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FX 61-163 AIRFOIL (fx61163-il) Xfoil prediction polar at RE=1,000,000 Ncrit=0


Details Polar file
Airfoil: FX 61-163 AIRFOIL (fx61163-il)
Reynolds number: 1,000,000
Max Cl/Cd: 127.4 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx61163-il-1000000.txt
Download as CSV file: xf-fx61163-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.4123   0.13682   0.13513  -0.0297   1.0001   0.0086
 -13.250  -0.4106   0.13235   0.13067  -0.0315   1.0001   0.0090
 -13.000  -0.4106   0.12715   0.12549  -0.0335   1.0001   0.0094
 -12.750  -0.4125   0.11959   0.11795  -0.0367   1.0001   0.0101
 -12.500  -0.4144   0.11366   0.11203  -0.0392   1.0001   0.0101
 -12.250  -0.4186   0.10709   0.10548  -0.0419   1.0001   0.0102
 -11.750  -0.4550   0.08312   0.08143  -0.0547   1.0001   0.0102
 -11.500  -0.4770   0.07490   0.07312  -0.0603   1.0001   0.0102
 -11.250  -0.4979   0.06858   0.06670  -0.0640   1.0001   0.0102
 -11.000  -0.5185   0.06342   0.06145  -0.0662   1.0001   0.0102
 -10.750  -0.5386   0.05906   0.05699  -0.0673   1.0001   0.0102
 -10.500  -0.5481   0.05363   0.05138  -0.0722   0.9901   0.0102
 -10.250  -0.5400   0.04703   0.04444  -0.0829   0.9486   0.0102
  -9.000  -0.4915   0.00909   0.00394  -0.0867   0.7105   0.0076
  -8.750  -0.4734   0.00752   0.00217  -0.0858   0.6996   0.0076
  -8.500  -0.4540   0.00641   0.00092  -0.0850   0.6900   0.0078
  -8.250  -0.4334   0.00564   0.00006  -0.0845   0.6815   0.0079
  -8.000  -0.4116   0.00515  -0.00051  -0.0843   0.6740   0.0082
  -7.750  -0.3896   0.00466  -0.00108  -0.0840   0.6673   0.0085
  -7.500  -0.3850   0.01587   0.00981  -0.0867   0.6699   0.0086
  -7.250  -0.3608   0.01524   0.00910  -0.0866   0.6633   0.0088
  -7.000  -0.3359   0.01462   0.00842  -0.0867   0.6579   0.0090
  -6.750  -0.3104   0.01400   0.00774  -0.0869   0.6527   0.0091
  -6.500  -0.2845   0.01345   0.00711  -0.0872   0.6479   0.0093
  -6.250  -0.2575   0.01295   0.00655  -0.0877   0.6436   0.0096
  -6.000  -0.2298   0.01254   0.00609  -0.0882   0.6393   0.0099
  -5.750  -0.2018   0.01216   0.00565  -0.0887   0.6350   0.0101
  -5.500  -0.1737   0.01163   0.00503  -0.0894   0.6309   0.0104
  -5.250  -0.1444   0.01106   0.00439  -0.0903   0.6277   0.0111
  -5.000  -0.1149   0.01074   0.00405  -0.0910   0.6240   0.0121
  -4.750  -0.0855   0.01050   0.00376  -0.0917   0.6202   0.0134
  -4.500  -0.0559   0.01024   0.00344  -0.0924   0.6166   0.0164
  -4.250  -0.0246   0.00964   0.00305  -0.0938   0.6136   0.0655
  -4.000   0.0109   0.00841   0.00250  -0.0971   0.6105   0.2442
  -3.750   0.0508   0.00713   0.00199  -0.1015   0.6073   0.4624
  -3.500   0.0839   0.00685   0.00189  -0.1030   0.6043   0.5313
  -3.250   0.1150   0.00681   0.00190  -0.1038   0.6010   0.5695
  -3.000   0.1456   0.00681   0.00193  -0.1045   0.5982   0.5902
  -2.750   0.1758   0.00687   0.00199  -0.1049   0.5950   0.6070
  -2.500   0.2057   0.00695   0.00205  -0.1053   0.5916   0.6186
  -2.250   0.2355   0.00705   0.00208  -0.1058   0.5884   0.6256
  -2.000   0.2652   0.00712   0.00209  -0.1062   0.5853   0.6293
  -1.750   0.2951   0.00713   0.00211  -0.1067   0.5831   0.6321
  -1.500   0.3249   0.00716   0.00213  -0.1071   0.5804   0.6355
  -1.250   0.3548   0.00721   0.00214  -0.1076   0.5775   0.6393
  -1.000   0.3847   0.00727   0.00215  -0.1081   0.5746   0.6425
  -0.750   0.4139   0.00733   0.00218  -0.1084   0.5715   0.6455
  -0.500   0.4434   0.00737   0.00223  -0.1088   0.5684   0.6483
  -0.250   0.4731   0.00740   0.00226  -0.1093   0.5650   0.6512
   0.000   0.5028   0.00744   0.00228  -0.1097   0.5617   0.6538
   0.250   0.5324   0.00750   0.00230  -0.1102   0.5587   0.6560
   0.500   0.5618   0.00757   0.00233  -0.1106   0.5554   0.6582
   0.750   0.5913   0.00757   0.00237  -0.1110   0.5528   0.6603
   1.000   0.6207   0.00760   0.00241  -0.1114   0.5495   0.6623
   1.250   0.6500   0.00764   0.00245  -0.1118   0.5461   0.6644
   1.500   0.6792   0.00771   0.00251  -0.1122   0.5427   0.6665
   1.750   0.7085   0.00778   0.00257  -0.1126   0.5392   0.6687
   2.000   0.7381   0.00781   0.00261  -0.1131   0.5350   0.6707
   2.250   0.7674   0.00784   0.00264  -0.1135   0.5304   0.6725
   2.500   0.7961   0.00791   0.00269  -0.1138   0.5262   0.6745
   2.750   0.8253   0.00793   0.00276  -0.1142   0.5223   0.6762
   3.000   0.8543   0.00796   0.00282  -0.1145   0.5171   0.6780
   3.500   0.9120   0.00808   0.00296  -0.1151   0.5056   0.6818
   3.750   0.9405   0.00817   0.00303  -0.1154   0.4981   0.6837
   4.000   0.9694   0.00823   0.00310  -0.1158   0.4897   0.6853
   4.250   0.9976   0.00834   0.00318  -0.1160   0.4805   0.6866
   4.500   1.0258   0.00840   0.00325  -0.1163   0.4700   0.6886
   4.750   1.0539   0.00850   0.00337  -0.1165   0.4601   0.6902
   5.000   1.0814   0.00864   0.00350  -0.1166   0.4494   0.6919
   5.250   1.1087   0.00880   0.00364  -0.1167   0.4380   0.6934
   5.500   1.1362   0.00894   0.00380  -0.1168   0.4270   0.6950
   5.750   1.1632   0.00913   0.00397  -0.1168   0.4144   0.6968
   6.000   1.1886   0.00945   0.00420  -0.1166   0.3933   0.6985
   6.250   1.2136   0.00979   0.00445  -0.1164   0.3687   0.7001
   6.500   1.2385   0.01015   0.00472  -0.1161   0.3489   0.7014
   6.750   1.2635   0.01045   0.00498  -0.1159   0.3289   0.7034
   7.000   1.2867   0.01089   0.00532  -0.1154   0.3024   0.7051
   7.250   1.3072   0.01153   0.00578  -0.1144   0.2656   0.7068
   7.500   1.3258   0.01229   0.00632  -0.1132   0.2250   0.7085
   7.750   1.3431   0.01312   0.00694  -0.1118   0.1859   0.7102
   8.000   1.3603   0.01391   0.00756  -0.1103   0.1540   0.7119
   8.250   1.3769   0.01470   0.00819  -0.1088   0.1265   0.7136
   8.500   1.3932   0.01546   0.00882  -0.1073   0.1025   0.7151
   9.250   1.4322   0.01787   0.01096  -0.1010   0.0492   0.7198
   9.500   1.4417   0.01863   0.01169  -0.0983   0.0378   0.7215
   9.750   1.4484   0.01964   0.01265  -0.0954   0.0259   0.7234
  10.000   1.4578   0.02055   0.01355  -0.0931   0.0201   0.7251
  10.250   1.4658   0.02159   0.01460  -0.0907   0.0151   0.7268
  10.500   1.4726   0.02278   0.01580  -0.0885   0.0107   0.7285
  10.750   1.4764   0.02430   0.01732  -0.0863   0.0057   0.7300
  11.000   1.4823   0.02582   0.01888  -0.0847   0.0042   0.7315
  11.250   1.4903   0.02733   0.02047  -0.0835   0.0038   0.7335
  11.500   1.4974   0.02901   0.02225  -0.0825   0.0035   0.7355
  11.750   1.5037   0.03087   0.02419  -0.0816   0.0033   0.7374
  12.000   1.5089   0.03289   0.02630  -0.0808   0.0030   0.7392
  12.250   1.5131   0.03506   0.02855  -0.0801   0.0029   0.7410
  12.500   1.5162   0.03739   0.03098  -0.0794   0.0028   0.7428
  12.750   1.5200   0.03965   0.03332  -0.0788   0.0027   0.7445
  13.000   1.5228   0.04203   0.03578  -0.0783   0.0027   0.7460
  13.250   1.5244   0.04457   0.03842  -0.0778   0.0026   0.7481
  13.500   1.5244   0.04728   0.04124  -0.0772   0.0026   0.7502
  13.750   1.5239   0.05005   0.04410  -0.0767   0.0026   0.7523
  14.000   1.5231   0.05291   0.04705  -0.0763   0.0025   0.7544
  14.250   1.5212   0.05596   0.05020  -0.0760   0.0025   0.7565
  14.500   1.5184   0.05916   0.05351  -0.0758   0.0025   0.7584
  14.750   1.5161   0.06239   0.05683  -0.0756   0.0024   0.7602
  15.000   1.5133   0.06577   0.06031  -0.0756   0.0024   0.7624
  15.250   1.5093   0.06937   0.06402  -0.0758   0.0024   0.7647
  15.500   1.5045   0.07311   0.06787  -0.0760   0.0023   0.7669
  15.750   1.4993   0.07700   0.07186  -0.0763   0.0023   0.7693
  16.000   1.4939   0.08099   0.07596  -0.0768   0.0023   0.7718
  16.250   1.4876   0.08518   0.08024  -0.0773   0.0023   0.7742
  16.500   1.4814   0.08938   0.08455  -0.0780   0.0023   0.7767
  16.750   1.4746   0.09377   0.08906  -0.0789   0.0023   0.7795
  17.000   1.4674   0.09828   0.09368  -0.0798   0.0022   0.7826
  17.250   1.4587   0.10312   0.09863  -0.0810   0.0022   0.7860
  17.500   1.4499   0.10797   0.10360  -0.0823   0.0022   0.7894
  17.750   1.4414   0.11286   0.10861  -0.0837   0.0022   0.7932
  18.000   1.4338   0.11770   0.11356  -0.0853   0.0022   0.7977
  18.250   1.4251   0.12281   0.11878  -0.0871   0.0022   0.8026
  18.500   1.4157   0.12810   0.12420  -0.0891   0.0022   0.8077
  18.750   1.4083   0.13307   0.12928  -0.0912   0.0021   0.8145
  19.000   1.4003   0.13825   0.13458  -0.0934   0.0021   0.8223
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