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WORTMANN FX 79-K-144/17 AIRFOIL (fx79k144-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 79-K-144/17 AIRFOIL (fx79k144-il)
Reynolds number: 200,000
Max Cl/Cd: 64.99 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx79k144-il-200000-n5.txt
Download as CSV file: xf-fx79k144-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 79-K-144/17 AIRFOIL                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.6074   0.06342   0.05919  -0.0713   0.8249   0.0141
 -11.500  -0.6330   0.05620   0.05175  -0.0763   0.8241   0.0140
 -11.250  -0.6589   0.05041   0.04566  -0.0780   0.8234   0.0140
 -11.000  -0.6817   0.04537   0.04023  -0.0775   0.8227   0.0141
 -10.750  -0.6845   0.04300   0.03769  -0.0765   0.8220   0.0142
 -10.500  -0.6816   0.04151   0.03606  -0.0751   0.8214   0.0145
 -10.250  -0.6724   0.04015   0.03456  -0.0743   0.8208   0.0149
 -10.000  -0.6627   0.03862   0.03283  -0.0734   0.8200   0.0154
  -9.750  -0.6536   0.03663   0.03053  -0.0723   0.8190   0.0162
  -9.500  -0.6444   0.03394   0.02738  -0.0711   0.8177   0.0173
  -9.250  -0.6316   0.03142   0.02436  -0.0699   0.8163   0.0183
  -9.000  -0.6128   0.03020   0.02307  -0.0696   0.8148   0.0190
  -8.750  -0.5926   0.02916   0.02188  -0.0692   0.8134   0.0200
  -8.500  -0.5719   0.02791   0.02037  -0.0687   0.8122   0.0215
  -8.250  -0.5498   0.02669   0.01881  -0.0682   0.8109   0.0230
  -8.000  -0.5279   0.02572   0.01781  -0.0679   0.8098   0.0242
  -7.750  -0.5046   0.02510   0.01710  -0.0677   0.8085   0.0256
  -7.500  -0.4808   0.02457   0.01641  -0.0674   0.8073   0.0275
  -7.250  -0.4568   0.02398   0.01564  -0.0672   0.8063   0.0296
  -7.000  -0.4322   0.02353   0.01522  -0.0674   0.8051   0.0318
  -6.750  -0.4069   0.02306   0.01468  -0.0674   0.8038   0.0339
  -6.500  -0.3815   0.02248   0.01398  -0.0674   0.8024   0.0354
  -6.250  -0.3562   0.02192   0.01332  -0.0673   0.8010   0.0364
  -6.000  -0.3326   0.02111   0.01251  -0.0670   0.7995   0.0375
  -5.750  -0.3084   0.02055   0.01192  -0.0668   0.7980   0.0386
  -5.500  -0.2840   0.02009   0.01142  -0.0665   0.7964   0.0399
  -5.250  -0.2594   0.01969   0.01094  -0.0662   0.7949   0.0414
  -5.000  -0.2346   0.01934   0.01052  -0.0660   0.7935   0.0433
  -4.750  -0.2094   0.01904   0.01015  -0.0658   0.7923   0.0455
  -4.500  -0.1844   0.01865   0.00979  -0.0658   0.7901   0.0499
  -4.250  -0.1589   0.01836   0.00950  -0.0658   0.7879   0.0572
  -4.000  -0.1339   0.01800   0.00924  -0.0658   0.7855   0.0733
  -3.750  -0.1090   0.01763   0.00898  -0.0656   0.7831   0.1024
  -3.500  -0.0839   0.01727   0.00874  -0.0654   0.7809   0.1405
  -3.250  -0.0587   0.01691   0.00853  -0.0652   0.7791   0.1858
  -3.000  -0.0343   0.01652   0.00839  -0.0653   0.7754   0.2453
  -2.750  -0.0117   0.01578   0.00818  -0.0652   0.7719   0.3662
  -2.500   0.0038   0.01458   0.00823  -0.0632   0.7692   0.6444
  -2.000   0.0457   0.01531   0.00929  -0.0582   0.7654   0.7903
  -1.750   0.0722   0.01553   0.00941  -0.0579   0.7635   0.8089
  -1.500   0.0963   0.01585   0.00971  -0.0573   0.7590   0.8256
  -1.250   0.1197   0.01608   0.00990  -0.0560   0.7558   0.8362
  -1.000   0.1428   0.01625   0.01002  -0.0545   0.7533   0.8477
  -0.750   0.1664   0.01636   0.01008  -0.0531   0.7514   0.8591
  -0.250   0.2124   0.01662   0.01031  -0.0511   0.7438   0.8742
   0.000   0.2351   0.01667   0.01034  -0.0497   0.7405   0.8813
   0.250   0.2614   0.01660   0.01022  -0.0494   0.7382   0.8878
   0.500   0.2883   0.01646   0.01004  -0.0491   0.7365   0.8903
   0.750   0.3123   0.01656   0.01016  -0.0489   0.7306   0.8929
   1.000   0.3392   0.01646   0.01005  -0.0489   0.7265   0.8953
   1.250   0.3678   0.01622   0.00977  -0.0491   0.7237   0.8976
   1.750   0.4214   0.01608   0.00965  -0.0495   0.7133   0.9029
   2.000   0.4485   0.01589   0.00946  -0.0493   0.7104   0.9048
   2.250   0.4765   0.01565   0.00923  -0.0493   0.7084   0.9068
   2.500   0.4998   0.01582   0.00945  -0.0491   0.7004   0.9093
   2.750   0.5278   0.01565   0.00931  -0.0493   0.6970   0.9112
   3.000   0.5569   0.01543   0.00911  -0.0496   0.6946   0.9130
   3.250   0.5816   0.01561   0.00935  -0.0497   0.6866   0.9153
   3.500   0.6108   0.01544   0.00921  -0.0502   0.6825   0.9171
   3.750   0.6356   0.01532   0.00916  -0.0497   0.6766   0.9193
   4.000   0.6610   0.01518   0.00908  -0.0493   0.6698   0.9219
   4.250   0.6895   0.01491   0.00884  -0.0493   0.6645   0.9237
   4.500   0.7173   0.01475   0.00873  -0.0495   0.6571   0.9253
   4.750   0.7483   0.01439   0.00839  -0.0499   0.6518   0.9264
   5.000   0.7773   0.01420   0.00824  -0.0502   0.6431   0.9274
   5.250   0.8079   0.01391   0.00794  -0.0505   0.6331   0.9283
   5.500   0.8374   0.01371   0.00771  -0.0508   0.6196   0.9293
   5.750   0.8635   0.01373   0.00771  -0.0506   0.6001   0.9308
   6.000   0.8884   0.01383   0.00776  -0.0502   0.5756   0.9320
   6.250   0.9099   0.01400   0.00786  -0.0493   0.5433   0.9332
   6.500   0.9290   0.01432   0.00802  -0.0480   0.5075   0.9346
   6.750   0.9453   0.01479   0.00835  -0.0464   0.4677   0.9363
   7.000   0.9547   0.01556   0.00884  -0.0439   0.4118   0.9387
   7.250   0.9579   0.01661   0.00959  -0.0408   0.3516   0.9416
   7.500   0.9565   0.01807   0.01071  -0.0376   0.2856   0.9456
   7.750   0.9539   0.01997   0.01219  -0.0350   0.2097   0.9492
   8.000   0.9592   0.02148   0.01347  -0.0332   0.1633   0.9523
   8.250   0.9660   0.02293   0.01469  -0.0317   0.1203   0.9555
   8.500   0.9751   0.02425   0.01587  -0.0304   0.0899   0.9586
   8.750   0.9848   0.02548   0.01700  -0.0291   0.0668   0.9619
   9.000   0.9958   0.02664   0.01812  -0.0279   0.0521   0.9657
   9.250   1.0083   0.02775   0.01924  -0.0269   0.0442   0.9701
   9.500   1.0203   0.02892   0.02042  -0.0260   0.0388   0.9752
   9.750   1.0334   0.03001   0.02156  -0.0253   0.0337   0.9823
  10.000   1.0440   0.03114   0.02274  -0.0243   0.0300   1.0000
  10.250   1.0579   0.03238   0.02408  -0.0239   0.0270   1.0000
  10.500   1.0686   0.03388   0.02562  -0.0232   0.0245   1.0000
  10.750   1.0811   0.03526   0.02711  -0.0227   0.0221   1.0000
  11.000   1.0912   0.03685   0.02877  -0.0221   0.0202   1.0000
  11.250   1.0990   0.03864   0.03063  -0.0213   0.0187   1.0000
  11.500   1.1081   0.04034   0.03246  -0.0206   0.0175   1.0000
  11.750   1.1166   0.04212   0.03433  -0.0199   0.0164   1.0000
  12.000   1.1245   0.04396   0.03626  -0.0193   0.0157   1.0000
  12.250   1.1315   0.04593   0.03830  -0.0186   0.0151   1.0000
  12.500   1.1377   0.04801   0.04046  -0.0180   0.0146   1.0000
  12.750   1.1457   0.04999   0.04257  -0.0174   0.0141   1.0000
  13.000   1.1537   0.05197   0.04467  -0.0169   0.0136   1.0000
  13.250   1.1619   0.05398   0.04679  -0.0165   0.0130   1.0000
  13.500   1.1698   0.05605   0.04896  -0.0162   0.0125   1.0000
  13.750   1.1772   0.05820   0.05122  -0.0161   0.0120   1.0000
  14.000   1.1836   0.06049   0.05360  -0.0160   0.0117   1.0000
  14.250   1.1885   0.06294   0.05613  -0.0158   0.0115   1.0000
  14.500   1.1933   0.06545   0.05876  -0.0155   0.0113   1.0000
  14.750   1.1978   0.06803   0.06150  -0.0152   0.0111   1.0000
  15.000   1.2014   0.07076   0.06439  -0.0149   0.0109   1.0000
  15.250   1.2038   0.07369   0.06750  -0.0148   0.0107   1.0000
  15.500   1.2048   0.07687   0.07086  -0.0148   0.0106   1.0000
  15.750   1.2043   0.08031   0.07449  -0.0149   0.0105   1.0000
  16.000   1.2020   0.08408   0.07846  -0.0154   0.0104   1.0000
  16.250   1.1978   0.08822   0.08282  -0.0161   0.0103   1.0000
  16.500   1.1917   0.09273   0.08754  -0.0171   0.0102   1.0000
  16.750   1.1836   0.09769   0.09272  -0.0185   0.0101   1.0000
  17.000   1.1737   0.10312   0.09837  -0.0204   0.0101   1.0000
  17.250   1.1617   0.10911   0.10458  -0.0228   0.0100   1.0000
  17.500   1.1479   0.11567   0.11137  -0.0258   0.0100   1.0000
  17.750   1.1319   0.12297   0.11889  -0.0295   0.0100   1.0000
  18.000   1.1133   0.13128   0.12743  -0.0341   0.0100   1.0000
  18.250   1.0916   0.14090   0.13729  -0.0399   0.0101   1.0000
  18.500   1.0644   0.15279   0.14942  -0.0475   0.0102   1.0000
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