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FX 73-CL3-152 (fx73cl3152-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 73-CL3-152 (fx73cl3152-il)
Reynolds number: 1,000,000
Max Cl/Cd: 129.31 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx73cl3152-il-1000000.txt
Download as CSV file: xf-fx73cl3152-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250   0.1808   0.09133   0.08874  -0.1260   0.8303   0.0262
 -10.000  -0.1325   0.03891   0.03604  -0.1553   0.8336   0.0253
  -9.750  -0.1609   0.02589   0.02259  -0.1746   0.8253   0.0254
  -9.500  -0.1389   0.02000   0.01628  -0.1854   0.8174   0.0257
  -9.250  -0.1144   0.01854   0.01468  -0.1870   0.8099   0.0260
  -9.000  -0.0883   0.01772   0.01380  -0.1878   0.8002   0.0263
  -8.750  -0.0620   0.01708   0.01307  -0.1882   0.7891   0.0266
  -8.500  -0.0361   0.01647   0.01233  -0.1884   0.7724   0.0270
  -8.250  -0.0116   0.01584   0.01150  -0.1883   0.7420   0.0273
  -8.000   0.0101   0.01543   0.01078  -0.1876   0.6941   0.0277
  -7.750   0.0328   0.01503   0.01011  -0.1870   0.6564   0.0280
  -7.500   0.0568   0.01467   0.00952  -0.1865   0.6274   0.0283
  -7.250   0.0820   0.01430   0.00897  -0.1862   0.6040   0.0286
  -7.000   0.1077   0.01402   0.00851  -0.1859   0.5833   0.0289
  -6.750   0.1330   0.01349   0.00780  -0.1856   0.5650   0.0293
  -6.500   0.1583   0.01301   0.00719  -0.1854   0.5486   0.0298
  -6.250   0.1847   0.01277   0.00686  -0.1851   0.5343   0.0303
  -6.000   0.2115   0.01257   0.00658  -0.1848   0.5225   0.0309
  -5.750   0.2379   0.01240   0.00630  -0.1844   0.5110   0.0314
  -5.500   0.2651   0.01219   0.00601  -0.1842   0.5021   0.0321
  -5.250   0.2917   0.01206   0.00577  -0.1838   0.4925   0.0327
  -5.000   0.3192   0.01191   0.00554  -0.1835   0.4860   0.0330
  -4.750   0.3455   0.01153   0.00510  -0.1832   0.4790   0.0342
  -4.500   0.3722   0.01143   0.00494  -0.1828   0.4721   0.0350
  -4.250   0.3999   0.01130   0.00478  -0.1826   0.4674   0.0359
  -4.000   0.4270   0.01120   0.00461  -0.1822   0.4621   0.0368
  -3.750   0.4537   0.01112   0.00444  -0.1818   0.4564   0.0376
  -3.500   0.4805   0.01090   0.00420  -0.1814   0.4525   0.0389
  -3.250   0.5081   0.01080   0.00408  -0.1812   0.4494   0.0402
  -3.000   0.5354   0.01073   0.00396  -0.1808   0.4459   0.0414
  -2.750   0.5622   0.01063   0.00381  -0.1804   0.4424   0.0429
  -2.500   0.5888   0.01058   0.00373  -0.1800   0.4386   0.0448
  -2.250   0.6154   0.01058   0.00369  -0.1795   0.4349   0.0467
  -2.000   0.6428   0.01045   0.00356  -0.1792   0.4330   0.0490
  -1.750   0.6702   0.01039   0.00349  -0.1789   0.4307   0.0517
  -1.500   0.6972   0.01032   0.00341  -0.1785   0.4281   0.0551
  -1.250   0.7240   0.01031   0.00337  -0.1781   0.4255   0.0590
  -1.000   0.7503   0.01027   0.00333  -0.1776   0.4229   0.0652
  -0.750   0.7763   0.01028   0.00333  -0.1770   0.4199   0.0738
  -0.500   0.8019   0.01028   0.00336  -0.1764   0.4167   0.0898
  -0.250   0.8289   0.01020   0.00336  -0.1761   0.4154   0.1118
   0.000   0.8558   0.01018   0.00338  -0.1757   0.4137   0.1303
   0.250   0.8826   0.01017   0.00341  -0.1753   0.4118   0.1470
   0.500   0.9091   0.01018   0.00345  -0.1749   0.4096   0.1629
   1.000   0.9610   0.01027   0.00357  -0.1738   0.4049   0.1953
   1.250   0.9862   0.01035   0.00367  -0.1732   0.4022   0.2120
   1.500   1.0109   0.01049   0.00380  -0.1725   0.3989   0.2279
   1.750   1.0373   0.01051   0.00386  -0.1720   0.3978   0.2447
   2.000   1.0635   0.01053   0.00393  -0.1716   0.3965   0.2620
   2.250   1.0894   0.01056   0.00402  -0.1711   0.3950   0.2843
   2.500   1.1151   0.01060   0.00411  -0.1705   0.3934   0.3079
   2.750   1.1405   0.01065   0.00421  -0.1699   0.3917   0.3316
   3.000   1.1655   0.01071   0.00431  -0.1693   0.3898   0.3575
   3.250   1.1900   0.01079   0.00443  -0.1685   0.3877   0.3844
   3.500   1.2137   0.01090   0.00457  -0.1677   0.3854   0.4119
   3.750   1.2369   0.01105   0.00475  -0.1667   0.3827   0.4416
   4.000   1.2603   0.01117   0.00492  -0.1658   0.3807   0.4738
   4.250   1.2838   0.01119   0.00505  -0.1649   0.3797   0.5111
   4.500   1.3067   0.01123   0.00518  -0.1638   0.3784   0.5483
   4.750   1.3294   0.01129   0.00532  -0.1628   0.3769   0.5865
   5.000   1.3520   0.01137   0.00548  -0.1617   0.3753   0.6255
   5.250   1.3743   0.01145   0.00564  -0.1606   0.3736   0.6681
   5.500   1.3958   0.01153   0.00581  -0.1593   0.3718   0.7152
   5.750   1.4901   0.01158   0.00622  -0.1739   0.3684   1.0000
   6.000   1.5138   0.01184   0.00645  -0.1732   0.3656   1.0000
   6.250   1.5385   0.01206   0.00665  -0.1727   0.3634   1.0000
   6.500   1.5641   0.01218   0.00679  -0.1724   0.3621   1.0000
   6.750   1.5893   0.01233   0.00695  -0.1719   0.3604   1.0000
   7.000   1.6141   0.01249   0.00713  -0.1715   0.3586   1.0000
   7.250   1.6384   0.01267   0.00731  -0.1710   0.3566   1.0000
   7.500   1.6621   0.01287   0.00752  -0.1703   0.3545   1.0000
   7.750   1.6849   0.01312   0.00775  -0.1696   0.3522   1.0000
   8.000   1.7065   0.01343   0.00804  -0.1687   0.3494   1.0000
   8.250   1.7288   0.01372   0.00833  -0.1679   0.3469   1.0000
   8.500   1.7526   0.01389   0.00855  -0.1674   0.3452   1.0000
   8.750   1.7759   0.01410   0.00878  -0.1668   0.3431   1.0000
   9.000   1.7986   0.01434   0.00905  -0.1662   0.3408   1.0000
   9.250   1.8203   0.01462   0.00934  -0.1654   0.3384   1.0000
   9.500   1.8408   0.01496   0.00968  -0.1644   0.3358   1.0000
   9.750   1.8596   0.01540   0.01010  -0.1633   0.3326   1.0000
  10.000   1.8805   0.01574   0.01047  -0.1624   0.3304   1.0000
  10.250   1.9023   0.01601   0.01080  -0.1618   0.3284   1.0000
  10.500   1.9235   0.01632   0.01115  -0.1610   0.3258   1.0000
  10.750   1.9431   0.01672   0.01156  -0.1600   0.3226   1.0000
  11.000   1.9603   0.01723   0.01206  -0.1588   0.3189   1.0000
  11.250   1.9776   0.01775   0.01259  -0.1576   0.3147   1.0000
  11.500   1.9981   0.01811   0.01299  -0.1569   0.3107   1.0000
  11.750   2.0155   0.01863   0.01353  -0.1558   0.3064   1.0000
  12.000   2.0298   0.01934   0.01423  -0.1543   0.3019   1.0000
  12.250   2.0470   0.01989   0.01482  -0.1532   0.2987   1.0000
  12.500   2.0650   0.02041   0.01538  -0.1522   0.2952   1.0000
  12.750   2.0804   0.02107   0.01607  -0.1510   0.2918   1.0000
  13.000   2.0930   0.02192   0.01692  -0.1494   0.2880   1.0000
  13.250   2.1065   0.02273   0.01776  -0.1480   0.2845   1.0000
  13.500   2.1222   0.02339   0.01849  -0.1469   0.2819   1.0000
  13.750   2.1359   0.02420   0.01933  -0.1456   0.2781   1.0000
  14.000   2.1451   0.02532   0.02046  -0.1439   0.2735   1.0000
  14.250   2.1549   0.02642   0.02158  -0.1424   0.2692   1.0000
  14.500   2.1674   0.02734   0.02255  -0.1411   0.2648   1.0000
  14.750   2.1747   0.02866   0.02389  -0.1394   0.2604   1.0000
  15.000   2.1783   0.03029   0.02554  -0.1375   0.2557   1.0000
  15.250   2.1903   0.03133   0.02666  -0.1364   0.2526   1.0000
  15.500   2.1969   0.03282   0.02818  -0.1349   0.2480   1.0000
  15.750   2.1967   0.03494   0.03032  -0.1331   0.2427   1.0000
  16.000   2.2029   0.03659   0.03203  -0.1318   0.2384   1.0000
  16.250   2.2044   0.03871   0.03419  -0.1304   0.2326   1.0000
  16.500   2.1980   0.04166   0.03716  -0.1287   0.2268   1.0000
  16.750   2.1998   0.04392   0.03948  -0.1276   0.2208   1.0000
  17.000   2.1892   0.04753   0.04312  -0.1262   0.2141   1.0000
  17.250   2.1834   0.05072   0.04637  -0.1251   0.2074   1.0000
  17.500   2.1652   0.05540   0.05108  -0.1239   0.2003   1.0000
  17.750   2.1499   0.05987   0.05560  -0.1230   0.1926   1.0000
  18.000   2.1206   0.06606   0.06183  -0.1221   0.1845   1.0000
  18.250   2.0919   0.07232   0.06814  -0.1215   0.1758   1.0000
  18.500   2.0595   0.07917   0.07505  -0.1211   0.1682   1.0000
  18.750   2.0224   0.08674   0.08267  -0.1209   0.1606   1.0000
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