392
  -4.750  -0.4559   0.01558   0.00767   0.0212   0.5438   0.0400
  -4.500  -0.4304   0.01513   0.00715   0.0220   0.5379   0.0407
  -4.250  -0.4045   0.01467   0.00669   0.0227   0.5306   0.0413
  -4.000  -0.3789   0.01428   0.00624   0.0234   0.5235   0.0419
  -3.750  -0.3536   0.01386   0.00579   0.0242   0.5158   0.0425
  -3.500  -0.3297   0.01331   0.00523   0.0252   0.5076   0.0436
  -3.250  -0.3045   0.01297   0.00489   0.0259   0.4993   0.0449
  -3.000  -0.2789   0.01269   0.00458   0.0266   0.4907   0.0463
  -2.750  -0.2531   0.01244   0.00429   0.0273   0.4827   0.0475
  -2.500  -0.2274   0.01219   0.00400   0.0281   0.4742   0.0489
  -2.250  -0.2020   0.01193   0.00373   0.0288   0.4663   0.0512
  -2.000  -0.1758   0.01175   0.00352   0.0294   0.4580   0.0540
  -1.750  -0.1501   0.01157   0.00332   0.0301   0.4506   0.0592
  -1.500  -0.1248   0.01130   0.00316   0.0308   0.4436   0.0769
  -1.250  -0.1049   0.01061   0.00293   0.0323   0.4375   0.1917
  -1.000  -0.0812   0.01030   0.00286   0.0332   0.4315   0.2663
  -0.750  -0.0569   0.01001   0.00276   0.0341   0.4253   0.3202
  -0.500  -0.0400   0.00925   0.00253   0.0361   0.4197   0.4669
  -0.250  -0.0324   0.00828   0.00249   0.0404   0.4152   0.7211
   0.000  -0.0097   0.00810   0.00258   0.0421   0.4102   0.7934
   0.250   0.0161   0.00811   0.00267   0.0430   0.4051   0.8341
   0.500   0.0423   0.00822   0.00276   0.0439   0.3999   0.8603
   0.750   0.0698   0.00829   0.00285   0.0444   0.3954   0.8785
   1.000   0.0983   0.00837   0.00295   0.0448   0.3904   0.8932
   1.250   0.1272   0.00853   0.00309   0.0451   0.3857   0.9090
   1.500   0.1576   0.00879   0.00328   0.0451   0.3809   0.9209
   1.750   0.1878   0.00894   0.00345   0.0452   0.3773   0.9319
   2.000   0.2226   0.00912   0.00361   0.0442   0.3729   0.9379
   2.250   0.2507   0.00926   0.00369   0.0445   0.3686   0.9448
   2.500   0.2884   0.00952   0.00386   0.0427   0.3637   0.9472
   2.750   0.3252   0.00964   0.00399   0.0411   0.3603   0.9496
   3.000   0.3606   0.00977   0.00410   0.0397   0.3564   0.9525
   3.250   0.3883   0.00988   0.00419   0.0399   0.3528   0.9581
   3.500   0.4273   0.01006   0.00431   0.0377   0.3487   0.9591
   3.750   0.4664   0.01027   0.00448   0.0355   0.3445   0.9605
   4.000   0.5047   0.01038   0.00461   0.0335   0.3410   0.9624
   4.250   0.5400   0.01050   0.00472   0.0321   0.3373   0.9650
   4.500   0.5679   0.01062   0.00481   0.0321   0.3333   0.9699
   4.750   0.6053   0.01085   0.00496   0.0302   0.3284   0.9717
   5.000   0.6452   0.01091   0.00508   0.0278   0.3244   0.9736
   5.250   0.6813   0.01099   0.00516   0.0261   0.3201   0.9759
   5.500   0.7142   0.01110   0.00524   0.0250   0.3153   0.9786
   5.750   0.7431   0.01129   0.00541   0.0247   0.3110   0.9824
   6.000   0.7798   0.01133   0.00549   0.0229   0.3073   0.9837
   6.250   0.8156   0.01139   0.00558   0.0212   0.3032   0.9854
   6.500   0.8502   0.01151   0.00567   0.0197   0.2990   0.9875
   6.750   0.8832   0.01169   0.00584   0.0185   0.2947   0.9900
   7.000   0.9158   0.01177   0.00599   0.0174   0.2910   0.9926
   7.250   0.9508   0.01182   0.00607   0.0158   0.2861   0.9944
   7.500   0.9852   0.01195   0.00616   0.0142   0.2808   0.9964
   7.750   1.0198   0.01202   0.00629   0.0127   0.2755   0.9985
   8.000   1.0527   0.01209   0.00639   0.0114   0.2693   1.0000
   8.250   1.0738   0.01229   0.00655   0.0124   0.2638   1.0000
   8.500   1.0964   0.01236   0.00670   0.0133   0.2578   1.0000
   8.750   1.1175   0.01253   0.00686   0.0143   0.2508   1.0000
   9.000   1.1388   0.01271   0.00708   0.0154   0.2444   1.0000
   9.250   1.1597   0.01292   0.00730   0.0164   0.2373   1.0000
   9.500   1.1799   0.01318   0.00757   0.0176   0.2306   1.0000
   9.750   1.2000   0.01345   0.00785   0.0187   0.2224   1.0000
  10.000   1.2193   0.01377   0.00818   0.0199   0.2139   1.0000
  10.250   1.2371   0.01420   0.00857   0.0213   0.2035   1.0000
  10.500   1.2548   0.01462   0.00899   0.0227   0.1921   1.0000
  10.750   1.2708   0.01515   0.00950   0.0243   0.1796   1.0000
  11.000   1.2849   0.01579   0.01010   0.0260   0.1669   1.0000
  11.250   1.2977   0.01650   0.01077   0.0279   0.1557   1.0000
  11.500   1.3089   0.01728   0.01152   0.0299   0.1462   1.0000
  11.750   1.3189   0.01810   0.01232   0.0320   0.1381   1.0000
  12.000   1.3283   0.01891   0.01316   0.0340   0.1317   1.0000
  12.250   1.3341   0.01990   0.01415   0.0363   0.1259   1.0000
  12.500   1.3368   0.02103   0.01531   0.0387   0.1212   1.0000
  12.750   1.3310   0.02239   0.01674   0.0417   0.1178   1.0000
  13.000   1.3230   0.02535   0.01977   0.0412   0.1143   1.0000
  13.250   1.3135   0.02854   0.02300   0.0409   0.1106   1.0000
  13.500   1.3142   0.03073   0.02526   0.0409   0.1072   1.0000
  13.750   1.3086   0.03352   0.02810   0.0408   0.1035   1.0000
  14.000   1.2973   0.03693   0.03153   0.0405   0.1002   1.0000
  14.250   1.2927   0.03979   0.03446   0.0402   0.0968   1.0000
  14.500   1.2865   0.04288   0.03761   0.0397   0.0929   1.0000
  14.750   1.2743   0.04668   0.04143   0.0390   0.0894   1.0000
  15.000   1.2665   0.05013   0.04494   0.0382   0.0854   1.0000
  15.250   1.2575   0.05394   0.04878   0.0371   0.0814   1.0000
  15.500   1.2449   0.05828   0.05315   0.0358   0.0778   1.0000
  15.750   1.2376   0.06208   0.05700   0.0347   0.0737   1.0000
  16.000   1.2253   0.06655   0.06149   0.0332   0.0707   1.0000
  16.250   1.2173   0.07055   0.06553   0.0319   0.0678   1.0000
  16.500   1.2115   0.07433   0.06935   0.0306   0.0653   1.0000
  16.750   1.2007   0.07881   0.07384   0.0290   0.0628   1.0000
  17.000   1.1931   0.08289   0.07795   0.0276   0.0611   1.0000
  17.250   1.1914   0.08624   0.08136   0.0265   0.0594   1.0000
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