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FX 63-110 AIRFOIL (fx63110-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 63-110 AIRFOIL (fx63110-il)
Reynolds number: 500,000
Max Cl/Cd: 105.8 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx63110-il-500000-n5.txt
Download as CSV file: xf-fx63110-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.7626   0.04609   0.04333  -0.0745   1.0000   0.0108
 -11.750  -0.7759   0.03425   0.03110  -0.0929   0.9952   0.0108
 -11.500  -0.7467   0.02882   0.02525  -0.1051   0.9902   0.0110
 -11.250  -0.7158   0.02592   0.02204  -0.1109   0.9870   0.0114
 -11.000  -0.6858   0.02375   0.01965  -0.1148   0.9835   0.0118
 -10.750  -0.6554   0.02239   0.01817  -0.1174   0.9796   0.0123
 -10.500  -0.6223   0.02131   0.01697  -0.1200   0.9769   0.0127
 -10.250  -0.5935   0.02031   0.01584  -0.1215   0.9718   0.0133
 -10.000  -0.5623   0.01926   0.01464  -0.1233   0.9673   0.0139
  -9.750  -0.5324   0.01830   0.01352  -0.1247   0.9618   0.0146
  -9.500  -0.5023   0.01748   0.01260  -0.1260   0.9554   0.0154
  -9.250  -0.4711   0.01697   0.01206  -0.1272   0.9495   0.0161
  -9.000  -0.4384   0.01644   0.01146  -0.1287   0.9434   0.0170
  -8.750  -0.4021   0.01576   0.01065  -0.1309   0.9392   0.0180
  -8.500  -0.3659   0.01510   0.00984  -0.1331   0.9329   0.0189
  -8.250  -0.3266   0.01452   0.00923  -0.1359   0.9277   0.0201
  -8.000  -0.2879   0.01418   0.00884  -0.1384   0.9216   0.0212
  -7.750  -0.2494   0.01375   0.00832  -0.1409   0.9138   0.0226
  -7.500  -0.2126   0.01331   0.00774  -0.1430   0.9047   0.0237
  -7.250  -0.1779   0.01272   0.00704  -0.1447   0.8948   0.0249
  -7.000  -0.1467   0.01239   0.00666  -0.1457   0.8844   0.0261
  -6.750  -0.1161   0.01214   0.00633  -0.1463   0.8747   0.0273
  -6.500  -0.0866   0.01185   0.00595  -0.1468   0.8646   0.0286
  -6.250  -0.0575   0.01160   0.00561  -0.1471   0.8555   0.0297
  -6.000  -0.0284   0.01138   0.00529  -0.1474   0.8468   0.0306
  -5.750   0.0008   0.01090   0.00473  -0.1479   0.8385   0.0320
  -5.500   0.0300   0.01057   0.00433  -0.1483   0.8301   0.0337
  -5.250   0.0591   0.01031   0.00402  -0.1486   0.8221   0.0350
  -5.000   0.0882   0.01010   0.00374  -0.1488   0.8144   0.0363
  -4.750   0.1172   0.00991   0.00348  -0.1491   0.8066   0.0378
  -4.500   0.1461   0.00975   0.00325  -0.1493   0.7978   0.0393
  -4.250   0.1748   0.00960   0.00302  -0.1494   0.7874   0.0403
  -4.000   0.2038   0.00939   0.00273  -0.1496   0.7763   0.0433
  -3.750   0.2327   0.00925   0.00253  -0.1497   0.7661   0.0475
  -3.500   0.2618   0.00912   0.00238  -0.1499   0.7576   0.0526
  -3.000   0.3200   0.00886   0.00214  -0.1504   0.7420   0.0774
  -2.500   0.3781   0.00867   0.00195  -0.1508   0.7266   0.1050
  -2.250   0.4070   0.00859   0.00186  -0.1510   0.7188   0.1211
  -2.000   0.4369   0.00837   0.00177  -0.1515   0.7112   0.1679
  -1.750   0.4677   0.00798   0.00172  -0.1525   0.7036   0.2957
  -1.500   0.4971   0.00787   0.00172  -0.1529   0.6957   0.3476
  -1.250   0.5261   0.00781   0.00173  -0.1531   0.6879   0.3892
  -1.000   0.5552   0.00775   0.00173  -0.1533   0.6803   0.4191
  -0.750   0.5839   0.00774   0.00174  -0.1534   0.6721   0.4410
  -0.500   0.6129   0.00771   0.00178  -0.1535   0.6640   0.4714
  -0.250   0.6414   0.00772   0.00184  -0.1536   0.6560   0.5033
   0.000   0.6700   0.00775   0.00190  -0.1536   0.6475   0.5311
   0.250   0.6981   0.00782   0.00197  -0.1536   0.6390   0.5548
   0.500   0.7264   0.00786   0.00204  -0.1535   0.6300   0.5740
   0.750   0.7543   0.00794   0.00211  -0.1534   0.6205   0.5901
   1.000   0.7818   0.00805   0.00218  -0.1532   0.6073   0.6021
   1.250   0.8090   0.00817   0.00225  -0.1529   0.5900   0.6108
   1.500   0.8360   0.00831   0.00232  -0.1527   0.5705   0.6187
   1.750   0.8630   0.00844   0.00242  -0.1524   0.5529   0.6272
   2.000   0.8903   0.00858   0.00252  -0.1522   0.5386   0.6353
   2.250   0.9172   0.00873   0.00264  -0.1519   0.5213   0.6433
   2.500   0.9432   0.00896   0.00278  -0.1515   0.4982   0.6504
   2.750   0.9694   0.00918   0.00293  -0.1511   0.4760   0.6578
   3.000   0.9956   0.00941   0.00310  -0.1508   0.4573   0.6653
   3.250   1.0212   0.00968   0.00330  -0.1503   0.4350   0.6735
   3.500   1.0466   0.00999   0.00352  -0.1499   0.4102   0.6820
   3.750   1.0719   0.01029   0.00375  -0.1494   0.3880   0.6906
   4.000   1.0980   0.01053   0.00397  -0.1491   0.3716   0.6996
   4.250   1.1235   0.01082   0.00421  -0.1487   0.3498   0.7112
   4.500   1.1476   0.01123   0.00451  -0.1480   0.3163   0.7236
   4.750   1.1711   0.01170   0.00485  -0.1474   0.2827   0.7362
   5.000   1.1939   0.01225   0.00524  -0.1466   0.2451   0.7494
   5.250   1.2168   0.01277   0.00565  -0.1458   0.2159   0.7637
   5.500   1.2398   0.01324   0.00605  -0.1450   0.1931   0.7807
   5.750   1.2629   0.01365   0.00645  -0.1442   0.1739   0.8026
   6.000   1.2854   0.01403   0.00684  -0.1433   0.1565   0.8298
   6.250   1.3052   0.01439   0.00722  -0.1418   0.1384   0.8724
   6.500   1.3210   0.01474   0.00757  -0.1395   0.1191   1.0000
   6.750   1.3428   0.01537   0.00807  -0.1386   0.0979   1.0000
   7.000   1.3649   0.01594   0.00858  -0.1378   0.0853   1.0000
   7.250   1.3875   0.01645   0.00906  -0.1370   0.0770   1.0000
   7.750   1.4313   0.01750   0.01009  -0.1353   0.0630   1.0000
   8.000   1.4523   0.01807   0.01064  -0.1343   0.0568   1.0000
   8.250   1.4732   0.01861   0.01119  -0.1332   0.0516   1.0000
   8.500   1.4930   0.01921   0.01178  -0.1321   0.0473   1.0000
   8.750   1.5128   0.01977   0.01239  -0.1309   0.0445   1.0000
   9.000   1.5312   0.02039   0.01302  -0.1295   0.0420   1.0000
   9.250   1.5471   0.02110   0.01374  -0.1277   0.0394   1.0000
   9.500   1.5631   0.02169   0.01439  -0.1258   0.0379   1.0000
   9.750   1.5776   0.02235   0.01509  -0.1239   0.0362   1.0000
  10.000   1.5908   0.02311   0.01589  -0.1217   0.0346   1.0000
  10.250   1.6024   0.02399   0.01680  -0.1195   0.0331   1.0000
  10.500   1.6135   0.02492   0.01780  -0.1173   0.0319   1.0000
  10.750   1.6266   0.02575   0.01870  -0.1154   0.0311   1.0000
  11.000   1.6387   0.02666   0.01970  -0.1135   0.0302   1.0000
  11.250   1.6498   0.02768   0.02079  -0.1117   0.0292   1.0000
  11.500   1.6597   0.02883   0.02201  -0.1098   0.0282   1.0000
  11.750   1.6681   0.03016   0.02340  -0.1079   0.0272   1.0000
  12.000   1.6740   0.03175   0.02506  -0.1060   0.0262   1.0000
  12.250   1.6845   0.03301   0.02641  -0.1046   0.0255   1.0000
  12.500   1.6946   0.03434   0.02784  -0.1033   0.0245   1.0000
  12.750   1.7036   0.03582   0.02941  -0.1020   0.0234   1.0000
  13.000   1.7113   0.03747   0.03113  -0.1008   0.0224   1.0000
  13.250   1.7174   0.03935   0.03307  -0.0996   0.0214   1.0000
  13.500   1.7232   0.04132   0.03513  -0.0985   0.0206   1.0000
  13.750   1.7301   0.04322   0.03714  -0.0976   0.0195   1.0000
  14.000   1.7359   0.04530   0.03930  -0.0968   0.0183   1.0000
  14.250   1.7403   0.04761   0.04169  -0.0961   0.0171   1.0000
  14.500   1.7433   0.05014   0.04430  -0.0955   0.0161   1.0000
  14.750   1.7456   0.05283   0.04709  -0.0950   0.0151   1.0000
  15.000   1.7469   0.05574   0.05009  -0.0947   0.0141   1.0000
  15.250   1.7466   0.05895   0.05337  -0.0946   0.0132   1.0000
  15.500   1.7457   0.06236   0.05690  -0.0946   0.0126   1.0000
  15.750   1.7435   0.06605   0.06071  -0.0949   0.0120   1.0000
  16.000   1.7405   0.07001   0.06477  -0.0954   0.0114   1.0000
  16.250   1.7362   0.07428   0.06916  -0.0961   0.0109   1.0000
  16.500   1.7304   0.07892   0.07391  -0.0972   0.0105   1.0000
  17.000   1.7164   0.08902   0.08428  -0.1000   0.0099   1.0000
  17.250   1.7092   0.09432   0.08972  -0.1018   0.0096   1.0000
  17.500   1.7007   0.09995   0.09550  -0.1038   0.0094   1.0000
  17.750   1.6914   0.10586   0.10155  -0.1062   0.0091   1.0000
  18.000   1.6815   0.11199   0.10782  -0.1088   0.0089   1.0000
  18.250   1.6705   0.11843   0.11439  -0.1118   0.0086   1.0000
  18.500   1.6588   0.12512   0.12122  -0.1151   0.0085   1.0000
  18.750   1.6463   0.13205   0.12829  -0.1187   0.0083   1.0000
  19.000   1.6338   0.13909   0.13546  -0.1226   0.0081   1.0000
  19.250   1.6203   0.14649   0.14300  -0.1269   0.0080   1.0000
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