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WORTMANN FX 63-137 AIRFOIL (fx63137-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 63-137 AIRFOIL (fx63137-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.72 at α=1.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx63137-il-1000000-n5.txt
Download as CSV file: xf-fx63137-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 63-137 AIRFOIL                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.2896   0.10874   0.10679  -0.0759   0.9863   0.0052
 -13.000  -0.2960   0.10151   0.09952  -0.0806   0.9841   0.0052
 -12.500  -0.5628   0.03603   0.03306  -0.1335   0.9435   0.0044
 -12.250  -0.5364   0.02909   0.02582  -0.1494   0.9252   0.0045
 -12.000  -0.4896   0.02429   0.02071  -0.1647   0.9093   0.0046
 -11.750  -0.4500   0.02138   0.01754  -0.1746   0.8912   0.0047
 -11.500  -0.4199   0.01949   0.01543  -0.1801   0.8744   0.0047
 -11.250  -0.3950   0.01823   0.01398  -0.1825   0.8590   0.0048
 -11.000  -0.3706   0.01736   0.01295  -0.1837   0.8453   0.0048
 -10.750  -0.3458   0.01654   0.01198  -0.1847   0.8335   0.0049
 -10.500  -0.3203   0.01579   0.01109  -0.1856   0.8237   0.0049
 -10.000  -0.2673   0.01457   0.00963  -0.1869   0.8045   0.0051
  -9.500  -0.2120   0.01351   0.00835  -0.1883   0.7902   0.0053
  -9.250  -0.1838   0.01307   0.00781  -0.1889   0.7838   0.0054
  -9.000  -0.1552   0.01265   0.00730  -0.1895   0.7781   0.0055
  -8.750  -0.1258   0.01223   0.00681  -0.1903   0.7727   0.0056
  -8.500  -0.0967   0.01187   0.00637  -0.1909   0.7666   0.0058
  -8.250  -0.0675   0.01155   0.00597  -0.1915   0.7604   0.0059
  -8.000  -0.0380   0.01124   0.00560  -0.1921   0.7532   0.0061
  -7.500   0.0214   0.01066   0.00491  -0.1933   0.7411   0.0071
  -7.250   0.0512   0.01040   0.00464  -0.1939   0.7352   0.0077
  -7.000   0.0799   0.01031   0.00455  -0.1941   0.7298   0.0119
  -6.750   0.1098   0.01014   0.00434  -0.1946   0.7244   0.0131
  -6.500   0.1390   0.01002   0.00417  -0.1949   0.7172   0.0140
  -6.250   0.1681   0.00992   0.00402  -0.1952   0.7101   0.0147
  -6.000   0.1974   0.00983   0.00388  -0.1955   0.7019   0.0150
  -5.750   0.2269   0.00968   0.00369  -0.1959   0.6948   0.0154
  -5.500   0.2570   0.00952   0.00349  -0.1965   0.6875   0.0159
  -5.250   0.2859   0.00943   0.00335  -0.1967   0.6789   0.0168
  -5.000   0.3153   0.00933   0.00321  -0.1971   0.6694   0.0174
  -4.750   0.3445   0.00926   0.00306  -0.1974   0.6602   0.0178
  -4.500   0.3736   0.00919   0.00293  -0.1977   0.6477   0.0180
  -4.250   0.4029   0.00912   0.00280  -0.1980   0.6340   0.0182
  -4.000   0.4322   0.00905   0.00265  -0.1983   0.6211   0.0185
  -3.750   0.4616   0.00898   0.00252  -0.1986   0.6105   0.0188
  -3.500   0.4915   0.00891   0.00240  -0.1991   0.6024   0.0193
  -3.250   0.5211   0.00885   0.00229  -0.1994   0.5954   0.0201
  -3.000   0.5510   0.00879   0.00220  -0.1999   0.5868   0.0208
  -2.750   0.5800   0.00879   0.00214  -0.2001   0.5753   0.0212
  -2.500   0.6087   0.00881   0.00210  -0.2002   0.5612   0.0215
  -2.250   0.6375   0.00883   0.00207  -0.2004   0.5508   0.0219
  -2.000   0.6665   0.00885   0.00205  -0.2006   0.5425   0.0232
  -1.750   0.6959   0.00884   0.00204  -0.2010   0.5341   0.0321
  -1.500   0.7247   0.00887   0.00205  -0.2011   0.5269   0.0367
  -1.250   0.7535   0.00890   0.00206  -0.2013   0.5170   0.0391
  -1.000   0.7819   0.00896   0.00207  -0.2014   0.5043   0.0423
  -0.750   0.8101   0.00904   0.00211  -0.2015   0.4910   0.0481
  -0.500   0.8387   0.00910   0.00215  -0.2017   0.4809   0.0667
  -0.250   0.8673   0.00915   0.00219  -0.2018   0.4727   0.0753
   0.000   0.8962   0.00919   0.00225  -0.2022   0.4628   0.1088
   0.250   0.9244   0.00931   0.00237  -0.2024   0.4315   0.1646
   0.500   0.9529   0.00944   0.00254  -0.2030   0.4005   0.2627
   0.750   0.9829   0.00948   0.00272  -0.2039   0.3735   0.3733
   1.000   1.0094   0.00972   0.00291  -0.2037   0.3514   0.4087
   1.250   1.0364   0.00990   0.00306  -0.2036   0.3383   0.4277
   1.500   1.0635   0.01006   0.00320  -0.2035   0.3283   0.4412
   1.750   1.0881   0.01041   0.00342  -0.2030   0.2988   0.4541
   2.000   1.1138   0.01068   0.00363  -0.2026   0.2840   0.4707
   2.250   1.1395   0.01094   0.00385  -0.2023   0.2682   0.4881
   2.500   1.1626   0.01140   0.00417  -0.2015   0.2346   0.5026
   2.750   1.1878   0.01169   0.00440  -0.2010   0.2229   0.5155
   3.000   1.2125   0.01198   0.00464  -0.2005   0.2068   0.5245
   3.250   1.2347   0.01249   0.00500  -0.1996   0.1785   0.5317
   3.500   1.2593   0.01277   0.00525  -0.1990   0.1697   0.5425
   3.750   1.2848   0.01299   0.00548  -0.1986   0.1637   0.5542
   4.000   1.3067   0.01347   0.00585  -0.1976   0.1384   0.5625
   4.250   1.3305   0.01378   0.00613  -0.1970   0.1316   0.5697
   4.500   1.3546   0.01406   0.00640  -0.1963   0.1260   0.5760
   4.750   1.3790   0.01431   0.00665  -0.1958   0.1206   0.5817
   5.000   1.4007   0.01472   0.00702  -0.1947   0.1049   0.5874
   5.250   1.4212   0.01520   0.00742  -0.1935   0.0939   0.5930
   5.500   1.4435   0.01554   0.00775  -0.1926   0.0884   0.5987
   5.750   1.4652   0.01588   0.00810  -0.1915   0.0840   0.6052
   6.000   1.4846   0.01626   0.00848  -0.1901   0.0796   0.6115
   6.250   1.5052   0.01654   0.00880  -0.1888   0.0772   0.6180
   6.750   1.5375   0.01759   0.00978  -0.1848   0.0580   0.6336
   7.000   1.5557   0.01802   0.01024  -0.1832   0.0565   0.6431
   7.250   1.5733   0.01848   0.01074  -0.1816   0.0549   0.6527
   7.500   1.5900   0.01901   0.01128  -0.1798   0.0525   0.6628
   7.750   1.6067   0.01954   0.01186  -0.1781   0.0505   0.6722
   8.000   1.6244   0.02002   0.01239  -0.1766   0.0500   0.6826
   8.250   1.6419   0.02052   0.01296  -0.1751   0.0495   0.6943
   8.500   1.6586   0.02108   0.01358  -0.1735   0.0490   0.7064
   8.750   1.6748   0.02168   0.01425  -0.1719   0.0481   0.7196
   9.000   1.6903   0.02234   0.01497  -0.1702   0.0473   0.7344
   9.500   1.7173   0.02399   0.01673  -0.1666   0.0440   0.7679
   9.750   1.7302   0.02490   0.01772  -0.1648   0.0425   0.7906
  10.000   1.7445   0.02571   0.01863  -0.1633   0.0415   0.8217
  10.250   1.7570   0.02638   0.01949  -0.1614   0.0408   0.9000
  10.500   1.7658   0.02721   0.02040  -0.1590   0.0399   1.0000
  10.750   1.7781   0.02826   0.02148  -0.1575   0.0379   1.0000
  11.000   1.7881   0.02955   0.02277  -0.1558   0.0352   1.0000
  11.250   1.7985   0.03084   0.02407  -0.1542   0.0320   1.0000
  11.500   1.7987   0.03306   0.02619  -0.1519   0.0211   1.0000
  11.750   1.7946   0.03582   0.02894  -0.1494   0.0114   1.0000
  12.000   1.7882   0.03897   0.03212  -0.1470   0.0036   1.0000
  12.250   1.7942   0.04097   0.03418  -0.1457   0.0030   1.0000
  12.500   1.8003   0.04302   0.03630  -0.1444   0.0027   1.0000
  12.750   1.8058   0.04519   0.03854  -0.1433   0.0025   1.0000
  13.000   1.8116   0.04739   0.04081  -0.1423   0.0023   1.0000
  13.250   1.8173   0.04965   0.04314  -0.1414   0.0022   1.0000
  13.500   1.8224   0.05204   0.04561  -0.1405   0.0021   1.0000
  13.750   1.8260   0.05468   0.04833  -0.1398   0.0019   1.0000
  14.000   1.8291   0.05745   0.05117  -0.1391   0.0019   1.0000
  14.250   1.8320   0.06031   0.05411  -0.1386   0.0018   1.0000
  14.500   1.8339   0.06340   0.05729  -0.1381   0.0017   1.0000
  14.750   1.8343   0.06674   0.06073  -0.1378   0.0016   1.0000
  15.000   1.8350   0.07013   0.06421  -0.1376   0.0016   1.0000
  15.250   1.8354   0.07364   0.06780  -0.1375   0.0015   1.0000
  15.500   1.8362   0.07716   0.07141  -0.1376   0.0015   1.0000
  15.750   1.8363   0.08085   0.07519  -0.1378   0.0015   1.0000
  16.000   1.8358   0.08468   0.07911  -0.1381   0.0015   1.0000
  16.250   1.8345   0.08871   0.08324  -0.1385   0.0014   1.0000
  16.500   1.8326   0.09289   0.08752  -0.1392   0.0014   1.0000
  16.750   1.8298   0.09729   0.09202  -0.1399   0.0014   1.0000
  17.000   1.8272   0.10167   0.09650  -0.1408   0.0013   1.0000
  17.250   1.8231   0.10636   0.10129  -0.1419   0.0013   1.0000
  17.500   1.8198   0.11095   0.10599  -0.1431   0.0013   1.0000
  17.750   1.8163   0.11559   0.11072  -0.1445   0.0012   1.0000
  18.000   1.8118   0.12045   0.11568  -0.1460   0.0012   1.0000
  18.250   1.8072   0.12535   0.12069  -0.1477   0.0012   1.0000
  18.500   1.8036   0.13006   0.12549  -0.1495   0.0012   1.0000
  18.750   1.7979   0.13517   0.13071  -0.1516   0.0012   1.0000
  19.000   1.7928   0.14017   0.13582  -0.1538   0.0012   1.0000
  19.250   1.7880   0.14515   0.14089  -0.1560   0.0011   1.0000
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