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FX 73-CL3-152 (fx73cl3152-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 73-CL3-152 (fx73cl3152-il)
Reynolds number: 1,000,000
Max Cl/Cd: 128.61 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx73cl3152-il-1000000-n5.txt
Download as CSV file: xf-fx73cl3152-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 73-CL3-152                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.1697   0.05642   0.05333  -0.1431   0.8131   0.0206
 -11.500  -0.2365   0.04634   0.04310  -0.1490   0.8053   0.0207
 -11.250  -0.2903   0.03794   0.03457  -0.1554   0.7967   0.0206
 -11.000  -0.3106   0.02810   0.02447  -0.1687   0.7882   0.0208
 -10.750  -0.2929   0.02069   0.01673  -0.1811   0.7753   0.0209
 -10.500  -0.2676   0.01891   0.01472  -0.1838   0.7550   0.0211
 -10.250  -0.2449   0.01796   0.01350  -0.1845   0.7138   0.0214
 -10.000  -0.2224   0.01727   0.01254  -0.1847   0.6729   0.0215
  -9.750  -0.1983   0.01670   0.01174  -0.1849   0.6426   0.0217
  -9.500  -0.1733   0.01616   0.01101  -0.1850   0.6170   0.0218
  -9.250  -0.1479   0.01569   0.01036  -0.1851   0.5939   0.0219
  -9.000  -0.1225   0.01510   0.00961  -0.1853   0.5734   0.0222
  -8.750  -0.0963   0.01464   0.00903  -0.1853   0.5568   0.0225
  -8.500  -0.0698   0.01429   0.00856  -0.1853   0.5423   0.0228
  -8.250  -0.0432   0.01398   0.00814  -0.1852   0.5296   0.0230
  -8.000  -0.0161   0.01369   0.00776  -0.1851   0.5183   0.0233
  -7.750   0.0109   0.01342   0.00739  -0.1849   0.5082   0.0236
  -7.500   0.0381   0.01316   0.00704  -0.1848   0.4987   0.0240
  -7.250   0.0652   0.01293   0.00671  -0.1846   0.4903   0.0243
  -7.000   0.0926   0.01269   0.00640  -0.1844   0.4828   0.0246
  -6.750   0.1197   0.01251   0.00611  -0.1842   0.4747   0.0250
  -6.500   0.1473   0.01231   0.00584  -0.1840   0.4684   0.0252
  -6.250   0.1746   0.01208   0.00554  -0.1838   0.4617   0.0256
  -6.000   0.2017   0.01189   0.00528  -0.1835   0.4556   0.0262
  -5.750   0.2293   0.01172   0.00507  -0.1833   0.4514   0.0267
  -5.500   0.2570   0.01157   0.00488  -0.1831   0.4472   0.0272
  -5.250   0.2845   0.01145   0.00470  -0.1828   0.4429   0.0278
  -5.000   0.3119   0.01135   0.00454  -0.1825   0.4385   0.0284
  -4.750   0.3394   0.01126   0.00439  -0.1822   0.4347   0.0290
  -4.500   0.3670   0.01109   0.00420  -0.1820   0.4320   0.0297
  -4.250   0.3946   0.01098   0.00406  -0.1817   0.4289   0.0304
  -4.000   0.4221   0.01089   0.00393  -0.1814   0.4254   0.0312
  -3.750   0.4494   0.01083   0.00383  -0.1811   0.4218   0.0320
  -3.500   0.4765   0.01079   0.00373  -0.1807   0.4182   0.0328
  -3.250   0.5040   0.01070   0.00362  -0.1804   0.4159   0.0338
  -3.000   0.5316   0.01062   0.00353  -0.1801   0.4141   0.0350
  -2.750   0.5591   0.01057   0.00346  -0.1798   0.4120   0.0363
  -2.500   0.5865   0.01053   0.00339  -0.1795   0.4098   0.0377
  -2.250   0.6137   0.01047   0.00333  -0.1792   0.4075   0.0394
  -2.000   0.6407   0.01046   0.00329  -0.1788   0.4050   0.0411
  -1.750   0.6676   0.01045   0.00325  -0.1784   0.4024   0.0429
  -1.500   0.6942   0.01045   0.00323  -0.1779   0.3995   0.0455
  -1.250   0.7214   0.01042   0.00320  -0.1776   0.3979   0.0483
  -1.000   0.7486   0.01039   0.00318  -0.1772   0.3966   0.0518
  -0.750   0.7756   0.01037   0.00317  -0.1768   0.3951   0.0559
  -0.500   0.8025   0.01036   0.00316  -0.1765   0.3933   0.0618
  -0.250   0.8291   0.01034   0.00316  -0.1760   0.3912   0.0706
   0.000   0.8556   0.01034   0.00318  -0.1756   0.3890   0.0825
   0.250   0.8817   0.01034   0.00321  -0.1751   0.3869   0.0964
   0.500   0.9077   0.01037   0.00325  -0.1746   0.3844   0.1118
   0.750   0.9332   0.01041   0.00331  -0.1740   0.3816   0.1268
   1.000   0.9596   0.01042   0.00336  -0.1735   0.3801   0.1417
   1.250   0.9860   0.01044   0.00341  -0.1731   0.3788   0.1564
   1.500   1.0122   0.01046   0.00347  -0.1726   0.3770   0.1707
   1.750   1.0381   0.01050   0.00354  -0.1721   0.3752   0.1860
   2.000   1.0638   0.01055   0.00361  -0.1715   0.3733   0.2015
   2.250   1.0891   0.01060   0.00370  -0.1709   0.3714   0.2217
   2.500   1.1142   0.01066   0.00380  -0.1703   0.3696   0.2390
   2.750   1.1390   0.01075   0.00389  -0.1696   0.3677   0.2537
   3.000   1.1633   0.01084   0.00401  -0.1688   0.3655   0.2695
   3.250   1.1877   0.01093   0.00412  -0.1680   0.3636   0.2853
   3.500   1.2127   0.01099   0.00422  -0.1674   0.3623   0.3018
   3.750   1.2371   0.01104   0.00433  -0.1666   0.3609   0.3227
   4.000   1.2605   0.01111   0.00444  -0.1657   0.3592   0.3430
   4.250   1.2831   0.01118   0.00456  -0.1646   0.3575   0.3671
   4.500   1.3055   0.01126   0.00469  -0.1635   0.3557   0.3900
   4.750   1.3278   0.01136   0.00483  -0.1624   0.3538   0.4135
   5.000   1.3498   0.01149   0.00499  -0.1612   0.3518   0.4380
   5.250   1.3712   0.01162   0.00518  -0.1600   0.3498   0.4668
   5.500   1.3923   0.01178   0.00538  -0.1587   0.3476   0.4982
   5.750   1.4149   0.01187   0.00557  -0.1577   0.3464   0.5348
   6.000   1.4373   0.01198   0.00576  -0.1567   0.3448   0.5659
   6.250   1.4595   0.01210   0.00595  -0.1557   0.3429   0.5994
   6.500   1.4812   0.01223   0.00616  -0.1546   0.3407   0.6355
   6.750   1.5023   0.01238   0.00638  -0.1534   0.3381   0.6723
   7.000   1.5230   0.01254   0.00661  -0.1522   0.3359   0.7186
   7.500   1.6578   0.01289   0.00731  -0.1697   0.3300   1.0000
   7.750   1.6816   0.01309   0.00753  -0.1692   0.3281   1.0000
   8.000   1.7049   0.01332   0.00777  -0.1685   0.3258   1.0000
   8.250   1.7277   0.01357   0.00803  -0.1678   0.3232   1.0000
   8.500   1.7494   0.01387   0.00832  -0.1670   0.3202   1.0000
   8.750   1.7703   0.01421   0.00865  -0.1661   0.3171   1.0000
   9.000   1.7920   0.01451   0.00897  -0.1653   0.3147   1.0000
   9.250   1.8140   0.01479   0.00927  -0.1646   0.3126   1.0000
   9.500   1.8355   0.01510   0.00960  -0.1638   0.3102   1.0000
   9.750   1.8562   0.01545   0.00998  -0.1629   0.3073   1.0000
  10.000   1.8758   0.01586   0.01039  -0.1619   0.3045   1.0000
  10.250   1.8945   0.01632   0.01085  -0.1608   0.3015   1.0000
  10.500   1.9142   0.01672   0.01128  -0.1599   0.2990   1.0000
  10.750   1.9340   0.01712   0.01171  -0.1590   0.2959   1.0000
  11.000   1.9522   0.01762   0.01222  -0.1579   0.2917   1.0000
  11.500   1.9843   0.01886   0.01345  -0.1553   0.2802   1.0000
  11.750   1.9988   0.01958   0.01417  -0.1539   0.2744   1.0000
  12.000   2.0127   0.02035   0.01494  -0.1524   0.2696   1.0000
  12.250   2.0288   0.02099   0.01560  -0.1512   0.2655   1.0000
  12.500   2.0422   0.02181   0.01644  -0.1497   0.2609   1.0000
  12.750   2.0545   0.02270   0.01734  -0.1482   0.2570   1.0000
  13.000   2.0683   0.02351   0.01818  -0.1469   0.2541   1.0000
  13.250   2.0820   0.02433   0.01905  -0.1456   0.2505   1.0000
  13.500   2.0943   0.02526   0.02002  -0.1442   0.2473   1.0000
  13.750   2.1031   0.02645   0.02122  -0.1425   0.2434   1.0000
  14.000   2.1128   0.02759   0.02239  -0.1410   0.2392   1.0000
  14.250   2.1218   0.02880   0.02364  -0.1394   0.2343   1.0000
  14.500   2.1235   0.03062   0.02546  -0.1374   0.2276   1.0000
  14.750   2.1311   0.03203   0.02690  -0.1359   0.2221   1.0000
  15.000   2.1316   0.03407   0.02896  -0.1341   0.2153   1.0000
  15.250   2.1337   0.03608   0.03099  -0.1325   0.2096   1.0000
  15.500   2.1306   0.03865   0.03358  -0.1308   0.2015   1.0000
  15.750   2.1256   0.04151   0.03647  -0.1292   0.1936   1.0000
  16.000   2.1127   0.04532   0.04029  -0.1275   0.1843   1.0000
  16.250   2.0954   0.04980   0.04479  -0.1260   0.1742   1.0000
  16.500   2.0737   0.05495   0.04997  -0.1248   0.1643   1.0000
  16.750   2.0464   0.06093   0.05599  -0.1237   0.1551   1.0000
  17.250   1.9901   0.07355   0.06874  -0.1224   0.1408   1.0000
  17.500   1.9599   0.08029   0.07554  -0.1221   0.1348   1.0000
  17.750   1.9335   0.08664   0.08195  -0.1220   0.1285   1.0000
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