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FAUVEL 14% AIRFOIL (fauvel-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FAUVEL 14% AIRFOIL (fauvel-il)
Reynolds number: 1,000,000
Max Cl/Cd: 96.01 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fauvel-il-1000000-n5.txt
Download as CSV file: xf-fauvel-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.3326   0.05422   0.05078  -0.0309   1.0000   0.0144
 -17.500  -1.3463   0.04928   0.04571  -0.0331   1.0000   0.0145
 -17.000  -1.3618   0.04230   0.03850  -0.0343   1.0000   0.0146
 -16.500  -1.3630   0.03773   0.03377  -0.0332   1.0000   0.0149
 -16.000  -1.3357   0.03451   0.02991  -0.0348   0.7509   0.0151
 -15.750  -1.3353   0.03317   0.02827  -0.0327   0.6690   0.0152
 -15.500  -1.3306   0.03193   0.02689  -0.0308   0.6523   0.0153
 -15.250  -1.3242   0.03082   0.02569  -0.0289   0.6432   0.0155
 -15.000  -1.3171   0.02978   0.02454  -0.0268   0.6365   0.0156
 -14.750  -1.3100   0.02876   0.02342  -0.0246   0.6316   0.0158
 -14.500  -1.3002   0.02793   0.02251  -0.0225   0.6268   0.0160
 -14.000  -1.2808   0.02627   0.02067  -0.0180   0.6189   0.0163
 -13.750  -1.2685   0.02560   0.01991  -0.0158   0.6154   0.0165
 -13.500  -1.2576   0.02484   0.01906  -0.0134   0.6123   0.0166
 -13.250  -1.2449   0.02420   0.01832  -0.0111   0.6089   0.0167
 -12.750  -1.2189   0.02297   0.01695  -0.0063   0.6013   0.0171
 -12.500  -1.2047   0.02244   0.01638  -0.0040   0.5974   0.0173
 -12.250  -1.1883   0.02195   0.01583  -0.0021   0.5939   0.0174
 -12.000  -1.1693   0.02151   0.01535  -0.0005   0.5909   0.0176
 -11.500  -1.1293   0.02066   0.01441   0.0023   0.5855   0.0180
 -11.250  -1.1085   0.02025   0.01394   0.0036   0.5829   0.0182
 -11.000  -1.0875   0.01981   0.01345   0.0048   0.5801   0.0184
 -10.750  -1.0660   0.01939   0.01298   0.0060   0.5770   0.0186
 -10.500  -1.0443   0.01897   0.01249   0.0072   0.5738   0.0189
 -10.250  -1.0220   0.01857   0.01203   0.0083   0.5710   0.0191
 -10.000  -0.9991   0.01819   0.01161   0.0094   0.5683   0.0194
  -9.750  -0.9758   0.01783   0.01120   0.0104   0.5653   0.0197
  -9.500  -0.9530   0.01740   0.01070   0.0114   0.5618   0.0198
  -9.250  -0.9290   0.01709   0.01033   0.0123   0.5581   0.0200
  -9.000  -0.9069   0.01656   0.00975   0.0135   0.5550   0.0203
  -8.750  -0.8835   0.01614   0.00930   0.0144   0.5518   0.0206
  -8.500  -0.8594   0.01577   0.00892   0.0153   0.5480   0.0208
  -8.250  -0.8349   0.01545   0.00857   0.0161   0.5439   0.0210
  -8.000  -0.8101   0.01516   0.00824   0.0169   0.5399   0.0213
  -7.750  -0.7851   0.01487   0.00792   0.0177   0.5361   0.0216
  -7.500  -0.7600   0.01458   0.00760   0.0184   0.5316   0.0219
  -7.250  -0.7345   0.01432   0.00731   0.0191   0.5256   0.0223
  -7.000  -0.7093   0.01404   0.00698   0.0198   0.5200   0.0226
  -6.750  -0.6839   0.01375   0.00665   0.0205   0.5141   0.0229
  -6.500  -0.6584   0.01347   0.00633   0.0212   0.5071   0.0232
  -6.250  -0.6327   0.01322   0.00604   0.0219   0.5003   0.0234
  -6.000  -0.6068   0.01299   0.00576   0.0225   0.4908   0.0236
  -5.750  -0.5820   0.01265   0.00537   0.0233   0.4815   0.0239
  -5.500  -0.5567   0.01237   0.00505   0.0241   0.4709   0.0244
  -5.250  -0.5307   0.01216   0.00481   0.0247   0.4624   0.0248
  -5.000  -0.5046   0.01196   0.00458   0.0253   0.4531   0.0252
  -4.750  -0.4784   0.01177   0.00435   0.0258   0.4452   0.0255
  -4.500  -0.4522   0.01159   0.00413   0.0264   0.4361   0.0259
  -4.250  -0.4258   0.01142   0.00393   0.0270   0.4286   0.0263
  -4.000  -0.3993   0.01127   0.00373   0.0275   0.4202   0.0267
  -3.750  -0.3727   0.01112   0.00355   0.0280   0.4142   0.0271
  -3.500  -0.3459   0.01097   0.00338   0.0285   0.4084   0.0274
  -3.250  -0.3194   0.01082   0.00320   0.0290   0.4022   0.0279
  -3.000  -0.2930   0.01065   0.00302   0.0296   0.3965   0.0287
  -2.750  -0.2661   0.01051   0.00287   0.0301   0.3908   0.0293
  -2.500  -0.2392   0.01040   0.00273   0.0305   0.3849   0.0299
  -2.250  -0.2122   0.01030   0.00261   0.0309   0.3801   0.0306
  -2.000  -0.1850   0.01019   0.00250   0.0313   0.3761   0.0313
  -1.750  -0.1577   0.01010   0.00240   0.0317   0.3713   0.0319
  -1.500  -0.1307   0.01001   0.00229   0.0321   0.3661   0.0332
  -1.250  -0.1035   0.00993   0.00220   0.0325   0.3615   0.0348
  -1.000  -0.0761   0.00984   0.00213   0.0329   0.3575   0.0368
  -0.750  -0.0490   0.00975   0.00205   0.0333   0.3534   0.0422
  -0.500  -0.0229   0.00958   0.00197   0.0338   0.3493   0.0686
  -0.250   0.0036   0.00945   0.00192   0.0343   0.3453   0.0919
   0.000   0.0296   0.00925   0.00184   0.0349   0.3420   0.1290
   0.250   0.0536   0.00891   0.00180   0.0357   0.3381   0.2182
   0.500   0.0804   0.00882   0.00178   0.0361   0.3342   0.2455
   0.750   0.1072   0.00874   0.00177   0.0365   0.3305   0.2748
   1.000   0.1330   0.00856   0.00175   0.0370   0.3277   0.3249
   1.250   0.1573   0.00825   0.00170   0.0378   0.3250   0.4086
   1.500   0.1709   0.00731   0.00158   0.0406   0.3221   0.6574
   1.750   0.1925   0.00705   0.00160   0.0421   0.3185   0.7374
   2.000   0.2174   0.00698   0.00164   0.0430   0.3151   0.7777
   2.250   0.2424   0.00693   0.00171   0.0439   0.3118   0.8167
   2.500   0.2689   0.00691   0.00177   0.0445   0.3098   0.8437
   2.750   0.2966   0.00693   0.00183   0.0448   0.3072   0.8586
   3.000   0.3243   0.00697   0.00190   0.0451   0.3040   0.8710
   3.250   0.3523   0.00703   0.00196   0.0453   0.3005   0.8802
   3.500   0.3804   0.00711   0.00204   0.0454   0.2970   0.8881
   3.750   0.4084   0.00718   0.00211   0.0456   0.2944   0.8956
   4.000   0.4372   0.00724   0.00218   0.0456   0.2912   0.9016
   4.250   0.4656   0.00731   0.00226   0.0456   0.2874   0.9080
   4.500   0.4936   0.00741   0.00234   0.0457   0.2832   0.9141
   4.750   0.5224   0.00752   0.00245   0.0457   0.2787   0.9219
   5.000   0.5503   0.00760   0.00254   0.0458   0.2755   0.9292
   5.250   0.5803   0.00770   0.00264   0.0455   0.2709   0.9337
   5.500   0.6092   0.00783   0.00276   0.0454   0.2657   0.9388
   5.750   0.6372   0.00795   0.00287   0.0454   0.2621   0.9445
   6.000   0.6693   0.00806   0.00300   0.0446   0.2582   0.9495
   6.250   0.6985   0.00820   0.00314   0.0444   0.2534   0.9555
   6.500   0.7285   0.00837   0.00328   0.0439   0.2488   0.9592
   6.750   0.7607   0.00850   0.00343   0.0430   0.2453   0.9615
   7.000   0.7917   0.00867   0.00358   0.0423   0.2384   0.9642
   7.250   0.8206   0.00887   0.00375   0.0420   0.2318   0.9678
   7.500   0.8495   0.00903   0.00392   0.0417   0.2257   0.9710
   7.750   0.8816   0.00929   0.00413   0.0406   0.2167   0.9723
   8.000   0.9134   0.00957   0.00437   0.0396   0.2057   0.9737
   8.250   0.9447   0.00984   0.00461   0.0386   0.1956   0.9754
   8.500   0.9740   0.01023   0.00492   0.0380   0.1808   0.9775
   8.750   1.0002   0.01076   0.00534   0.0378   0.1616   0.9806
   9.000   1.0275   0.01125   0.00576   0.0374   0.1455   0.9829
   9.250   1.0575   0.01175   0.00619   0.0363   0.1326   0.9841
   9.500   1.0871   0.01224   0.00664   0.0353   0.1226   0.9856
   9.750   1.1164   0.01267   0.00704   0.0345   0.1152   0.9873
  10.000   1.1449   0.01312   0.00747   0.0338   0.1089   0.9893
  10.250   1.1726   0.01353   0.00788   0.0332   0.1040   0.9914
  10.500   1.1993   0.01402   0.00835   0.0328   0.0988   0.9934
  10.750   1.2292   0.01441   0.00876   0.0317   0.0947   0.9948
  11.000   1.2576   0.01498   0.00930   0.0307   0.0889   0.9965
  11.250   1.2861   0.01546   0.00979   0.0298   0.0843   0.9981
  11.500   1.3132   0.01613   0.01043   0.0288   0.0781   0.9994
  11.750   1.3338   0.01673   0.01104   0.0292   0.0726   1.0000
  12.000   1.3445   0.01740   0.01170   0.0313   0.0679   1.0000
  12.250   1.3536   0.01815   0.01244   0.0335   0.0631   1.0000
  12.500   1.3604   0.01900   0.01331   0.0359   0.0588   1.0000
  12.750   1.3621   0.02006   0.01439   0.0386   0.0553   1.0000
  13.000   1.3519   0.02178   0.01618   0.0413   0.0534   1.0000
  13.250   1.3490   0.02477   0.01924   0.0401   0.0508   1.0000
  13.500   1.3456   0.02754   0.02206   0.0396   0.0487   1.0000
  13.750   1.3411   0.03032   0.02489   0.0394   0.0467   1.0000
  14.000   1.3369   0.03309   0.02771   0.0392   0.0453   1.0000
  14.250   1.3302   0.03616   0.03083   0.0388   0.0436   1.0000
  14.500   1.3236   0.03928   0.03401   0.0384   0.0426   1.0000
  14.750   1.3169   0.04250   0.03730   0.0378   0.0415   1.0000
  15.000   1.3112   0.04570   0.04056   0.0371   0.0407   1.0000
  15.250   1.3051   0.04902   0.04395   0.0363   0.0399   1.0000
  15.500   1.2999   0.05241   0.04740   0.0354   0.0393   1.0000
  15.750   1.2934   0.05604   0.05109   0.0344   0.0384   1.0000
  16.000   1.2869   0.05972   0.05485   0.0333   0.0379   1.0000
  16.250   1.2799   0.06355   0.05874   0.0320   0.0372   1.0000
  16.500   1.2740   0.06726   0.06250   0.0309   0.0367   1.0000
  16.750   1.2677   0.07108   0.06639   0.0296   0.0361   1.0000
  17.000   1.2627   0.07481   0.07018   0.0283   0.0359   1.0000
  17.250   1.2601   0.07820   0.07364   0.0272   0.0355   1.0000
  17.500   1.2548   0.08204   0.07755   0.0258   0.0352   1.0000
  17.750   1.2521   0.08554   0.08110   0.0245   0.0348   1.0000
  18.000   1.2465   0.08949   0.08512   0.0231   0.0345   1.0000
  18.250   1.2439   0.09302   0.08871   0.0218   0.0342   1.0000
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