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FAUVEL 14% AIRFOIL (fauvel-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FAUVEL 14% AIRFOIL (fauvel-il)
Reynolds number: 500,000
Max Cl/Cd: 82.65 at α=8.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fauvel-il-500000-n5.txt
Download as CSV file: xf-fauvel-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.9746   0.05785   0.05384  -0.0271   0.6732   0.0183
 -14.000  -1.0092   0.05101   0.04672  -0.0298   0.6669   0.0183
 -13.750  -1.0324   0.04652   0.04199  -0.0298   0.6598   0.0184
 -13.500  -1.0451   0.04352   0.03878  -0.0286   0.6538   0.0185
 -13.250  -1.0570   0.04079   0.03583  -0.0267   0.6485   0.0187
 -13.000  -1.0647   0.03855   0.03339  -0.0242   0.6434   0.0189
 -12.750  -1.0711   0.03647   0.03107  -0.0212   0.6382   0.0191
 -12.500  -1.0733   0.03472   0.02911  -0.0182   0.6333   0.0193
 -12.250  -1.0734   0.03311   0.02728  -0.0150   0.6285   0.0195
 -12.000  -1.0710   0.03169   0.02563  -0.0117   0.6237   0.0198
 -11.750  -1.0658   0.03048   0.02420  -0.0086   0.6199   0.0200
 -11.500  -1.0571   0.02936   0.02295  -0.0060   0.6164   0.0202
 -11.250  -1.0431   0.02852   0.02204  -0.0040   0.6127   0.0204
 -11.000  -1.0274   0.02779   0.02124  -0.0023   0.6089   0.0206
 -10.750  -1.0100   0.02723   0.02060  -0.0007   0.6055   0.0208
 -10.500  -0.9919   0.02663   0.01994   0.0008   0.6023   0.0210
 -10.250  -0.9730   0.02603   0.01927   0.0022   0.5989   0.0213
 -10.000  -0.9539   0.02536   0.01851   0.0036   0.5953   0.0217
  -9.750  -0.9344   0.02463   0.01765   0.0050   0.5916   0.0220
  -9.500  -0.9145   0.02386   0.01674   0.0063   0.5883   0.0224
  -9.250  -0.8936   0.02309   0.01585   0.0075   0.5851   0.0227
  -9.000  -0.8721   0.02237   0.01501   0.0087   0.5812   0.0231
  -8.750  -0.8499   0.02173   0.01423   0.0098   0.5775   0.0234
  -8.500  -0.8273   0.02114   0.01351   0.0108   0.5737   0.0236
  -8.250  -0.8051   0.02036   0.01269   0.0118   0.5702   0.0240
  -8.000  -0.7818   0.01983   0.01216   0.0127   0.5664   0.0244
  -7.750  -0.7580   0.01935   0.01164   0.0135   0.5619   0.0248
  -7.500  -0.7341   0.01889   0.01113   0.0144   0.5574   0.0252
  -7.250  -0.7100   0.01840   0.01057   0.0152   0.5534   0.0255
  -7.000  -0.6855   0.01790   0.01003   0.0160   0.5491   0.0259
  -6.750  -0.6609   0.01743   0.00950   0.0168   0.5442   0.0264
  -6.500  -0.6363   0.01698   0.00898   0.0176   0.5391   0.0267
  -6.250  -0.6112   0.01657   0.00851   0.0184   0.5337   0.0272
  -6.000  -0.5858   0.01624   0.00811   0.0190   0.5274   0.0275
  -5.750  -0.5619   0.01566   0.00752   0.0199   0.5217   0.0281
  -5.500  -0.5372   0.01524   0.00709   0.0207   0.5155   0.0286
  -5.250  -0.5122   0.01487   0.00669   0.0214   0.5081   0.0290
  -5.000  -0.4870   0.01453   0.00632   0.0222   0.5004   0.0295
  -4.750  -0.4617   0.01420   0.00596   0.0229   0.4914   0.0300
  -4.500  -0.4362   0.01391   0.00561   0.0236   0.4830   0.0305
  -4.250  -0.4107   0.01363   0.00529   0.0243   0.4742   0.0310
  -4.000  -0.3849   0.01339   0.00500   0.0249   0.4662   0.0316
  -3.750  -0.3592   0.01315   0.00471   0.0256   0.4575   0.0322
  -3.500  -0.3340   0.01286   0.00440   0.0263   0.4493   0.0330
  -3.250  -0.3081   0.01265   0.00416   0.0269   0.4408   0.0338
  -3.000  -0.2821   0.01247   0.00393   0.0275   0.4334   0.0346
  -2.750  -0.2557   0.01229   0.00373   0.0281   0.4268   0.0355
  -2.500  -0.2294   0.01215   0.00355   0.0286   0.4202   0.0364
  -2.250  -0.2030   0.01200   0.00337   0.0292   0.4143   0.0375
  -2.000  -0.1767   0.01184   0.00320   0.0297   0.4080   0.0392
  -1.750  -0.1502   0.01172   0.00306   0.0303   0.4017   0.0417
  -1.500  -0.1238   0.01159   0.00293   0.0308   0.3967   0.0458
  -1.250  -0.0977   0.01141   0.00282   0.0313   0.3918   0.0580
  -1.000  -0.0721   0.01121   0.00272   0.0320   0.3868   0.0853
  -0.750  -0.0466   0.01104   0.00261   0.0326   0.3819   0.1136
  -0.500  -0.0233   0.01063   0.00253   0.0335   0.3776   0.1975
  -0.250   0.0020   0.01043   0.00248   0.0341   0.3727   0.2489
   0.000   0.0276   0.01027   0.00243   0.0347   0.3683   0.2863
   0.250   0.0517   0.01001   0.00237   0.0355   0.3643   0.3497
   0.500   0.0602   0.00877   0.00217   0.0392   0.3615   0.6375
   0.750   0.0815   0.00849   0.00219   0.0409   0.3578   0.7175
   1.000   0.1056   0.00837   0.00223   0.0420   0.3536   0.7693
   1.250   0.1307   0.00832   0.00232   0.0430   0.3494   0.8155
   1.500   0.1575   0.00836   0.00241   0.0436   0.3457   0.8450
   1.750   0.1856   0.00839   0.00251   0.0440   0.3426   0.8682
   2.000   0.2140   0.00846   0.00259   0.0442   0.3392   0.8819
   2.250   0.2425   0.00854   0.00266   0.0444   0.3353   0.8920
   2.500   0.2715   0.00864   0.00273   0.0444   0.3315   0.9002
   2.750   0.3006   0.00875   0.00282   0.0444   0.3280   0.9075
   3.000   0.3289   0.00882   0.00289   0.0445   0.3252   0.9141
   3.250   0.3603   0.00892   0.00299   0.0440   0.3219   0.9195
   3.500   0.3892   0.00903   0.00308   0.0440   0.3187   0.9255
   3.750   0.4185   0.00915   0.00318   0.0438   0.3152   0.9309
   4.000   0.4507   0.00931   0.00331   0.0430   0.3117   0.9354
   4.250   0.4799   0.00941   0.00342   0.0429   0.3089   0.9414
   4.500   0.5104   0.00952   0.00354   0.0425   0.3056   0.9454
   4.750   0.5435   0.00965   0.00367   0.0415   0.3017   0.9483
   5.000   0.5753   0.00983   0.00381   0.0408   0.2971   0.9528
   5.250   0.6040   0.00996   0.00394   0.0407   0.2930   0.9583
   5.500   0.6383   0.01009   0.00409   0.0394   0.2889   0.9601
   5.750   0.6715   0.01025   0.00423   0.0383   0.2836   0.9619
   6.000   0.7038   0.01043   0.00438   0.0373   0.2787   0.9640
   6.250   0.7350   0.01056   0.00453   0.0366   0.2749   0.9668
   6.500   0.7626   0.01070   0.00470   0.0367   0.2711   0.9706
   6.750   0.7962   0.01089   0.00487   0.0354   0.2664   0.9718
   7.000   0.8292   0.01107   0.00505   0.0342   0.2621   0.9733
   7.250   0.8617   0.01122   0.00524   0.0332   0.2579   0.9751
   7.500   0.8930   0.01141   0.00544   0.0323   0.2527   0.9774
   7.750   0.9222   0.01164   0.00565   0.0319   0.2469   0.9803
   8.000   0.9518   0.01183   0.00586   0.0313   0.2395   0.9828
   8.250   0.9841   0.01209   0.00611   0.0301   0.2320   0.9842
   8.500   1.0157   0.01235   0.00635   0.0290   0.2222   0.9859
   8.750   1.0463   0.01266   0.00665   0.0281   0.2118   0.9880
   9.000   1.0754   0.01307   0.00701   0.0273   0.1974   0.9904
   9.250   1.1030   0.01356   0.00744   0.0267   0.1823   0.9929
   9.500   1.1326   0.01408   0.00791   0.0256   0.1681   0.9947
   9.750   1.1617   0.01468   0.00846   0.0245   0.1537   0.9969
  10.000   1.1904   0.01533   0.00906   0.0234   0.1412   0.9989
  10.250   1.2141   0.01597   0.00968   0.0232   0.1316   1.0000
  10.500   1.2281   0.01660   0.01029   0.0250   0.1244   1.0000
  10.750   1.2423   0.01717   0.01087   0.0268   0.1187   1.0000
  11.000   1.2544   0.01786   0.01157   0.0287   0.1128   1.0000
  11.250   1.2668   0.01851   0.01223   0.0306   0.1086   1.0000
  11.500   1.2781   0.01919   0.01295   0.0325   0.1042   1.0000
  11.750   1.2860   0.02006   0.01383   0.0346   0.1002   1.0000
  12.000   1.2934   0.02094   0.01475   0.0366   0.0969   1.0000
  12.250   1.2942   0.02200   0.01587   0.0393   0.0938   1.0000
  12.500   1.2848   0.02439   0.01834   0.0403   0.0910   1.0000
  12.750   1.2801   0.02717   0.02118   0.0400   0.0882   1.0000
  13.000   1.2793   0.02948   0.02355   0.0400   0.0854   1.0000
  13.250   1.2754   0.03211   0.02622   0.0400   0.0820   1.0000
  13.500   1.2684   0.03507   0.02922   0.0398   0.0791   1.0000
  13.750   1.2636   0.03791   0.03212   0.0396   0.0762   1.0000
  14.000   1.2575   0.04096   0.03522   0.0392   0.0730   1.0000
  14.250   1.2486   0.04441   0.03871   0.0386   0.0702   1.0000
  14.500   1.2416   0.04773   0.04208   0.0379   0.0675   1.0000
  14.750   1.2342   0.05118   0.04559   0.0372   0.0648   1.0000
  15.000   1.2250   0.05504   0.04948   0.0361   0.0620   1.0000
  15.250   1.2194   0.05858   0.05307   0.0351   0.0596   1.0000
  15.500   1.2136   0.06219   0.05674   0.0340   0.0574   1.0000
  15.750   1.2045   0.06628   0.06087   0.0327   0.0550   1.0000
  16.000   1.1983   0.07008   0.06472   0.0315   0.0533   1.0000
  16.250   1.1939   0.07368   0.06838   0.0303   0.0516   1.0000
  16.500   1.1887   0.07743   0.07218   0.0290   0.0502   1.0000
  16.750   1.1804   0.08167   0.07646   0.0275   0.0486   1.0000
  17.000   1.1757   0.08546   0.08030   0.0262   0.0475   1.0000
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