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FX 73-CL2-152 (fx73cl2152-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 73-CL2-152 (fx73cl2152-il)
Reynolds number: 1,000,000
Max Cl/Cd: 136.24 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx73cl2152-il-1000000.txt
Download as CSV file: xf-fx73cl2152-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 73-CL2-152                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.5588   0.05255   0.05003  -0.1071   0.9819   0.0262
 -12.000  -0.5724   0.04382   0.04111  -0.1192   0.9767   0.0264
 -11.750  -0.5858   0.03727   0.03441  -0.1266   0.9688   0.0265
 -11.500  -0.5590   0.03082   0.02777  -0.1402   0.9659   0.0268
 -11.250  -0.5310   0.02621   0.02297  -0.1507   0.9610   0.0271
 -11.000  -0.4935   0.02335   0.01993  -0.1588   0.9577   0.0275
 -10.750  -0.4554   0.02170   0.01814  -0.1637   0.9559   0.0279
 -10.500  -0.4164   0.02045   0.01678  -0.1677   0.9544   0.0281
 -10.250  -0.3762   0.01839   0.01457  -0.1731   0.9532   0.0288
 -10.000  -0.3534   0.01759   0.01375  -0.1730   0.9467   0.0292
  -9.750  -0.3188   0.01686   0.01300  -0.1749   0.9431   0.0297
  -9.500  -0.2816   0.01608   0.01217  -0.1773   0.9401   0.0302
  -9.250  -0.2577   0.01547   0.01151  -0.1769   0.9297   0.0306
  -9.000  -0.2209   0.01471   0.01067  -0.1790   0.9211   0.0312
  -8.750  -0.1712   0.01390   0.00975  -0.1837   0.9083   0.0318
  -8.500  -0.0713   0.01264   0.00816  -0.1991   0.8617   0.0328
  -8.250  -0.0351   0.01262   0.00764  -0.2011   0.7580   0.0335
  -8.000  -0.0159   0.01272   0.00742  -0.1994   0.6910   0.0340
  -7.750   0.0090   0.01270   0.00718  -0.1989   0.6460   0.0347
  -7.500   0.0364   0.01261   0.00689  -0.1989   0.6116   0.0353
  -7.250   0.0655   0.01246   0.00659  -0.1992   0.5847   0.0360
  -7.000   0.0951   0.01234   0.00631  -0.1996   0.5618   0.0365
  -6.750   0.1266   0.01204   0.00587  -0.2005   0.5422   0.0372
  -6.500   0.1586   0.01175   0.00549  -0.2016   0.5262   0.0382
  -6.250   0.1892   0.01162   0.00527  -0.2021   0.5121   0.0390
  -6.000   0.2198   0.01149   0.00507  -0.2026   0.5012   0.0400
  -5.750   0.2500   0.01141   0.00490  -0.2030   0.4911   0.0410
  -5.500   0.2801   0.01132   0.00475  -0.2033   0.4831   0.0417
  -5.250   0.3131   0.01103   0.00438  -0.2044   0.4744   0.0432
  -5.000   0.3439   0.01089   0.00421  -0.2049   0.4690   0.0444
  -4.750   0.3742   0.01080   0.00407  -0.2053   0.4633   0.0457
  -4.500   0.4040   0.01076   0.00395  -0.2055   0.4572   0.0469
  -4.250   0.4357   0.01058   0.00374  -0.2062   0.4525   0.0490
  -4.000   0.4661   0.01049   0.00363  -0.2066   0.4487   0.0510
  -3.750   0.4960   0.01045   0.00354  -0.2068   0.4449   0.0529
  -3.500   0.5271   0.01033   0.00340  -0.2074   0.4409   0.0560
  -3.250   0.5568   0.01033   0.00334  -0.2076   0.4364   0.0591
  -3.000   0.5877   0.01023   0.00325  -0.2080   0.4338   0.0640
  -2.750   0.6185   0.01013   0.00317  -0.2085   0.4314   0.0711
  -2.500   0.6496   0.01003   0.00309  -0.2090   0.4286   0.0847
  -2.250   0.6817   0.00987   0.00305  -0.2099   0.4257   0.1210
  -2.000   0.7120   0.00984   0.00307  -0.2102   0.4226   0.1491
  -1.750   0.7414   0.00988   0.00312  -0.2104   0.4187   0.1677
  -1.500   0.7704   0.00992   0.00316  -0.2104   0.4157   0.1805
  -1.250   0.8001   0.00991   0.00319  -0.2106   0.4140   0.1935
  -1.000   0.8294   0.00992   0.00322  -0.2107   0.4121   0.2045
  -0.750   0.8585   0.00994   0.00325  -0.2107   0.4099   0.2155
  -0.500   0.8876   0.00997   0.00330  -0.2108   0.4074   0.2277
  -0.250   0.9162   0.01003   0.00335  -0.2107   0.4049   0.2380
   0.000   0.9449   0.01010   0.00342  -0.2107   0.4020   0.2517
   0.250   0.9734   0.01022   0.00354  -0.2107   0.3986   0.2685
   0.500   1.0025   0.01025   0.00362  -0.2108   0.3970   0.2876
   0.750   1.0317   0.01027   0.00369  -0.2109   0.3957   0.3068
   1.000   1.0606   0.01030   0.00376  -0.2109   0.3941   0.3248
   1.250   1.0895   0.01033   0.00384  -0.2110   0.3924   0.3447
   1.500   1.1182   0.01038   0.00393  -0.2110   0.3905   0.3672
   1.750   1.1467   0.01044   0.00403  -0.2110   0.3885   0.3905
   2.000   1.1749   0.01052   0.00414  -0.2109   0.3862   0.4127
   2.250   1.2028   0.01063   0.00426  -0.2107   0.3836   0.4360
   2.750   1.2588   0.01085   0.00457  -0.2106   0.3788   0.4853
   3.000   1.2871   0.01090   0.00468  -0.2105   0.3774   0.5106
   3.250   1.3151   0.01096   0.00480  -0.2104   0.3757   0.5374
   3.500   1.3429   0.01102   0.00492  -0.2102   0.3738   0.5626
   3.750   1.3704   0.01110   0.00505  -0.2100   0.3718   0.5864
   4.000   1.3975   0.01120   0.00519  -0.2097   0.3697   0.6109
   4.250   1.4241   0.01132   0.00534  -0.2094   0.3673   0.6365
   4.500   1.4503   0.01148   0.00553  -0.2090   0.3644   0.6610
   4.750   1.4767   0.01165   0.00574  -0.2086   0.3616   0.6867
   5.000   1.5035   0.01169   0.00587  -0.2082   0.3601   0.7161
   5.250   1.5300   0.01175   0.00602  -0.2079   0.3581   0.7492
   5.500   1.5562   0.01182   0.00618  -0.2074   0.3559   0.7839
   5.750   1.5814   0.01189   0.00635  -0.2068   0.3535   0.8284
   6.000   1.5935   0.01178   0.00643  -0.2033   0.3512   0.9644
   6.250   1.6186   0.01197   0.00660  -0.2027   0.3483   1.0000
   6.500   1.6429   0.01224   0.00683  -0.2020   0.3449   1.0000
   6.750   1.6688   0.01234   0.00697  -0.2015   0.3432   1.0000
   7.000   1.6943   0.01247   0.00712  -0.2010   0.3407   1.0000
   7.250   1.7193   0.01262   0.00728  -0.2004   0.3378   1.0000
   7.500   1.7435   0.01280   0.00746  -0.1996   0.3348   1.0000
   7.750   1.7663   0.01305   0.00768  -0.1987   0.3309   1.0000
   8.000   1.7898   0.01325   0.00789  -0.1978   0.3269   1.0000
   8.250   1.8142   0.01339   0.00805  -0.1971   0.3222   1.0000
   8.500   1.8364   0.01363   0.00826  -0.1961   0.3164   1.0000
   8.750   1.8582   0.01391   0.00853  -0.1950   0.3113   1.0000
   9.000   1.8817   0.01411   0.00875  -0.1942   0.3070   1.0000
   9.250   1.9037   0.01438   0.00902  -0.1931   0.3022   1.0000
   9.500   1.9238   0.01475   0.00936  -0.1918   0.2965   1.0000
   9.750   1.9464   0.01499   0.00963  -0.1909   0.2926   1.0000
  10.000   1.9672   0.01530   0.00996  -0.1896   0.2883   1.0000
  10.250   1.9864   0.01570   0.01034  -0.1882   0.2836   1.0000
  10.500   2.0063   0.01606   0.01072  -0.1868   0.2794   1.0000
  10.750   2.0268   0.01639   0.01108  -0.1856   0.2752   1.0000
  11.000   2.0453   0.01682   0.01151  -0.1841   0.2707   1.0000
  11.250   2.0615   0.01735   0.01204  -0.1822   0.2658   1.0000
  11.500   2.0813   0.01771   0.01245  -0.1810   0.2626   1.0000
  11.750   2.0994   0.01816   0.01292  -0.1795   0.2583   1.0000
  12.000   2.1144   0.01876   0.01352  -0.1775   0.2533   1.0000
  12.250   2.1303   0.01932   0.01411  -0.1757   0.2485   1.0000
  12.500   2.1470   0.01984   0.01467  -0.1741   0.2438   1.0000
  12.750   2.1598   0.02057   0.01540  -0.1719   0.2382   1.0000
  13.000   2.1736   0.02127   0.01612  -0.1699   0.2331   1.0000
  13.250   2.1868   0.02200   0.01688  -0.1679   0.2271   1.0000
  13.500   2.1951   0.02304   0.01791  -0.1654   0.2198   1.0000
  13.750   2.2062   0.02393   0.01883  -0.1632   0.2122   1.0000
  14.000   2.2112   0.02522   0.02011  -0.1604   0.2030   1.0000
  14.250   2.2120   0.02686   0.02171  -0.1573   0.1915   1.0000
  14.500   2.2088   0.02885   0.02367  -0.1540   0.1784   1.0000
  15.000   2.1865   0.03450   0.02926  -0.1471   0.1518   1.0000
  15.250   2.1720   0.03801   0.03278  -0.1442   0.1410   1.0000
  15.500   2.1574   0.04187   0.03668  -0.1420   0.1326   1.0000
  15.750   2.1384   0.04662   0.04148  -0.1404   0.1253   1.0000
  16.000   2.1228   0.05140   0.04633  -0.1395   0.1192   1.0000
  16.500   2.0819   0.06330   0.05842  -0.1396   0.1096   1.0000
  16.750   2.0569   0.07034   0.06556  -0.1403   0.1056   1.0000
  17.000   2.0310   0.07776   0.07309  -0.1415   0.1019   1.0000
  17.250   2.0104   0.08455   0.08000  -0.1427   0.0988   1.0000
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