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FX 63-110 AIRFOIL (fx63110-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 63-110 AIRFOIL (fx63110-il)
Reynolds number: 1,000,000
Max Cl/Cd: 117.17 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx63110-il-1000000-n5.txt
Download as CSV file: xf-fx63110-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.9134   0.04576   0.04319  -0.0819   1.0000   0.0071
 -13.750  -0.9653   0.03754   0.03478  -0.0857   1.0000   0.0069
 -13.500  -0.9493   0.03034   0.02732  -0.1001   0.9969   0.0070
 -13.250  -0.9183   0.02649   0.02325  -0.1098   0.9947   0.0073
 -13.000  -0.8917   0.02441   0.02102  -0.1137   0.9925   0.0074
 -12.750  -0.8628   0.02279   0.01926  -0.1169   0.9903   0.0076
 -12.500  -0.8322   0.02140   0.01775  -0.1198   0.9884   0.0078
 -12.250  -0.8001   0.02020   0.01643  -0.1225   0.9870   0.0081
 -12.000  -0.7671   0.01909   0.01520  -0.1251   0.9858   0.0083
 -11.750  -0.7409   0.01819   0.01419  -0.1260   0.9821   0.0086
 -11.500  -0.7103   0.01737   0.01326  -0.1275   0.9793   0.0088
 -11.250  -0.6781   0.01639   0.01219  -0.1296   0.9772   0.0092
 -11.000  -0.6490   0.01562   0.01136  -0.1307   0.9735   0.0097
 -10.750  -0.6208   0.01495   0.01063  -0.1314   0.9681   0.0101
 -10.500  -0.5901   0.01433   0.00994  -0.1326   0.9636   0.0106
 -10.250  -0.5609   0.01377   0.00930  -0.1333   0.9563   0.0111
 -10.000  -0.5262   0.01321   0.00866  -0.1351   0.9510   0.0115
  -9.750  -0.4885   0.01261   0.00801  -0.1377   0.9443   0.0123
  -9.500  -0.4465   0.01211   0.00746  -0.1410   0.9379   0.0133
  -9.250  -0.4050   0.01165   0.00693  -0.1442   0.9279   0.0142
  -9.000  -0.3666   0.01126   0.00644  -0.1466   0.9140   0.0150
  -8.750  -0.3340   0.01099   0.00610  -0.1478   0.8984   0.0163
  -8.500  -0.3046   0.01080   0.00583  -0.1482   0.8845   0.0174
  -8.250  -0.2760   0.01059   0.00553  -0.1484   0.8728   0.0183
  -7.750  -0.2194   0.01013   0.00493  -0.1488   0.8526   0.0200
  -7.500  -0.1912   0.00997   0.00473  -0.1489   0.8433   0.0210
  -7.250  -0.1630   0.00982   0.00454  -0.1490   0.8341   0.0221
  -7.000  -0.1346   0.00967   0.00433  -0.1491   0.8264   0.0230
  -6.750  -0.1061   0.00951   0.00410  -0.1492   0.8182   0.0236
  -6.500  -0.0777   0.00939   0.00392  -0.1493   0.8104   0.0240
  -6.250  -0.0486   0.00906   0.00355  -0.1497   0.8023   0.0256
  -6.000  -0.0199   0.00889   0.00333  -0.1499   0.7952   0.0266
  -5.750   0.0090   0.00874   0.00315  -0.1501   0.7876   0.0277
  -5.500   0.0376   0.00861   0.00296  -0.1502   0.7794   0.0287
  -5.250   0.0663   0.00849   0.00278  -0.1503   0.7693   0.0296
  -5.000   0.0948   0.00838   0.00261  -0.1504   0.7583   0.0303
  -4.750   0.1233   0.00830   0.00245  -0.1505   0.7469   0.0307
  -4.500   0.1523   0.00815   0.00223  -0.1506   0.7365   0.0318
  -4.250   0.1815   0.00800   0.00204  -0.1509   0.7285   0.0339
  -4.000   0.2105   0.00790   0.00191  -0.1511   0.7205   0.0358
  -3.750   0.2396   0.00780   0.00178  -0.1513   0.7131   0.0376
  -3.500   0.2685   0.00773   0.00168  -0.1514   0.7052   0.0395
  -3.250   0.2976   0.00766   0.00158  -0.1515   0.6978   0.0436
  -3.000   0.3267   0.00758   0.00149  -0.1517   0.6902   0.0515
  -2.750   0.3558   0.00749   0.00143  -0.1520   0.6830   0.0653
  -2.500   0.3849   0.00741   0.00137  -0.1522   0.6750   0.0797
  -2.250   0.4139   0.00736   0.00132  -0.1523   0.6679   0.0920
  -2.000   0.4430   0.00731   0.00128  -0.1525   0.6604   0.1028
  -1.750   0.4719   0.00727   0.00124  -0.1527   0.6530   0.1157
  -1.500   0.5014   0.00716   0.00120  -0.1530   0.6450   0.1464
  -1.250   0.5324   0.00680   0.00115  -0.1540   0.6378   0.2693
  -1.000   0.5620   0.00668   0.00117  -0.1544   0.6299   0.3292
  -0.750   0.5910   0.00664   0.00119  -0.1546   0.6219   0.3658
  -0.500   0.6200   0.00663   0.00121  -0.1548   0.6136   0.3895
  -0.250   0.6486   0.00665   0.00124  -0.1549   0.6054   0.4050
   0.250   0.7057   0.00670   0.00131  -0.1550   0.5818   0.4448
   0.500   0.7335   0.00678   0.00137  -0.1550   0.5618   0.4706
   0.750   0.7614   0.00686   0.00146  -0.1550   0.5392   0.5111
   1.000   0.7889   0.00699   0.00156  -0.1548   0.5171   0.5410
   1.250   0.8165   0.00713   0.00165  -0.1547   0.4998   0.5598
   1.500   0.8438   0.00729   0.00176  -0.1546   0.4800   0.5745
   1.750   0.8704   0.00752   0.00189  -0.1543   0.4546   0.5833
   2.000   0.8974   0.00772   0.00201  -0.1541   0.4360   0.5903
   2.250   0.9243   0.00792   0.00214  -0.1538   0.4159   0.5974
   2.500   0.9509   0.00816   0.00230  -0.1536   0.3940   0.6034
   2.750   0.9779   0.00835   0.00244  -0.1534   0.3773   0.6105
   3.250   1.0311   0.00880   0.00276  -0.1529   0.3384   0.6232
   3.500   1.0575   0.00905   0.00293  -0.1526   0.3184   0.6292
   3.750   1.0831   0.00937   0.00314  -0.1522   0.2918   0.6347
   4.000   1.1065   0.00993   0.00348  -0.1515   0.2449   0.6408
   4.250   1.1303   0.01045   0.00381  -0.1509   0.2086   0.6476
   4.500   1.1554   0.01080   0.00409  -0.1504   0.1869   0.6562
   5.000   1.2064   0.01142   0.00462  -0.1497   0.1564   0.6747
   5.250   1.2314   0.01177   0.00491  -0.1492   0.1390   0.6843
   5.500   1.2554   0.01222   0.00526  -0.1486   0.1170   0.6956
   5.750   1.2789   0.01272   0.00566  -0.1479   0.0944   0.7074
   6.000   1.3031   0.01311   0.00602  -0.1474   0.0820   0.7201
   6.250   1.3281   0.01342   0.00635  -0.1469   0.0753   0.7357
   6.500   1.3527   0.01375   0.00670  -0.1464   0.0689   0.7540
   6.750   1.3773   0.01406   0.00705  -0.1459   0.0630   0.7742
   7.000   1.4012   0.01442   0.00743  -0.1453   0.0560   0.7946
   7.250   1.4244   0.01482   0.00784  -0.1445   0.0484   0.8158
   7.500   1.4474   0.01516   0.00824  -0.1438   0.0431   0.8447
   7.750   1.4627   0.01533   0.00857  -0.1412   0.0392   1.0000
   8.000   1.4861   0.01571   0.00897  -0.1406   0.0374   1.0000
   8.250   1.5090   0.01613   0.00938  -0.1398   0.0358   1.0000
   8.500   1.5310   0.01660   0.00986  -0.1389   0.0338   1.0000
   8.750   1.5528   0.01707   0.01034  -0.1380   0.0318   1.0000
   9.000   1.5748   0.01748   0.01078  -0.1372   0.0307   1.0000
   9.250   1.5960   0.01794   0.01126  -0.1362   0.0297   1.0000
   9.500   1.6163   0.01844   0.01178  -0.1350   0.0286   1.0000
   9.750   1.6354   0.01899   0.01235  -0.1337   0.0275   1.0000
  10.000   1.6533   0.01958   0.01298  -0.1322   0.0263   1.0000
  10.250   1.6704   0.02008   0.01351  -0.1305   0.0258   1.0000
  10.500   1.6865   0.02056   0.01405  -0.1287   0.0252   1.0000
  10.750   1.7016   0.02110   0.01463  -0.1267   0.0244   1.0000
  11.000   1.7159   0.02171   0.01528  -0.1247   0.0235   1.0000
  11.250   1.7292   0.02240   0.01601  -0.1227   0.0225   1.0000
  11.500   1.7413   0.02319   0.01683  -0.1205   0.0215   1.0000
  11.750   1.7538   0.02398   0.01767  -0.1185   0.0206   1.0000
  12.000   1.7665   0.02478   0.01852  -0.1166   0.0196   1.0000
  12.250   1.7779   0.02570   0.01948  -0.1147   0.0181   1.0000
  12.500   1.7877   0.02678   0.02057  -0.1127   0.0167   1.0000
  12.750   1.7976   0.02789   0.02174  -0.1109   0.0155   1.0000
  13.000   1.8061   0.02917   0.02306  -0.1091   0.0140   1.0000
  13.250   1.8134   0.03060   0.02452  -0.1073   0.0127   1.0000
  13.500   1.8205   0.03211   0.02610  -0.1056   0.0116   1.0000
  13.750   1.8259   0.03385   0.02789  -0.1040   0.0107   1.0000
  14.000   1.8311   0.03567   0.02977  -0.1025   0.0099   1.0000
  14.250   1.8362   0.03756   0.03174  -0.1012   0.0093   1.0000
  14.500   1.8400   0.03967   0.03392  -0.0999   0.0087   1.0000
  14.750   1.8422   0.04201   0.03633  -0.0988   0.0081   1.0000
  15.000   1.8440   0.04449   0.03890  -0.0978   0.0077   1.0000
  15.250   1.8466   0.04697   0.04146  -0.0970   0.0074   1.0000
  15.500   1.8481   0.04966   0.04424  -0.0964   0.0071   1.0000
  15.750   1.8484   0.05259   0.04727  -0.0959   0.0068   1.0000
  16.000   1.8478   0.05574   0.05051  -0.0956   0.0065   1.0000
  16.250   1.8459   0.05918   0.05404  -0.0956   0.0063   1.0000
  16.500   1.8429   0.06290   0.05786  -0.0957   0.0061   1.0000
  16.750   1.8384   0.06695   0.06202  -0.0961   0.0059   1.0000
  17.000   1.8338   0.07116   0.06634  -0.0967   0.0057   1.0000
  17.250   1.8302   0.07536   0.07067  -0.0975   0.0056   1.0000
  17.500   1.8248   0.07994   0.07537  -0.0985   0.0055   1.0000
  17.750   1.8183   0.08483   0.08038  -0.0999   0.0054   1.0000
  18.000   1.8111   0.08998   0.08564  -0.1014   0.0053   1.0000
  18.250   1.8025   0.09552   0.09131  -0.1033   0.0052   1.0000
  18.500   1.7928   0.10134   0.09726  -0.1055   0.0051   1.0000
  18.750   1.7818   0.10751   0.10356  -0.1080   0.0050   1.0000
  19.000   1.7706   0.11384   0.11001  -0.1108   0.0049   1.0000
  19.250   1.7582   0.12049   0.11679  -0.1139   0.0048   1.0000
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