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FX 63-110 AIRFOIL (fx63110-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 63-110 AIRFOIL (fx63110-il)
Reynolds number: 1,000,000
Max Cl/Cd: 136.26 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx63110-il-1000000.txt
Download as CSV file: xf-fx63110-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 63-110 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
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.7328   0.06629   0.06424  -0.0638   1.0000   0.0118
 -13.000  -0.7792   0.05419   0.05197  -0.0712   1.0000   0.0116
 -12.750  -0.8036   0.04733   0.04501  -0.0753   1.0000   0.0115
 -12.500  -0.8336   0.04122   0.03880  -0.0781   1.0000   0.0115
 -12.250  -0.8663   0.03513   0.03256  -0.0816   1.0000   0.0114
 -12.000  -0.8494   0.02648   0.02339  -0.0988   0.9976   0.0118
 -11.750  -0.8159   0.02395   0.02068  -0.1044   0.9958   0.0122
 -11.500  -0.7811   0.02258   0.01920  -0.1081   0.9945   0.0125
 -11.250  -0.7479   0.02156   0.01809  -0.1107   0.9929   0.0128
 -11.000  -0.7149   0.02050   0.01692  -0.1132   0.9907   0.0133
 -10.750  -0.6810   0.01939   0.01567  -0.1158   0.9888   0.0137
 -10.500  -0.6463   0.01845   0.01459  -0.1183   0.9872   0.0141
 -10.250  -0.6110   0.01723   0.01320  -0.1212   0.9858   0.0146
 -10.000  -0.5750   0.01613   0.01202  -0.1240   0.9847   0.0153
  -9.750  -0.5416   0.01567   0.01153  -0.1256   0.9826   0.0159
  -9.500  -0.5104   0.01519   0.01101  -0.1266   0.9787   0.0165
  -9.250  -0.4761   0.01471   0.01045  -0.1283   0.9763   0.0172
  -9.000  -0.4406   0.01437   0.01003  -0.1301   0.9743   0.0178
  -8.750  -0.4043   0.01332   0.00892  -0.1327   0.9727   0.0189
  -8.500  -0.3764   0.01298   0.00856  -0.1328   0.9656   0.0196
  -8.250  -0.3426   0.01260   0.00813  -0.1342   0.9616   0.0205
  -8.000  -0.3104   0.01224   0.00771  -0.1352   0.9551   0.0213
  -7.750  -0.2741   0.01151   0.00690  -0.1373   0.9491   0.0224
  -7.500  -0.2348   0.01110   0.00649  -0.1400   0.9441   0.0235
  -7.250  -0.1962   0.01085   0.00619  -0.1423   0.9358   0.0248
  -7.000  -0.1572   0.01055   0.00582  -0.1447   0.9259   0.0259
  -6.750  -0.1210   0.01001   0.00516  -0.1467   0.9129   0.0270
  -6.500  -0.0890   0.00963   0.00471  -0.1477   0.8992   0.0284
  -6.250  -0.0594   0.00947   0.00448  -0.1481   0.8867   0.0297
  -6.000  -0.0307   0.00928   0.00422  -0.1482   0.8754   0.0309
  -5.750  -0.0020   0.00914   0.00400  -0.1484   0.8651   0.0317
  -5.500   0.0271   0.00871   0.00348  -0.1488   0.8548   0.0334
  -5.250   0.0559   0.00847   0.00320  -0.1490   0.8444   0.0349
  -5.000   0.0843   0.00832   0.00297  -0.1491   0.8335   0.0363
  -4.750   0.1127   0.00820   0.00278  -0.1491   0.8223   0.0378
  -4.500   0.1415   0.00804   0.00257  -0.1492   0.8125   0.0390
  -4.250   0.1708   0.00780   0.00226  -0.1495   0.8041   0.0418
  -4.000   0.1999   0.00765   0.00210  -0.1497   0.7956   0.0445
  -3.750   0.2287   0.00756   0.00195  -0.1498   0.7876   0.0472
  -3.500   0.2581   0.00738   0.00178  -0.1501   0.7794   0.0545
  -3.250   0.2873   0.00724   0.00165  -0.1503   0.7716   0.0708
  -3.000   0.3166   0.00709   0.00157  -0.1506   0.7636   0.0916
  -2.750   0.3455   0.00701   0.00149  -0.1507   0.7557   0.1079
  -2.500   0.3749   0.00688   0.00140  -0.1510   0.7478   0.1293
  -2.250   0.4055   0.00649   0.00128  -0.1519   0.7403   0.2316
  -2.000   0.4357   0.00623   0.00126  -0.1525   0.7322   0.3208
  -1.750   0.4645   0.00619   0.00125  -0.1526   0.7244   0.3539
  -1.500   0.4937   0.00614   0.00124  -0.1528   0.7167   0.3786
  -1.250   0.5224   0.00613   0.00123  -0.1529   0.7088   0.4020
  -1.000   0.5517   0.00605   0.00124  -0.1532   0.7008   0.4342
  -0.750   0.5807   0.00598   0.00127  -0.1534   0.6929   0.4839
  -0.500   0.6098   0.00595   0.00131  -0.1535   0.6849   0.5208
  -0.250   0.6383   0.00599   0.00136  -0.1535   0.6767   0.5496
   0.000   0.6669   0.00601   0.00141  -0.1535   0.6682   0.5704
   0.250   0.6950   0.00608   0.00145  -0.1535   0.6576   0.5836
   0.500   0.7229   0.00616   0.00149  -0.1533   0.6445   0.5956
   0.750   0.7507   0.00625   0.00154  -0.1532   0.6313   0.6079
   1.000   0.7789   0.00630   0.00160  -0.1531   0.6196   0.6185
   1.250   0.8069   0.00638   0.00166  -0.1530   0.6087   0.6290
   1.500   0.8346   0.00648   0.00173  -0.1528   0.5972   0.6380
   1.750   0.8625   0.00656   0.00180  -0.1527   0.5850   0.6449
   2.000   0.8900   0.00668   0.00188  -0.1525   0.5686   0.6521
   2.250   0.9171   0.00683   0.00197  -0.1523   0.5492   0.6587
   2.500   0.9444   0.00696   0.00206  -0.1521   0.5309   0.6657
   2.750   0.9715   0.00713   0.00217  -0.1519   0.5116   0.6727
   3.000   0.9978   0.00734   0.00231  -0.1516   0.4884   0.6804
   3.250   1.0238   0.00761   0.00247  -0.1512   0.4599   0.6883
   3.500   1.0499   0.00786   0.00265  -0.1508   0.4358   0.6962
   3.750   1.0763   0.00810   0.00282  -0.1505   0.4152   0.7045
   4.000   1.1026   0.00833   0.00301  -0.1502   0.3968   0.7134
   4.250   1.1289   0.00857   0.00320  -0.1499   0.3782   0.7231
   4.500   1.1547   0.00885   0.00340  -0.1495   0.3526   0.7347
   4.750   1.1799   0.00918   0.00365  -0.1490   0.3237   0.7479
   5.000   1.2041   0.00961   0.00394  -0.1484   0.2882   0.7617
   5.250   1.2277   0.01009   0.00428  -0.1478   0.2517   0.7770
   5.500   1.2513   0.01057   0.00464  -0.1471   0.2207   0.7952
   5.750   1.2749   0.01099   0.00500  -0.1464   0.1961   0.8166
   6.000   1.2985   0.01134   0.00534  -0.1457   0.1756   0.8475
   6.250   1.3139   0.01149   0.00560  -0.1430   0.1558   1.0000
   6.500   1.3371   0.01205   0.00601  -0.1423   0.1295   1.0000
   6.750   1.3589   0.01273   0.00649  -0.1415   0.1000   1.0000
   7.000   1.3815   0.01330   0.00695  -0.1407   0.0827   1.0000
   7.250   1.4045   0.01382   0.00741  -0.1399   0.0712   1.0000
   7.500   1.4272   0.01435   0.00787  -0.1391   0.0602   1.0000
   7.750   1.4494   0.01489   0.00835  -0.1383   0.0502   1.0000
   8.000   1.4717   0.01541   0.00883  -0.1374   0.0441   1.0000
   8.250   1.4942   0.01588   0.00931  -0.1366   0.0406   1.0000
   8.500   1.5163   0.01636   0.00979  -0.1357   0.0382   1.0000
   8.750   1.5371   0.01695   0.01037  -0.1346   0.0356   1.0000
   9.000   1.5580   0.01748   0.01093  -0.1335   0.0341   1.0000
   9.250   1.5794   0.01793   0.01143  -0.1326   0.0331   1.0000
   9.500   1.5997   0.01844   0.01197  -0.1314   0.0319   1.0000
   9.750   1.6185   0.01903   0.01258  -0.1301   0.0306   1.0000
  10.000   1.6348   0.01978   0.01335  -0.1283   0.0291   1.0000
  10.250   1.6485   0.02051   0.01415  -0.1261   0.0280   1.0000
  10.500   1.6649   0.02097   0.01466  -0.1243   0.0273   1.0000
  10.750   1.6797   0.02154   0.01528  -0.1223   0.0264   1.0000
  11.000   1.6935   0.02218   0.01596  -0.1202   0.0255   1.0000
  11.250   1.7055   0.02296   0.01677  -0.1180   0.0246   1.0000
  11.500   1.7135   0.02403   0.01788  -0.1153   0.0235   1.0000
  11.750   1.7226   0.02506   0.01899  -0.1129   0.0226   1.0000
  12.000   1.7370   0.02576   0.01975  -0.1113   0.0219   1.0000
  12.250   1.7500   0.02660   0.02063  -0.1096   0.0211   1.0000
  12.500   1.7616   0.02755   0.02162  -0.1079   0.0201   1.0000
  12.750   1.7697   0.02882   0.02292  -0.1060   0.0192   1.0000
  13.000   1.7743   0.03046   0.02463  -0.1039   0.0183   1.0000
  13.250   1.7857   0.03158   0.02583  -0.1025   0.0177   1.0000
  13.500   1.7956   0.03287   0.02718  -0.1011   0.0169   1.0000
  13.750   1.8039   0.03436   0.02872  -0.0998   0.0162   1.0000
  14.000   1.8093   0.03618   0.03058  -0.0984   0.0154   1.0000
  14.250   1.8094   0.03861   0.03309  -0.0969   0.0147   1.0000
  14.500   1.8166   0.04041   0.03497  -0.0959   0.0142   1.0000
  14.750   1.8223   0.04241   0.03705  -0.0949   0.0137   1.0000
  15.000   1.8263   0.04466   0.03938  -0.0941   0.0132   1.0000
  15.250   1.8287   0.04718   0.04197  -0.0934   0.0127   1.0000
  15.500   1.8270   0.05029   0.04515  -0.0928   0.0122   1.0000
  15.750   1.8203   0.05415   0.04911  -0.0924   0.0117   1.0000
  16.000   1.8218   0.05710   0.05217  -0.0923   0.0114   1.0000
  16.250   1.8210   0.06046   0.05564  -0.0923   0.0112   1.0000
  16.500   1.8189   0.06412   0.05940  -0.0926   0.0109   1.0000
  16.750   1.8157   0.06804   0.06344  -0.0931   0.0106   1.0000
  17.000   1.8117   0.07223   0.06773  -0.0938   0.0104   1.0000
  17.250   1.8057   0.07688   0.07249  -0.0949   0.0102   1.0000
  17.500   1.7980   0.08196   0.07768  -0.0962   0.0099   1.0000
  17.750   1.7882   0.08752   0.08336  -0.0980   0.0097   1.0000
  18.000   1.7741   0.09406   0.09002  -0.1003   0.0095   1.0000
  18.250   1.7581   0.10114   0.09725  -0.1031   0.0094   1.0000
  18.500   1.7409   0.10861   0.10486  -0.1064   0.0092   1.0000
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