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FX 62-K-153/20 AIRFOIL (fx62k153-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 62-K-153/20 AIRFOIL (fx62k153-il)
Reynolds number: 500,000
Max Cl/Cd: 122.8 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx62k153-il-500000-n5.txt
Download as CSV file: xf-fx62k153-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.4431   0.04766   0.04423  -0.1316   0.8453   0.0040
 -12.000  -0.4701   0.04072   0.03698  -0.1359   0.8398   0.0039
 -11.750  -0.4871   0.03570   0.03162  -0.1380   0.8350   0.0039
 -11.250  -0.4932   0.02909   0.02441  -0.1395   0.8278   0.0040
 -11.000  -0.4870   0.02684   0.02191  -0.1397   0.8246   0.0040
 -10.750  -0.4771   0.02506   0.01987  -0.1398   0.8216   0.0041
 -10.500  -0.4624   0.02332   0.01791  -0.1405   0.8189   0.0042
 -10.000  -0.4211   0.02114   0.01546  -0.1419   0.8142   0.0046
  -9.750  -0.3985   0.02029   0.01450  -0.1424   0.8121   0.0048
  -9.500  -0.3756   0.01947   0.01355  -0.1428   0.8100   0.0050
  -9.250  -0.3522   0.01867   0.01263  -0.1432   0.8080   0.0054
  -9.000  -0.3285   0.01787   0.01168  -0.1435   0.8060   0.0058
  -8.750  -0.3042   0.01713   0.01081  -0.1438   0.8040   0.0062
  -8.500  -0.2783   0.01665   0.01027  -0.1443   0.8022   0.0067
  -8.250  -0.2522   0.01620   0.00977  -0.1448   0.8005   0.0074
  -8.000  -0.2263   0.01569   0.00918  -0.1452   0.7988   0.0083
  -7.750  -0.2002   0.01518   0.00861  -0.1457   0.7969   0.0090
  -7.500  -0.1733   0.01481   0.00820  -0.1462   0.7950   0.0098
  -7.250  -0.1461   0.01447   0.00781  -0.1467   0.7930   0.0109
  -7.000  -0.1184   0.01421   0.00748  -0.1472   0.7913   0.0119
  -6.750  -0.0908   0.01382   0.00708  -0.1479   0.7897   0.0135
  -6.500  -0.0624   0.01360   0.00682  -0.1486   0.7882   0.0151
  -6.250  -0.0339   0.01328   0.00643  -0.1493   0.7865   0.0164
  -6.000  -0.0058   0.01280   0.00594  -0.1501   0.7848   0.0178
  -5.750   0.0228   0.01245   0.00557  -0.1509   0.7831   0.0189
  -5.500   0.0519   0.01214   0.00522  -0.1517   0.7812   0.0202
  -5.250   0.0813   0.01187   0.00489  -0.1525   0.7793   0.0217
  -5.000   0.1111   0.01153   0.00456  -0.1535   0.7776   0.0252
  -4.750   0.1411   0.01130   0.00429  -0.1544   0.7759   0.0289
  -4.500   0.1716   0.01105   0.00404  -0.1554   0.7743   0.0375
  -4.250   0.2025   0.01081   0.00382  -0.1566   0.7727   0.0521
  -4.000   0.2333   0.01056   0.00363  -0.1578   0.7711   0.0758
  -3.750   0.2649   0.01017   0.00344  -0.1593   0.7692   0.1269
  -3.500   0.3014   0.00936   0.00312  -0.1626   0.7673   0.2725
  -3.250   0.3460   0.00824   0.00284  -0.1681   0.7655   0.5229
  -3.000   0.3774   0.00818   0.00287  -0.1691   0.7635   0.5711
  -2.750   0.4077   0.00820   0.00291  -0.1697   0.7616   0.6002
  -2.500   0.4375   0.00830   0.00303  -0.1702   0.7597   0.6270
  -2.250   0.4675   0.00844   0.00312  -0.1707   0.7580   0.6438
  -2.000   0.4965   0.00848   0.00315  -0.1711   0.7560   0.6474
  -1.750   0.5254   0.00852   0.00317  -0.1714   0.7538   0.6507
  -1.500   0.5547   0.00855   0.00318  -0.1719   0.7514   0.6545
  -1.250   0.5846   0.00857   0.00316  -0.1726   0.7490   0.6581
  -1.000   0.6139   0.00859   0.00315  -0.1731   0.7465   0.6607
  -0.750   0.6432   0.00862   0.00316  -0.1735   0.7442   0.6629
  -0.500   0.6723   0.00866   0.00319  -0.1739   0.7417   0.6654
  -0.250   0.7008   0.00869   0.00323  -0.1743   0.7383   0.6682
   0.000   0.7297   0.00870   0.00323  -0.1747   0.7346   0.6712
   0.250   0.7592   0.00872   0.00321  -0.1753   0.7310   0.6739
   0.500   0.7881   0.00875   0.00322  -0.1756   0.7279   0.6758
   0.750   0.8162   0.00878   0.00330  -0.1759   0.7246   0.6776
   1.000   0.8446   0.00882   0.00337  -0.1762   0.7212   0.6796
   1.250   0.8732   0.00885   0.00342  -0.1766   0.7179   0.6818
   1.500   0.9022   0.00889   0.00345  -0.1770   0.7150   0.6841
   1.750   0.9309   0.00894   0.00353  -0.1774   0.7117   0.6863
   2.000   0.9594   0.00899   0.00360  -0.1778   0.7077   0.6885
   2.250   0.9875   0.00902   0.00366  -0.1780   0.7029   0.6903
   2.500   1.0147   0.00905   0.00372  -0.1781   0.6964   0.6920
   2.750   1.0413   0.00908   0.00377  -0.1780   0.6871   0.6937
   3.000   1.0680   0.00913   0.00385  -0.1779   0.6781   0.6955
   3.250   1.0949   0.00921   0.00393  -0.1779   0.6705   0.6976
   3.500   1.1213   0.00928   0.00403  -0.1778   0.6600   0.6997
   3.750   1.1472   0.00939   0.00413  -0.1776   0.6476   0.7018
   4.000   1.1715   0.00954   0.00424  -0.1770   0.6303   0.7038
   4.250   1.1940   0.00975   0.00440  -0.1761   0.6093   0.7055
   4.500   1.2135   0.01008   0.00463  -0.1746   0.5817   0.7071
   4.750   1.2288   0.01058   0.00496  -0.1723   0.5434   0.7088
   5.000   1.2430   0.01114   0.00537  -0.1699   0.5072   0.7105
   5.250   1.2575   0.01169   0.00579  -0.1676   0.4757   0.7124
   5.500   1.2716   0.01221   0.00622  -0.1652   0.4492   0.7145
   5.750   1.2828   0.01276   0.00667  -0.1623   0.4230   0.7167
   6.000   1.2933   0.01345   0.00724  -0.1593   0.3930   0.7187
   6.250   1.2995   0.01439   0.00800  -0.1558   0.3500   0.7203
   6.500   1.2996   0.01566   0.00899  -0.1514   0.2981   0.7219
   6.750   1.3033   0.01685   0.00999  -0.1478   0.2579   0.7235
   7.000   1.3103   0.01796   0.01095  -0.1450   0.2250   0.7253
   7.250   1.3168   0.01916   0.01200  -0.1421   0.1910   0.7273
   7.500   1.3225   0.02047   0.01313  -0.1394   0.1560   0.7293
   7.750   1.3295   0.02176   0.01428  -0.1369   0.1284   0.7312
   8.000   1.3375   0.02304   0.01545  -0.1346   0.1053   0.7329
   8.250   1.3479   0.02417   0.01652  -0.1328   0.0888   0.7345
   8.500   1.3596   0.02523   0.01756  -0.1311   0.0771   0.7361
   8.750   1.3711   0.02631   0.01863  -0.1294   0.0667   0.7377
   9.000   1.3825   0.02742   0.01973  -0.1277   0.0572   0.7395
   9.250   1.3931   0.02859   0.02089  -0.1261   0.0477   0.7413
   9.500   1.4039   0.02978   0.02207  -0.1245   0.0401   0.7431
   9.750   1.4140   0.03103   0.02333  -0.1228   0.0333   0.7448
  10.000   1.4254   0.03219   0.02451  -0.1214   0.0288   0.7466
  10.250   1.4354   0.03347   0.02580  -0.1198   0.0247   0.7484
  10.500   1.4462   0.03470   0.02708  -0.1183   0.0217   0.7501
  10.750   1.4551   0.03609   0.02850  -0.1167   0.0186   0.7517
  11.000   1.4657   0.03736   0.02984  -0.1153   0.0161   0.7535
  11.250   1.4739   0.03885   0.03136  -0.1138   0.0137   0.7552
  11.500   1.4834   0.04026   0.03285  -0.1124   0.0112   0.7569
  11.750   1.4890   0.04205   0.03465  -0.1107   0.0068   0.7586
  12.000   1.4938   0.04393   0.03656  -0.1091   0.0044   0.7604
  12.250   1.4996   0.04576   0.03844  -0.1075   0.0037   0.7622
  12.500   1.5052   0.04765   0.04041  -0.1061   0.0032   0.7640
  12.750   1.5113   0.04952   0.04240  -0.1047   0.0028   0.7658
  13.000   1.5176   0.05142   0.04439  -0.1035   0.0027   0.7676
  13.250   1.5225   0.05349   0.04657  -0.1022   0.0025   0.7694
  13.500   1.5268   0.05565   0.04884  -0.1010   0.0024   0.7713
  13.750   1.5297   0.05800   0.05130  -0.0998   0.0023   0.7732
  14.000   1.5324   0.06042   0.05386  -0.0987   0.0022   0.7750
  14.250   1.5354   0.06287   0.05641  -0.0977   0.0021   0.7769
  14.500   1.5382   0.06538   0.05904  -0.0969   0.0021   0.7787
  14.750   1.5403   0.06802   0.06181  -0.0961   0.0020   0.7805
  15.000   1.5414   0.07081   0.06473  -0.0953   0.0020   0.7825
  15.250   1.5417   0.07375   0.06780  -0.0947   0.0020   0.7847
  15.500   1.5415   0.07684   0.07102  -0.0942   0.0019   0.7870
  15.750   1.5402   0.08011   0.07441  -0.0938   0.0019   0.7893
  16.000   1.5375   0.08363   0.07808  -0.0936   0.0018   0.7916
  16.250   1.5347   0.08724   0.08182  -0.0935   0.0018   0.7936
  16.500   1.5299   0.09117   0.08590  -0.0936   0.0017   0.7956
  16.750   1.5258   0.09509   0.08995  -0.0939   0.0017   0.7979
  17.000   1.5205   0.09928   0.09429  -0.0944   0.0017   0.8003
  17.250   1.5137   0.10376   0.09891  -0.0951   0.0016   0.8027
  17.500   1.5072   0.10830   0.10361  -0.0961   0.0016   0.8052
  18.000   1.4908   0.11813   0.11373  -0.0988   0.0016   0.8102
  18.250   1.4825   0.12324   0.11898  -0.1005   0.0016   0.8131
  18.500   1.4723   0.12880   0.12470  -0.1026   0.0015   0.8162
  18.750   1.4634   0.13424   0.13029  -0.1050   0.0015   0.8197
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