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FX 62-K-153/20 AIRFOIL (fx62k153-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 62-K-153/20 AIRFOIL (fx62k153-il)
Reynolds number: 1,000,000
Max Cl/Cd: 161.95 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx62k153-il-1000000.txt
Download as CSV file: xf-fx62k153-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 62-K-153/20 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.0720   0.08334   0.08092  -0.1133   0.8292   0.0104
 -11.250  -0.0746   0.07865   0.07624  -0.1148   0.8275   0.0105
 -11.000  -0.2292   0.07143   0.06902  -0.1187   0.8358   0.0061
 -10.750  -0.4698   0.02429   0.02015  -0.1428   0.8261   0.0046
 -10.500  -0.4570   0.02186   0.01744  -0.1439   0.8235   0.0046
 -10.250  -0.4384   0.02020   0.01555  -0.1448   0.8211   0.0046
 -10.000  -0.4174   0.01891   0.01407  -0.1454   0.8188   0.0047
  -9.750  -0.3946   0.01787   0.01287  -0.1459   0.8163   0.0048
  -9.500  -0.3714   0.01692   0.01181  -0.1464   0.8146   0.0049
  -9.250  -0.3471   0.01611   0.01089  -0.1468   0.8127   0.0050
  -9.000  -0.3221   0.01536   0.01004  -0.1473   0.8109   0.0052
  -8.750  -0.2965   0.01467   0.00926  -0.1478   0.8090   0.0055
  -8.500  -0.2703   0.01407   0.00857  -0.1483   0.8071   0.0058
  -8.250  -0.2431   0.01362   0.00804  -0.1489   0.8053   0.0061
  -8.000  -0.2162   0.01297   0.00733  -0.1496   0.8034   0.0071
  -7.750  -0.1876   0.01276   0.00709  -0.1503   0.8015   0.0082
  -7.500  -0.1600   0.01231   0.00662  -0.1510   0.8001   0.0098
  -7.250  -0.1316   0.01215   0.00647  -0.1515   0.7985   0.0111
  -7.000  -0.1030   0.01205   0.00635  -0.1521   0.7968   0.0119
  -6.750  -0.0746   0.01143   0.00569  -0.1531   0.7951   0.0135
  -6.500  -0.0456   0.01119   0.00544  -0.1538   0.7935   0.0146
  -6.250  -0.0164   0.01096   0.00517  -0.1546   0.7918   0.0155
  -6.000   0.0131   0.01068   0.00484  -0.1554   0.7902   0.0165
  -5.750   0.0434   0.01033   0.00446  -0.1566   0.7885   0.0185
  -5.500   0.0735   0.01018   0.00430  -0.1575   0.7866   0.0202
  -5.250   0.1029   0.01000   0.00411  -0.1582   0.7852   0.0215
  -5.000   0.1337   0.00960   0.00369  -0.1594   0.7837   0.0248
  -4.750   0.1640   0.00939   0.00347  -0.1603   0.7820   0.0282
  -4.500   0.1954   0.00906   0.00320  -0.1615   0.7802   0.0433
  -4.250   0.2270   0.00875   0.00300  -0.1629   0.7785   0.0733
  -4.000   0.2598   0.00836   0.00279  -0.1647   0.7768   0.1316
  -3.750   0.2984   0.00750   0.00247  -0.1684   0.7752   0.3002
  -3.500   0.3412   0.00660   0.00220  -0.1731   0.7736   0.5093
  -3.250   0.3745   0.00649   0.00222  -0.1747   0.7717   0.5716
  -3.000   0.4051   0.00646   0.00225  -0.1754   0.7702   0.6021
  -2.750   0.4351   0.00648   0.00227  -0.1760   0.7684   0.6172
  -2.500   0.4651   0.00651   0.00228  -0.1766   0.7665   0.6277
  -2.250   0.4947   0.00657   0.00234  -0.1771   0.7645   0.6394
  -2.000   0.5238   0.00669   0.00247  -0.1773   0.7624   0.6535
  -1.750   0.5539   0.00677   0.00248  -0.1779   0.7602   0.6592
  -1.500   0.5836   0.00682   0.00251  -0.1785   0.7575   0.6622
  -1.250   0.6123   0.00682   0.00253  -0.1788   0.7553   0.6649
  -1.000   0.6413   0.00683   0.00254  -0.1792   0.7526   0.6679
  -0.750   0.6707   0.00685   0.00253  -0.1797   0.7498   0.6709
  -0.500   0.7005   0.00686   0.00252  -0.1803   0.7472   0.6735
  -0.250   0.7300   0.00687   0.00251  -0.1808   0.7448   0.6759
   0.000   0.7595   0.00693   0.00256  -0.1813   0.7424   0.6779
   0.250   0.7881   0.00694   0.00260  -0.1817   0.7400   0.6801
   0.500   0.8171   0.00696   0.00264  -0.1821   0.7375   0.6824
   0.750   0.8462   0.00698   0.00267  -0.1825   0.7348   0.6848
   1.000   0.8755   0.00700   0.00268  -0.1830   0.7320   0.6871
   1.250   0.9051   0.00706   0.00270  -0.1836   0.7288   0.6891
   1.500   0.9334   0.00703   0.00273  -0.1839   0.7251   0.6911
   1.750   0.9615   0.00701   0.00274  -0.1841   0.7203   0.6929
   2.000   0.9896   0.00703   0.00275  -0.1843   0.7152   0.6947
   2.250   1.0176   0.00705   0.00281  -0.1845   0.7101   0.6967
   2.500   1.0456   0.00706   0.00284  -0.1847   0.7045   0.6986
   2.750   1.0736   0.00712   0.00288  -0.1849   0.6989   0.7006
   3.000   1.1017   0.00714   0.00295  -0.1852   0.6926   0.7025
   3.250   1.1289   0.00720   0.00298  -0.1852   0.6842   0.7042
   3.500   1.1560   0.00723   0.00303  -0.1853   0.6740   0.7061
   3.750   1.1822   0.00730   0.00311  -0.1851   0.6614   0.7078
   4.000   1.2061   0.00746   0.00321  -0.1845   0.6417   0.7094
   4.250   1.2304   0.00764   0.00336  -0.1839   0.6225   0.7113
   4.500   1.2544   0.00785   0.00353  -0.1833   0.6045   0.7132
   5.000   1.2991   0.00842   0.00397  -0.1816   0.5607   0.7169
   5.250   1.3162   0.00894   0.00431  -0.1797   0.5249   0.7187
   5.500   1.3298   0.00959   0.00474  -0.1772   0.4784   0.7204
   5.750   1.3406   0.01033   0.00525  -0.1741   0.4283   0.7222
   6.000   1.3482   0.01113   0.00582  -0.1705   0.3808   0.7239
   6.250   1.3504   0.01204   0.00647  -0.1659   0.3267   0.7256
   6.500   1.3548   0.01304   0.00722  -0.1619   0.2797   0.7275
   6.750   1.3621   0.01395   0.00795  -0.1586   0.2435   0.7295
   7.000   1.3697   0.01489   0.00872  -0.1554   0.2092   0.7314
   7.250   1.3752   0.01598   0.00961  -0.1521   0.1714   0.7331
   7.500   1.3813   0.01711   0.01058  -0.1490   0.1394   0.7346
   7.750   1.3899   0.01816   0.01151  -0.1464   0.1152   0.7364
   8.000   1.4004   0.01914   0.01242  -0.1442   0.0966   0.7380
   8.250   1.4107   0.02016   0.01337  -0.1421   0.0806   0.7398
   8.500   1.4228   0.02111   0.01428  -0.1402   0.0688   0.7417
   8.750   1.4353   0.02205   0.01520  -0.1385   0.0592   0.7435
   9.000   1.4477   0.02303   0.01615  -0.1368   0.0506   0.7453
   9.250   1.4591   0.02409   0.01719  -0.1351   0.0420   0.7469
   9.500   1.4701   0.02519   0.01826  -0.1333   0.0343   0.7484
   9.750   1.4813   0.02629   0.01934  -0.1316   0.0278   0.7501
  10.000   1.4915   0.02746   0.02051  -0.1299   0.0221   0.7520
  10.250   1.5020   0.02863   0.02168  -0.1282   0.0178   0.7538
  10.500   1.5109   0.02994   0.02299  -0.1263   0.0133   0.7555
  10.750   1.5185   0.03134   0.02439  -0.1244   0.0080   0.7572
  11.000   1.5237   0.03297   0.02601  -0.1222   0.0044   0.7589
  11.250   1.5322   0.03438   0.02748  -0.1205   0.0037   0.7606
  11.500   1.5409   0.03579   0.02895  -0.1188   0.0033   0.7623
  11.750   1.5499   0.03720   0.03042  -0.1173   0.0031   0.7639
  12.000   1.5586   0.03865   0.03197  -0.1157   0.0030   0.7660
  12.250   1.5669   0.04017   0.03357  -0.1142   0.0029   0.7678
  12.500   1.5739   0.04182   0.03531  -0.1127   0.0027   0.7695
  12.750   1.5795   0.04364   0.03721  -0.1111   0.0026   0.7713
  13.000   1.5856   0.04542   0.03907  -0.1096   0.0025   0.7731
  13.250   1.5877   0.04763   0.04138  -0.1078   0.0023   0.7749
  13.500   1.5891   0.04997   0.04383  -0.1061   0.0022   0.7765
  13.750   1.5875   0.05267   0.04665  -0.1043   0.0022   0.7781
  14.000   1.5919   0.05482   0.04890  -0.1031   0.0021   0.7802
  14.250   1.5949   0.05714   0.05132  -0.1019   0.0021   0.7823
  14.500   1.5962   0.05971   0.05400  -0.1007   0.0021   0.7843
  14.750   1.5967   0.06243   0.05683  -0.0996   0.0020   0.7863
  15.000   1.5960   0.06535   0.05985  -0.0986   0.0019   0.7882
  15.250   1.5951   0.06834   0.06296  -0.0977   0.0019   0.7902
  15.500   1.5925   0.07159   0.06631  -0.0969   0.0019   0.7920
  15.750   1.5894   0.07499   0.06983  -0.0963   0.0019   0.7939
  16.000   1.5846   0.07872   0.07368  -0.0958   0.0018   0.7960
  16.250   1.5798   0.08250   0.07759  -0.0955   0.0018   0.7981
  16.500   1.5732   0.08662   0.08184  -0.0954   0.0018   0.8002
  16.750   1.5674   0.09067   0.08602  -0.0955   0.0018   0.8026
  17.000   1.5600   0.09506   0.09054  -0.0957   0.0018   0.8050
  17.250   1.5512   0.09973   0.09533  -0.0962   0.0018   0.8071
  17.500   1.5433   0.10440   0.10014  -0.0970   0.0018   0.8097
  17.750   1.5344   0.10931   0.10519  -0.0980   0.0018   0.8122
  18.000   1.5242   0.11448   0.11050  -0.0993   0.0018   0.8149
  18.250   1.5146   0.11965   0.11579  -0.1008   0.0017   0.8177
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