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FX 63-120 AIRFOIL (fx63120-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 63-120 AIRFOIL (fx63120-il)
Reynolds number: 500,000
Max Cl/Cd: 114.73 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx63120-il-500000-n5.txt
Download as CSV file: xf-fx63120-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 63-120 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.3379   0.12513   0.12268  -0.0400   1.0000   0.0101
 -11.250  -0.5855   0.03797   0.03502  -0.1095   0.9707   0.0130
 -11.000  -0.5709   0.03185   0.02864  -0.1214   0.9562   0.0131
 -10.750  -0.5438   0.02937   0.02603  -0.1276   0.9461   0.0134
 -10.500  -0.5116   0.02729   0.02377  -0.1329   0.9402   0.0137
 -10.250  -0.4803   0.02530   0.02158  -0.1373   0.9327   0.0142
 -10.000  -0.4435   0.02270   0.01862  -0.1431   0.9278   0.0150
  -9.750  -0.4042   0.02033   0.01584  -0.1484   0.9232   0.0158
  -9.500  -0.3630   0.01970   0.01517  -0.1522   0.9185   0.0163
  -9.250  -0.3209   0.01918   0.01458  -0.1559   0.9135   0.0168
  -9.000  -0.2805   0.01844   0.01369  -0.1595   0.9071   0.0176
  -8.750  -0.2430   0.01741   0.01243  -0.1625   0.8991   0.0185
  -8.500  -0.2078   0.01643   0.01118  -0.1649   0.8907   0.0193
  -8.250  -0.1757   0.01577   0.01041  -0.1665   0.8812   0.0199
  -8.000  -0.1450   0.01542   0.00999  -0.1675   0.8724   0.0205
  -7.750  -0.1151   0.01505   0.00953  -0.1683   0.8638   0.0213
  -7.500  -0.0858   0.01457   0.00891  -0.1689   0.8559   0.0221
  -7.250  -0.0567   0.01407   0.00826  -0.1695   0.8475   0.0229
  -7.000  -0.0276   0.01372   0.00777  -0.1699   0.8400   0.0236
  -6.750   0.0011   0.01309   0.00709  -0.1706   0.8325   0.0244
  -6.500   0.0302   0.01273   0.00667  -0.1711   0.8256   0.0252
  -6.250   0.0591   0.01236   0.00623  -0.1715   0.8181   0.0259
  -6.000   0.0884   0.01204   0.00583  -0.1719   0.8111   0.0268
  -5.750   0.1175   0.01173   0.00545  -0.1723   0.8043   0.0278
  -5.500   0.1468   0.01145   0.00508  -0.1727   0.7974   0.0284
  -5.250   0.1768   0.01106   0.00462  -0.1734   0.7909   0.0291
  -5.000   0.2069   0.01068   0.00421  -0.1740   0.7839   0.0301
  -4.750   0.2367   0.01045   0.00391  -0.1745   0.7772   0.0312
  -4.500   0.2661   0.01023   0.00365  -0.1749   0.7684   0.0323
  -4.250   0.2955   0.01005   0.00339  -0.1753   0.7592   0.0333
  -4.000   0.3248   0.00989   0.00315  -0.1756   0.7496   0.0342
  -3.750   0.3546   0.00972   0.00292  -0.1760   0.7425   0.0353
  -3.500   0.3845   0.00955   0.00272  -0.1764   0.7355   0.0373
  -3.250   0.4140   0.00945   0.00257  -0.1767   0.7290   0.0399
  -3.000   0.4437   0.00933   0.00243  -0.1771   0.7222   0.0433
  -2.750   0.4732   0.00922   0.00232  -0.1774   0.7155   0.0520
  -2.500   0.5032   0.00909   0.00222  -0.1779   0.7092   0.0725
  -2.250   0.5335   0.00890   0.00213  -0.1785   0.7023   0.1078
  -2.000   0.5652   0.00857   0.00203  -0.1796   0.6960   0.2007
  -1.750   0.5974   0.00822   0.00201  -0.1809   0.6894   0.3216
  -1.500   0.6264   0.00821   0.00205  -0.1811   0.6826   0.3667
  -1.250   0.6553   0.00822   0.00206  -0.1812   0.6759   0.3885
  -1.000   0.6841   0.00825   0.00208  -0.1813   0.6688   0.4043
  -0.750   0.7128   0.00827   0.00210  -0.1814   0.6624   0.4209
  -0.500   0.7416   0.00828   0.00214  -0.1815   0.6549   0.4401
   0.000   0.7989   0.00832   0.00223  -0.1817   0.6402   0.4725
   0.250   0.8270   0.00839   0.00228  -0.1817   0.6324   0.4823
   0.750   0.8834   0.00852   0.00241  -0.1817   0.6157   0.5050
   1.000   0.9115   0.00858   0.00249  -0.1817   0.6052   0.5202
   1.250   0.9388   0.00868   0.00258  -0.1815   0.5914   0.5376
   1.500   0.9657   0.00882   0.00268  -0.1812   0.5751   0.5543
   1.750   0.9927   0.00895   0.00279  -0.1810   0.5608   0.5694
   2.000   1.0197   0.00909   0.00292  -0.1808   0.5479   0.5834
   2.250   1.0464   0.00925   0.00305  -0.1805   0.5342   0.5963
   2.500   1.0729   0.00942   0.00319  -0.1802   0.5195   0.6086
   2.750   1.0994   0.00960   0.00335  -0.1799   0.5046   0.6199
   3.000   1.1255   0.00981   0.00352  -0.1795   0.4886   0.6305
   3.250   1.1509   0.01006   0.00371  -0.1790   0.4706   0.6413
   3.500   1.1764   0.01031   0.00393  -0.1786   0.4532   0.6519
   3.750   1.2017   0.01058   0.00416  -0.1781   0.4369   0.6622
   4.000   1.2269   0.01085   0.00439  -0.1776   0.4213   0.6726
   4.250   1.2519   0.01113   0.00465  -0.1771   0.4056   0.6820
   4.500   1.2766   0.01144   0.00491  -0.1765   0.3876   0.6918
   4.750   1.3008   0.01177   0.00519  -0.1759   0.3666   0.7014
   5.000   1.3245   0.01215   0.00549  -0.1752   0.3450   0.7110
   5.250   1.3480   0.01253   0.00582  -0.1745   0.3239   0.7213
   5.500   1.3707   0.01296   0.00618  -0.1736   0.2996   0.7314
   5.750   1.3921   0.01349   0.00659  -0.1726   0.2720   0.7423
   6.000   1.4130   0.01405   0.00706  -0.1715   0.2464   0.7556
   6.250   1.4345   0.01454   0.00750  -0.1705   0.2267   0.7704
   6.500   1.4556   0.01505   0.00796  -0.1694   0.2088   0.7868
   6.750   1.4759   0.01557   0.00845  -0.1682   0.1911   0.8061
   7.000   1.4955   0.01607   0.00896  -0.1668   0.1747   0.8295
   7.250   1.5127   0.01654   0.00945  -0.1650   0.1590   0.8696
   7.750   1.5425   0.01756   0.01042  -0.1604   0.1288   1.0000
   8.000   1.5585   0.01824   0.01104  -0.1585   0.1138   1.0000
   8.250   1.5731   0.01894   0.01168  -0.1564   0.1017   1.0000
   8.750   1.6024   0.02031   0.01302  -0.1523   0.0860   1.0000
   9.000   1.6157   0.02109   0.01380  -0.1502   0.0797   1.0000
   9.250   1.6305   0.02178   0.01453  -0.1483   0.0751   1.0000
   9.500   1.6433   0.02262   0.01537  -0.1462   0.0702   1.0000
   9.750   1.6563   0.02346   0.01625  -0.1442   0.0663   1.0000
  10.000   1.6695   0.02431   0.01714  -0.1423   0.0619   1.0000
  10.250   1.6794   0.02542   0.01825  -0.1401   0.0566   1.0000
  10.500   1.6914   0.02641   0.01928  -0.1383   0.0520   1.0000
  10.750   1.7005   0.02765   0.02052  -0.1362   0.0475   1.0000
  11.000   1.7113   0.02881   0.02172  -0.1345   0.0446   1.0000
  11.250   1.7211   0.03008   0.02304  -0.1327   0.0421   1.0000
  11.500   1.7292   0.03155   0.02454  -0.1309   0.0395   1.0000
  11.750   1.7385   0.03296   0.02602  -0.1294   0.0378   1.0000
  12.000   1.7471   0.03447   0.02760  -0.1278   0.0362   1.0000
  12.250   1.7544   0.03615   0.02934  -0.1263   0.0345   1.0000
  12.500   1.7603   0.03804   0.03128  -0.1249   0.0329   1.0000
  12.750   1.7670   0.03989   0.03321  -0.1236   0.0316   1.0000
  13.000   1.7740   0.04176   0.03518  -0.1224   0.0305   1.0000
  13.250   1.7796   0.04383   0.03733  -0.1213   0.0292   1.0000
  13.500   1.7837   0.04612   0.03970  -0.1203   0.0278   1.0000
  13.750   1.7859   0.04871   0.04235  -0.1193   0.0265   1.0000
  14.000   1.7917   0.05094   0.04469  -0.1185   0.0254   1.0000
  14.250   1.7958   0.05345   0.04729  -0.1179   0.0239   1.0000
  14.500   1.7979   0.05626   0.05018  -0.1173   0.0225   1.0000
  14.750   1.7995   0.05922   0.05323  -0.1169   0.0212   1.0000
  15.000   1.8016   0.06219   0.05630  -0.1166   0.0196   1.0000
  15.250   1.8018   0.06549   0.05968  -0.1164   0.0182   1.0000
  15.500   1.8011   0.06902   0.06330  -0.1164   0.0169   1.0000
  15.750   1.7997   0.07275   0.06712  -0.1166   0.0156   1.0000
  16.000   1.7966   0.07680   0.07125  -0.1170   0.0145   1.0000
  16.250   1.7928   0.08108   0.07563  -0.1175   0.0135   1.0000
  16.500   1.7890   0.08545   0.08012  -0.1183   0.0128   1.0000
  16.750   1.7838   0.09015   0.08492  -0.1192   0.0120   1.0000
  17.000   1.7771   0.09521   0.09009  -0.1205   0.0114   1.0000
  17.250   1.7700   0.10040   0.09539  -0.1219   0.0109   1.0000
  17.500   1.7639   0.10553   0.10066  -0.1235   0.0105   1.0000
  17.750   1.7569   0.11088   0.10615  -0.1253   0.0100   1.0000
  18.000   1.7500   0.11629   0.11169  -0.1274   0.0098   1.0000
  18.250   1.7416   0.12204   0.11757  -0.1297   0.0095   1.0000
  18.500   1.7328   0.12790   0.12355  -0.1322   0.0092   1.0000
  18.750   1.7237   0.13389   0.12966  -0.1350   0.0089   1.0000
  19.000   1.7140   0.14005   0.13594  -0.1381   0.0087   1.0000
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