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FX 61-163 AIRFOIL (fx61163-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 61-163 AIRFOIL (fx61163-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.71 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx61163-il-1000000-n5.txt
Download as CSV file: xf-fx61163-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 61-163 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.7146   0.07490   0.07275  -0.0548   1.0001   0.0034
 -14.250  -0.7547   0.06370   0.06129  -0.0616   1.0001   0.0034
 -14.000  -0.7750   0.05714   0.05456  -0.0650   1.0001   0.0034
 -13.750  -0.7896   0.05216   0.04943  -0.0671   1.0001   0.0034
 -13.500  -0.8006   0.04807   0.04520  -0.0683   1.0001   0.0034
 -13.250  -0.8083   0.04466   0.04166  -0.0689   1.0001   0.0034
 -13.000  -0.8142   0.04167   0.03854  -0.0690   1.0001   0.0034
 -12.750  -0.8183   0.03904   0.03579  -0.0687   1.0001   0.0035
 -12.500  -0.8152   0.03642   0.03303  -0.0695   0.9990   0.0035
 -12.250  -0.8115   0.03406   0.03055  -0.0696   0.9886   0.0035
 -12.000  -0.7533   0.03052   0.02672  -0.0821   0.9393   0.0036
 -11.750  -0.7278   0.02878   0.02440  -0.0855   0.8253   0.0037
 -11.500  -0.7187   0.02747   0.02281  -0.0848   0.7845   0.0038
 -11.250  -0.7072   0.02620   0.02133  -0.0844   0.7564   0.0038
 -11.000  -0.6938   0.02502   0.01996  -0.0839   0.7344   0.0039
 -10.750  -0.6791   0.02387   0.01864  -0.0836   0.7170   0.0040
 -10.500  -0.6630   0.02283   0.01745  -0.0833   0.7029   0.0041
 -10.250  -0.6462   0.02185   0.01633  -0.0829   0.6909   0.0042
 -10.000  -0.6298   0.02097   0.01533  -0.0824   0.6806   0.0043
  -9.750  -0.6104   0.02013   0.01437  -0.0823   0.6719   0.0044
  -9.500  -0.5894   0.01935   0.01348  -0.0824   0.6634   0.0045
  -9.250  -0.5674   0.01858   0.01260  -0.0826   0.6563   0.0046
  -9.000  -0.5446   0.01787   0.01179  -0.0829   0.6492   0.0047
  -8.750  -0.5209   0.01723   0.01106  -0.0833   0.6436   0.0048
  -8.500  -0.4967   0.01662   0.01037  -0.0836   0.6384   0.0048
  -8.250  -0.4723   0.01606   0.00974  -0.0838   0.6334   0.0049
  -8.000  -0.4474   0.01555   0.00916  -0.0841   0.6292   0.0050
  -7.750  -0.4231   0.01480   0.00833  -0.0844   0.6250   0.0051
  -7.500  -0.3982   0.01412   0.00758  -0.0848   0.6206   0.0052
  -7.000  -0.3451   0.01315   0.00650  -0.0858   0.6131   0.0056
  -6.750  -0.3175   0.01277   0.00609  -0.0863   0.6098   0.0058
  -6.500  -0.2897   0.01243   0.00571  -0.0868   0.6065   0.0061
  -6.250  -0.2617   0.01208   0.00531  -0.0874   0.6033   0.0063
  -6.000  -0.2334   0.01176   0.00494  -0.0879   0.6002   0.0065
  -5.750  -0.2045   0.01146   0.00460  -0.0886   0.5974   0.0068
  -5.500  -0.1755   0.01119   0.00430  -0.0892   0.5943   0.0071
  -5.250  -0.1464   0.01095   0.00402  -0.0898   0.5913   0.0074
  -5.000  -0.1171   0.01069   0.00372  -0.0904   0.5883   0.0081
  -4.750  -0.0879   0.01050   0.00350  -0.0910   0.5851   0.0091
  -4.500  -0.0582   0.01031   0.00330  -0.0917   0.5824   0.0103
  -4.250  -0.0283   0.01010   0.00309  -0.0924   0.5795   0.0147
  -4.000   0.0018   0.00983   0.00289  -0.0933   0.5765   0.0322
  -3.750   0.0323   0.00952   0.00268  -0.0943   0.5737   0.0634
  -3.500   0.0647   0.00893   0.00238  -0.0961   0.5710   0.1545
  -3.250   0.1036   0.00767   0.00188  -0.1002   0.5687   0.3675
  -3.000   0.1400   0.00703   0.00166  -0.1029   0.5659   0.4945
  -2.750   0.1725   0.00683   0.00161  -0.1042   0.5623   0.5478
  -2.500   0.2033   0.00680   0.00162  -0.1050   0.5586   0.5772
  -2.250   0.2333   0.00683   0.00163  -0.1055   0.5553   0.5892
  -2.000   0.2635   0.00684   0.00161  -0.1060   0.5530   0.5948
  -1.750   0.2935   0.00686   0.00160  -0.1065   0.5506   0.5985
  -1.500   0.3235   0.00688   0.00161  -0.1070   0.5478   0.6029
  -1.250   0.3533   0.00691   0.00161  -0.1075   0.5447   0.6079
  -1.000   0.3830   0.00696   0.00161  -0.1079   0.5418   0.6123
  -0.750   0.4128   0.00699   0.00164  -0.1084   0.5393   0.6159
  -0.500   0.4426   0.00702   0.00166  -0.1089   0.5358   0.6196
  -0.250   0.4723   0.00706   0.00168  -0.1094   0.5316   0.6230
   0.000   0.5018   0.00711   0.00169  -0.1098   0.5276   0.6257
   0.250   0.5314   0.00715   0.00171  -0.1102   0.5248   0.6279
   0.500   0.5611   0.00718   0.00175  -0.1107   0.5219   0.6302
   0.750   0.5907   0.00722   0.00180  -0.1112   0.5183   0.6325
   1.000   0.6200   0.00727   0.00184  -0.1116   0.5143   0.6348
   1.250   0.6493   0.00733   0.00188  -0.1120   0.5105   0.6370
   1.500   0.6789   0.00738   0.00193  -0.1124   0.5069   0.6393
   1.750   0.7082   0.00743   0.00197  -0.1128   0.5021   0.6414
   2.000   0.7371   0.00751   0.00203  -0.1132   0.4964   0.6433
   2.250   0.7664   0.00755   0.00210  -0.1136   0.4903   0.6452
   2.500   0.7953   0.00763   0.00217  -0.1139   0.4843   0.6471
   2.750   0.8242   0.00771   0.00225  -0.1143   0.4790   0.6490
   3.000   0.8530   0.00780   0.00232  -0.1146   0.4708   0.6510
   3.250   0.8815   0.00790   0.00242  -0.1149   0.4615   0.6530
   3.500   0.9097   0.00803   0.00251  -0.1151   0.4516   0.6547
   3.750   0.9375   0.00819   0.00262  -0.1153   0.4379   0.6562
   4.000   0.9649   0.00838   0.00276  -0.1154   0.4215   0.6577
   4.250   0.9920   0.00858   0.00292  -0.1154   0.4051   0.6594
   4.500   1.0189   0.00881   0.00310  -0.1155   0.3879   0.6610
   4.750   1.0458   0.00904   0.00329  -0.1155   0.3729   0.6626
   5.000   1.0725   0.00927   0.00348  -0.1155   0.3588   0.6642
   5.250   1.0992   0.00950   0.00368  -0.1155   0.3463   0.6657
   5.500   1.1259   0.00973   0.00389  -0.1155   0.3353   0.6674
   5.750   1.1523   0.00997   0.00410  -0.1155   0.3221   0.6691
   6.000   1.1759   0.01044   0.00443  -0.1150   0.2929   0.6706
   6.250   1.1974   0.01106   0.00485  -0.1143   0.2532   0.6721
   6.500   1.2184   0.01170   0.00531  -0.1134   0.2185   0.6737
   6.750   1.2391   0.01233   0.00580  -0.1125   0.1857   0.6753
   7.000   1.2602   0.01291   0.00627  -0.1117   0.1615   0.6769
   7.250   1.2775   0.01374   0.00689  -0.1103   0.1254   0.6784
   7.500   1.2943   0.01457   0.00754  -0.1088   0.0939   0.6800
   7.750   1.3110   0.01536   0.00818  -0.1073   0.0684   0.6817
   8.000   1.3288   0.01602   0.00878  -0.1059   0.0531   0.6832
   8.250   1.3480   0.01656   0.00929  -0.1048   0.0434   0.6845
   8.500   1.3612   0.01742   0.01004  -0.1027   0.0268   0.6857
   8.750   1.3760   0.01806   0.01067  -0.1009   0.0200   0.6870
   9.000   1.3888   0.01866   0.01128  -0.0987   0.0160   0.6886
   9.250   1.4029   0.01929   0.01194  -0.0968   0.0132   0.6902
   9.500   1.4158   0.02000   0.01268  -0.0948   0.0100   0.6916
   9.750   1.4245   0.02096   0.01365  -0.0925   0.0049   0.6931
  10.000   1.4327   0.02201   0.01473  -0.0902   0.0028   0.6945
  10.250   1.4435   0.02297   0.01575  -0.0885   0.0025   0.6959
  10.500   1.4537   0.02407   0.01690  -0.0869   0.0022   0.6975
  10.750   1.4632   0.02529   0.01818  -0.0855   0.0021   0.6991
  11.000   1.4724   0.02665   0.01961  -0.0843   0.0019   0.7005
  11.250   1.4805   0.02819   0.02123  -0.0832   0.0018   0.7019
  11.500   1.4891   0.02979   0.02292  -0.0824   0.0017   0.7033
  11.750   1.4973   0.03150   0.02471  -0.0816   0.0017   0.7048
  12.000   1.5045   0.03334   0.02663  -0.0810   0.0017   0.7062
  12.250   1.5110   0.03528   0.02866  -0.0804   0.0016   0.7077
  12.500   1.5164   0.03739   0.03084  -0.0798   0.0016   0.7092
  12.750   1.5208   0.03958   0.03311  -0.0793   0.0015   0.7108
  13.000   1.5243   0.04188   0.03550  -0.0787   0.0015   0.7124
  13.250   1.5268   0.04430   0.03799  -0.0782   0.0014   0.7140
  13.500   1.5282   0.04685   0.04063  -0.0776   0.0014   0.7155
  13.750   1.5289   0.04947   0.04333  -0.0772   0.0013   0.7168
  14.000   1.5295   0.05214   0.04609  -0.0768   0.0013   0.7183
  14.250   1.5291   0.05500   0.04904  -0.0764   0.0013   0.7198
  14.500   1.5280   0.05798   0.05212  -0.0762   0.0012   0.7214
  14.750   1.5270   0.06100   0.05523  -0.0760   0.0012   0.7230
  15.000   1.5251   0.06421   0.05853  -0.0759   0.0012   0.7246
  15.250   1.5226   0.06757   0.06198  -0.0760   0.0012   0.7262
  15.500   1.5192   0.07107   0.06557  -0.0761   0.0012   0.7278
  15.750   1.5152   0.07470   0.06929  -0.0763   0.0011   0.7293
  16.000   1.5117   0.07835   0.07303  -0.0766   0.0011   0.7307
  16.250   1.5065   0.08231   0.07710  -0.0771   0.0011   0.7324
  16.500   1.5019   0.08623   0.08112  -0.0776   0.0011   0.7343
  16.750   1.4954   0.09047   0.08547  -0.0783   0.0011   0.7362
  17.000   1.4889   0.09478   0.08989  -0.0791   0.0011   0.7382
  17.250   1.4805   0.09946   0.09467  -0.0802   0.0011   0.7402
  17.500   1.4724   0.10415   0.09947  -0.0813   0.0010   0.7422
  17.750   1.4635   0.10899   0.10442  -0.0826   0.0010   0.7440
  18.000   1.4550   0.11385   0.10938  -0.0840   0.0010   0.7458
  18.250   1.4457   0.11897   0.11461  -0.0857   0.0010   0.7477
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