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FX 62-K-153/20 AIRFOIL (fx62k153-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX 62-K-153/20 AIRFOIL (fx62k153-il)
Reynolds number: 500,000
Max Cl/Cd: 124.82 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx62k153-il-500000.txt
Download as CSV file: xf-fx62k153-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 62-K-153/20 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.1677   0.10529   0.10255  -0.1086   0.9056   0.0161
 -11.750  -0.1719   0.09959   0.09684  -0.1107   0.8998   0.0163
 -11.500  -0.1679   0.09645   0.09366  -0.1117   0.8944   0.0166
 -11.250  -0.1628   0.09334   0.09050  -0.1130   0.8899   0.0168
 -11.000  -0.1583   0.09006   0.08722  -0.1146   0.8855   0.0171
 -10.750  -0.1548   0.08646   0.08362  -0.1164   0.8811   0.0173
 -10.500  -0.1524   0.08249   0.07962  -0.1187   0.8771   0.0176
 -10.250  -0.1516   0.07796   0.07508  -0.1215   0.8735   0.0179
 -10.000  -0.1533   0.07249   0.06963  -0.1254   0.8698   0.0181
  -9.750  -0.1648   0.06295   0.06007  -0.1342   0.8657   0.0179
  -9.500  -0.1831   0.05532   0.05229  -0.1411   0.8615   0.0178
  -9.250  -0.2573   0.03847   0.03475  -0.1489   0.8541   0.0125
  -9.000  -0.2482   0.03565   0.03177  -0.1501   0.8509   0.0111
  -8.750  -0.2655   0.02449   0.01941  -0.1509   0.8472   0.0095
  -8.500  -0.2447   0.02278   0.01747  -0.1513   0.8450   0.0098
  -8.250  -0.2231   0.02127   0.01575  -0.1514   0.8426   0.0102
  -8.000  -0.2003   0.01984   0.01408  -0.1513   0.8401   0.0110
  -7.750  -0.1751   0.01894   0.01293  -0.1514   0.8379   0.0119
  -7.500  -0.1528   0.01744   0.01135  -0.1513   0.8358   0.0132
  -7.250  -0.1260   0.01694   0.01079  -0.1517   0.8339   0.0148
  -7.000  -0.1001   0.01618   0.00987  -0.1519   0.8320   0.0166
  -6.750  -0.0739   0.01580   0.00953  -0.1524   0.8300   0.0187
  -6.500  -0.0469   0.01562   0.00930  -0.1527   0.8280   0.0209
  -6.250  -0.0223   0.01481   0.00847  -0.1528   0.8258   0.0233
  -6.000   0.0048   0.01443   0.00808  -0.1533   0.8237   0.0254
  -5.750   0.0326   0.01403   0.00764  -0.1538   0.8216   0.0274
  -5.500   0.0612   0.01362   0.00715  -0.1544   0.8198   0.0285
  -5.250   0.0909   0.01280   0.00626  -0.1558   0.8181   0.0312
  -5.000   0.1213   0.01248   0.00591  -0.1570   0.8163   0.0349
  -4.750   0.1504   0.01208   0.00549  -0.1578   0.8143   0.0407
  -4.500   0.1809   0.01162   0.00511  -0.1591   0.8122   0.0598
  -4.250   0.2135   0.01098   0.00475  -0.1612   0.8101   0.1334
  -4.000   0.2621   0.00911   0.00413  -0.1687   0.8084   0.4827
  -3.750   0.2955   0.00894   0.00422  -0.1702   0.8065   0.5785
  -3.500   0.3262   0.00905   0.00431  -0.1709   0.8046   0.6136
  -3.250   0.3560   0.00925   0.00447  -0.1712   0.8028   0.6336
  -3.000   0.3856   0.00944   0.00460  -0.1717   0.8009   0.6457
  -2.750   0.4125   0.00964   0.00481  -0.1714   0.7986   0.6561
  -2.500   0.4377   0.00999   0.00520  -0.1706   0.7961   0.6685
  -2.250   0.4631   0.01033   0.00555  -0.1697   0.7937   0.6789
  -2.000   0.4916   0.01042   0.00560  -0.1699   0.7916   0.6827
  -1.750   0.5226   0.01046   0.00557  -0.1708   0.7896   0.6869
  -1.500   0.5536   0.01050   0.00554  -0.1717   0.7877   0.6903
  -1.250   0.5808   0.01059   0.00563  -0.1716   0.7852   0.6925
  -1.000   0.6077   0.01064   0.00570  -0.1716   0.7822   0.6950
  -0.750   0.6361   0.01066   0.00572  -0.1719   0.7793   0.6978
  -0.500   0.6662   0.01067   0.00568  -0.1726   0.7768   0.7011
  -0.250   0.6984   0.01065   0.00559  -0.1738   0.7742   0.7045
   0.000   0.7274   0.01067   0.00560  -0.1741   0.7714   0.7062
   0.250   0.7533   0.01067   0.00565  -0.1739   0.7675   0.7082
   0.500   0.7811   0.01069   0.00569  -0.1740   0.7643   0.7105
   0.750   0.8105   0.01070   0.00569  -0.1745   0.7616   0.7130
   1.000   0.8413   0.01070   0.00567  -0.1753   0.7592   0.7158
   1.250   0.8725   0.01074   0.00568  -0.1763   0.7567   0.7188
   1.500   0.8991   0.01074   0.00574  -0.1764   0.7531   0.7207
   1.750   0.9266   0.01075   0.00580  -0.1765   0.7497   0.7223
   2.000   0.9554   0.01075   0.00582  -0.1768   0.7467   0.7243
   2.250   0.9856   0.01073   0.00578  -0.1775   0.7436   0.7264
   2.500   1.0118   0.01069   0.00582  -0.1773   0.7381   0.7288
   2.750   1.0407   0.01057   0.00570  -0.1776   0.7321   0.7312
   3.000   1.0713   0.01052   0.00562  -0.1784   0.7275   0.7338
   3.250   1.0969   0.01049   0.00568  -0.1781   0.7218   0.7357
   3.500   1.1246   0.01042   0.00564  -0.1782   0.7163   0.7373
   3.750   1.1508   0.01039   0.00567  -0.1780   0.7098   0.7391
   4.000   1.1772   0.01033   0.00565  -0.1778   0.7019   0.7412
   4.250   1.2027   0.01031   0.00568  -0.1775   0.6925   0.7436
   4.500   1.2284   0.01028   0.00567  -0.1772   0.6810   0.7461
   4.750   1.2534   0.01029   0.00567  -0.1767   0.6659   0.7483
   5.000   1.2775   0.01034   0.00574  -0.1761   0.6515   0.7502
   5.250   1.3007   0.01044   0.00587  -0.1753   0.6368   0.7520
   5.500   1.3231   0.01060   0.00603  -0.1744   0.6201   0.7540
   5.750   1.3430   0.01086   0.00623  -0.1730   0.5985   0.7560
   6.000   1.3587   0.01126   0.00652  -0.1707   0.5657   0.7582
   6.250   1.3708   0.01181   0.00692  -0.1679   0.5291   0.7605
   6.500   1.3790   0.01246   0.00740  -0.1643   0.4923   0.7630
   6.750   1.3813   0.01321   0.00798  -0.1597   0.4536   0.7651
   7.000   1.3835   0.01418   0.00877  -0.1553   0.4110   0.7670
   7.250   1.3827   0.01540   0.00975  -0.1507   0.3640   0.7690
   7.500   1.3812   0.01679   0.01090  -0.1463   0.3137   0.7712
   7.750   1.3802   0.01831   0.01218  -0.1423   0.2693   0.7734
   8.000   1.3820   0.01982   0.01347  -0.1390   0.2302   0.7758
   8.250   1.3869   0.02124   0.01472  -0.1363   0.1956   0.7781
   8.750   1.3947   0.02425   0.01743  -0.1308   0.1326   0.7817
   9.000   1.4010   0.02567   0.01874  -0.1285   0.1098   0.7836
   9.250   1.4073   0.02713   0.02010  -0.1263   0.0913   0.7856
   9.500   1.4163   0.02843   0.02138  -0.1244   0.0775   0.7879
   9.750   1.4255   0.02975   0.02266  -0.1227   0.0663   0.7902
  10.000   1.4361   0.03100   0.02390  -0.1212   0.0578   0.7924
  10.250   1.4459   0.03226   0.02519  -0.1196   0.0504   0.7943
  10.500   1.4539   0.03368   0.02660  -0.1178   0.0430   0.7962
  10.750   1.4641   0.03495   0.02791  -0.1163   0.0376   0.7982
  11.000   1.4727   0.03638   0.02936  -0.1147   0.0326   0.8004
  11.250   1.4822   0.03776   0.03078  -0.1133   0.0288   0.8028
  11.500   1.4902   0.03930   0.03235  -0.1118   0.0247   0.8052
  11.750   1.4967   0.04101   0.03405  -0.1102   0.0196   0.8074
  12.000   1.5020   0.04282   0.03589  -0.1086   0.0142   0.8095
  12.250   1.5052   0.04486   0.03796  -0.1068   0.0100   0.8115
  12.500   1.5096   0.04683   0.03998  -0.1052   0.0077   0.8137
  12.750   1.5133   0.04895   0.04217  -0.1036   0.0066   0.8160
  13.000   1.5191   0.05092   0.04424  -0.1024   0.0061   0.8184
  13.250   1.5238   0.05304   0.04645  -0.1011   0.0056   0.8210
  13.500   1.5271   0.05532   0.04883  -0.0999   0.0053   0.8234
  13.750   1.5268   0.05799   0.05162  -0.0984   0.0049   0.8259
  14.000   1.5270   0.06071   0.05447  -0.0972   0.0048   0.8285
  14.250   1.5286   0.06335   0.05725  -0.0962   0.0046   0.8313
  14.500   1.5289   0.06622   0.06024  -0.0953   0.0045   0.8341
  14.750   1.5284   0.06923   0.06338  -0.0945   0.0044   0.8368
  15.000   1.5269   0.07237   0.06666  -0.0938   0.0042   0.8395
  15.250   1.5246   0.07570   0.07013  -0.0932   0.0041   0.8424
  15.500   1.5218   0.07918   0.07374  -0.0927   0.0040   0.8457
  15.750   1.5180   0.08289   0.07758  -0.0925   0.0039   0.8492
  16.000   1.5129   0.08683   0.08166  -0.0924   0.0038   0.8526
  16.250   1.5072   0.09087   0.08584  -0.0925   0.0038   0.8565
  16.500   1.5002   0.09523   0.09034  -0.0927   0.0037   0.8608
  16.750   1.4938   0.09959   0.09484  -0.0933   0.0037   0.8655
  17.000   1.4860   0.10421   0.09961  -0.0940   0.0036   0.8707
  17.250   1.4771   0.10908   0.10463  -0.0949   0.0036   0.8768
  17.500   1.4692   0.11380   0.10950  -0.0960   0.0036   0.8846
  18.000   1.4478   0.12319   0.11924  -0.0975   0.0035   0.9363
  18.250   1.4382   0.12800   0.12419  -0.0990   0.0035   0.9999
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