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FX 73-CL3-152 (fx73cl3152-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX 73-CL3-152 (fx73cl3152-il)
Reynolds number: 500,000
Max Cl/Cd: 99.08 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx73cl3152-il-500000.txt
Download as CSV file: xf-fx73cl3152-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250   0.1961   0.09443   0.09149  -0.1272   0.8896   0.0349
 -10.000   0.2050   0.09216   0.08920  -0.1281   0.8814   0.0359
  -9.750   0.1892   0.08787   0.08489  -0.1328   0.8735   0.0374
  -9.500   0.2068   0.08560   0.08258  -0.1324   0.8663   0.0377
  -9.250   0.2194   0.08386   0.08084  -0.1317   0.8568   0.0379
  -9.000   0.2329   0.08218   0.07912  -0.1317   0.8477   0.0383
  -8.750   0.2416   0.08044   0.07737  -0.1315   0.8370   0.0387
  -8.500   0.2501   0.07863   0.07552  -0.1315   0.8252   0.0397
  -8.250   0.2310   0.07430   0.07117  -0.1353   0.8138   0.0421
  -8.000   0.2383   0.07197   0.06882  -0.1345   0.7968   0.0424
  -7.750   0.2478   0.07056   0.06732  -0.1333   0.7696   0.0426
  -7.500   0.2535   0.06962   0.06612  -0.1308   0.7133   0.0429
  -7.250   0.2569   0.06873   0.06494  -0.1285   0.6650   0.0433
  -7.000   0.2609   0.06747   0.06352  -0.1273   0.6330   0.0438
  -6.750   0.1444   0.02250   0.01783  -0.1805   0.6779   0.0364
  -6.500   0.1667   0.02020   0.01491  -0.1824   0.6465   0.0368
  -6.250   0.1909   0.01892   0.01316  -0.1830   0.6208   0.0373
  -6.000   0.2144   0.01764   0.01155  -0.1831   0.5992   0.0378
  -5.750   0.2386   0.01703   0.01079  -0.1828   0.5804   0.0384
  -5.500   0.2636   0.01661   0.01021  -0.1825   0.5642   0.0390
  -5.000   0.3150   0.01584   0.00910  -0.1818   0.5385   0.0408
  -4.750   0.3411   0.01554   0.00856  -0.1815   0.5285   0.0419
  -4.500   0.3670   0.01489   0.00780  -0.1812   0.5198   0.0427
  -4.250   0.3924   0.01460   0.00742  -0.1807   0.5116   0.0437
  -4.000   0.4193   0.01432   0.00709  -0.1804   0.5052   0.0448
  -3.750   0.4458   0.01409   0.00675  -0.1800   0.4988   0.0461
  -3.500   0.4719   0.01398   0.00648  -0.1795   0.4927   0.0472
  -3.250   0.4983   0.01355   0.00606  -0.1792   0.4880   0.0489
  -3.000   0.5251   0.01341   0.00589  -0.1788   0.4829   0.0508
  -2.750   0.5516   0.01333   0.00570  -0.1784   0.4782   0.0527
  -2.500   0.5772   0.01312   0.00543  -0.1779   0.4737   0.0548
  -2.250   0.6043   0.01299   0.00530  -0.1775   0.4704   0.0572
  -2.000   0.6313   0.01284   0.00512  -0.1772   0.4671   0.0600
  -1.750   0.6579   0.01272   0.00500  -0.1768   0.4637   0.0638
  -1.500   0.6844   0.01263   0.00486  -0.1764   0.4604   0.0681
  -1.250   0.7107   0.01263   0.00481  -0.1759   0.4568   0.0734
  -1.000   0.7372   0.01261   0.00477  -0.1755   0.4533   0.0816
  -0.750   0.7640   0.01250   0.00471  -0.1751   0.4510   0.0946
  -0.500   0.7908   0.01243   0.00470  -0.1748   0.4485   0.1157
  -0.250   0.8173   0.01239   0.00474  -0.1744   0.4459   0.1407
   0.000   0.8438   0.01243   0.00478  -0.1740   0.4432   0.1611
   0.250   0.8701   0.01249   0.00485  -0.1735   0.4404   0.1802
   0.500   0.8965   0.01262   0.00496  -0.1731   0.4375   0.1979
   0.750   0.9235   0.01277   0.00510  -0.1729   0.4348   0.2156
   1.000   0.9497   0.01279   0.00518  -0.1724   0.4328   0.2336
   1.250   0.9759   0.01283   0.00526  -0.1719   0.4305   0.2519
   1.500   1.0020   0.01288   0.00535  -0.1715   0.4281   0.2710
   1.750   1.0279   0.01295   0.00545  -0.1710   0.4257   0.2928
   2.250   1.0795   0.01315   0.00570  -0.1700   0.4209   0.3424
   2.500   1.1061   0.01335   0.00591  -0.1698   0.4181   0.3702
   2.750   1.1323   0.01348   0.00609  -0.1694   0.4160   0.4004
   3.000   1.1573   0.01351   0.00623  -0.1687   0.4142   0.4332
   3.250   1.1823   0.01358   0.00639  -0.1681   0.4122   0.4682
   3.500   1.2073   0.01366   0.00657  -0.1675   0.4101   0.5074
   3.750   1.2320   0.01376   0.00675  -0.1668   0.4081   0.5492
   4.000   1.2564   0.01386   0.00692  -0.1661   0.4060   0.5922
   4.250   1.2806   0.01397   0.00711  -0.1654   0.4039   0.6371
   4.500   1.3052   0.01413   0.00733  -0.1647   0.4015   0.6859
   4.750   1.3319   0.01432   0.00761  -0.1646   0.3986   0.7530
   5.000   1.3883   0.01429   0.00787  -0.1708   0.3966   1.0000
   5.250   1.4134   0.01446   0.00804  -0.1704   0.3948   1.0000
   5.500   1.4385   0.01465   0.00822  -0.1699   0.3927   1.0000
   5.750   1.4635   0.01484   0.00841  -0.1694   0.3906   1.0000
   6.000   1.4883   0.01505   0.00860  -0.1689   0.3885   1.0000
   6.250   1.5129   0.01527   0.00880  -0.1684   0.3864   1.0000
   6.500   1.5380   0.01554   0.00903  -0.1680   0.3842   1.0000
   6.750   1.5661   0.01597   0.00939  -0.1682   0.3812   1.0000
   7.000   1.5882   0.01614   0.00962  -0.1673   0.3797   1.0000
   7.250   1.6096   0.01633   0.00984  -0.1662   0.3776   1.0000
   7.500   1.6308   0.01654   0.01009  -0.1651   0.3753   1.0000
   7.750   1.6523   0.01676   0.01033  -0.1641   0.3730   1.0000
   8.000   1.6738   0.01700   0.01057  -0.1631   0.3708   1.0000
   8.250   1.6955   0.01726   0.01084  -0.1621   0.3686   1.0000
   8.500   1.7186   0.01760   0.01114  -0.1615   0.3662   1.0000
   8.750   1.7437   0.01800   0.01153  -0.1613   0.3636   1.0000
   9.000   1.7619   0.01826   0.01187  -0.1599   0.3618   1.0000
   9.250   1.7806   0.01855   0.01222  -0.1585   0.3594   1.0000
   9.500   1.7998   0.01886   0.01258  -0.1574   0.3569   1.0000
   9.750   1.8190   0.01918   0.01293  -0.1562   0.3544   1.0000
  10.000   1.8383   0.01953   0.01330  -0.1551   0.3520   1.0000
  10.250   1.8588   0.01994   0.01369  -0.1543   0.3496   1.0000
  10.500   1.8806   0.02040   0.01415  -0.1536   0.3469   1.0000
  10.750   1.8967   0.02084   0.01469  -0.1522   0.3448   1.0000
  11.000   1.9133   0.02129   0.01523  -0.1509   0.3423   1.0000
  11.250   1.9300   0.02177   0.01576  -0.1496   0.3397   1.0000
  11.500   1.9463   0.02226   0.01629  -0.1483   0.3370   1.0000
  11.750   1.9632   0.02279   0.01683  -0.1471   0.3344   1.0000
  12.000   1.9806   0.02338   0.01740  -0.1460   0.3310   1.0000
  12.250   1.9911   0.02409   0.01824  -0.1442   0.3277   1.0000
  12.500   2.0024   0.02482   0.01905  -0.1425   0.3236   1.0000
  12.750   2.0140   0.02560   0.01985  -0.1409   0.3197   1.0000
  13.000   2.0272   0.02641   0.02062  -0.1395   0.3159   1.0000
  13.250   2.0381   0.02732   0.02166  -0.1380   0.3129   1.0000
  13.500   2.0498   0.02822   0.02266  -0.1366   0.3096   1.0000
  13.750   2.0609   0.02919   0.02369  -0.1352   0.3065   1.0000
  14.000   2.0710   0.03024   0.02476  -0.1337   0.3035   1.0000
  14.250   2.0804   0.03136   0.02589  -0.1322   0.3000   1.0000
  14.500   2.0892   0.03258   0.02724  -0.1308   0.2972   1.0000
  14.750   2.0975   0.03386   0.02862  -0.1294   0.2939   1.0000
  15.000   2.1043   0.03527   0.03008  -0.1279   0.2903   1.0000
  15.250   2.1083   0.03692   0.03173  -0.1263   0.2865   1.0000
  15.500   2.1127   0.03868   0.03360  -0.1250   0.2826   1.0000
  15.750   2.1160   0.04061   0.03563  -0.1238   0.2781   1.0000
  16.000   2.1164   0.04284   0.03789  -0.1225   0.2736   1.0000
  16.250   2.1160   0.04520   0.04030  -0.1212   0.2695   1.0000
  16.500   2.1172   0.04759   0.04282  -0.1203   0.2655   1.0000
  16.750   2.1147   0.05036   0.04566  -0.1193   0.2610   1.0000
  17.000   2.1082   0.05357   0.04887  -0.1183   0.2565   1.0000
  17.250   2.1054   0.05656   0.05201  -0.1176   0.2526   1.0000
  17.500   2.0981   0.06008   0.05563  -0.1170   0.2477   1.0000
  17.750   2.0858   0.06418   0.05974  -0.1163   0.2428   1.0000
  18.000   2.0752   0.06824   0.06392  -0.1159   0.2378   1.0000
  18.250   2.0604   0.07285   0.06862  -0.1156   0.2321   1.0000
  18.500   2.0411   0.07797   0.07376  -0.1153   0.2264   1.0000
  18.750   2.0232   0.08315   0.07908  -0.1153   0.2200   1.0000
  19.000   1.9996   0.08901   0.08495  -0.1153   0.2135   1.0000
  19.250   1.9788   0.09464   0.09069  -0.1156   0.2061   1.0000
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