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GOE 364 AIRFOIL (goe364-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 364 AIRFOIL (goe364-il)
Reynolds number: 1,000,000
Max Cl/Cd: 133.36 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe364-il-1000000.txt
Download as CSV file: xf-goe364-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 364 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.2479   0.12818   0.12653  -0.0314   1.0000   0.0129
 -11.500  -0.2452   0.12559   0.12395  -0.0314   1.0000   0.0133
 -11.250  -0.2414   0.12224   0.12061  -0.0325   0.9998   0.0138
 -11.000  -0.2286   0.11802   0.11639  -0.0369   0.9989   0.0139
 -10.750  -0.2167   0.11359   0.11197  -0.0416   0.9974   0.0139
 -10.500  -0.2024   0.10921   0.10759  -0.0442   0.9952   0.0141
 -10.250  -0.1875   0.10607   0.10445  -0.0464   0.9919   0.0142
 -10.000  -0.1720   0.10296   0.10134  -0.0492   0.9882   0.0144
  -9.750  -0.1554   0.09954   0.09792  -0.0528   0.9843   0.0145
  -9.500  -0.1413   0.09630   0.09467  -0.0557   0.9768   0.0147
  -9.250  -0.1224   0.09266   0.09104  -0.0601   0.9712   0.0151
  -9.000  -0.1018   0.08794   0.08628  -0.0669   0.9614   0.0167
  -8.750  -0.0725   0.08170   0.08001  -0.0791   0.9506   0.0168
  -8.500  -0.0399   0.07571   0.07395  -0.0892   0.9320   0.0169
  -8.250  -0.0045   0.07218   0.07025  -0.0953   0.8890   0.0171
  -8.000   0.0033   0.07045   0.06822  -0.0954   0.8296   0.0173
  -7.750   0.0053   0.06881   0.06646  -0.0946   0.8011   0.0174
  -7.500   0.0069   0.06731   0.06488  -0.0937   0.7820   0.0180
  -7.250   0.0060   0.06517   0.06269  -0.0938   0.7668   0.0181
  -7.000   0.0120   0.06273   0.06021  -0.0952   0.7541   0.0191
  -6.750   0.0159   0.05737   0.05476  -0.1019   0.7430   0.0200
  -6.500   0.0273   0.05351   0.05081  -0.1047   0.7331   0.0200
  -6.250   0.0363   0.04934   0.04658  -0.1065   0.7247   0.0202
  -6.000   0.0507   0.04772   0.04490  -0.1064   0.7157   0.0204
  -5.750   0.0675   0.04574   0.04286  -0.1071   0.7080   0.0206
  -5.500   0.0855   0.04386   0.04092  -0.1077   0.7001   0.0210
  -5.250   0.1049   0.04171   0.03870  -0.1087   0.6932   0.0218
  -5.000   0.1319   0.03508   0.03174  -0.1119   0.6870   0.0237
  -4.750   0.1349   0.01645   0.01317  -0.1044   0.6682   0.0240
  -4.500   0.1669   0.02996   0.02639  -0.1119   0.6739   0.0243
  -4.250   0.1886   0.02871   0.02506  -0.1117   0.6670   0.0246
  -4.000   0.2112   0.02733   0.02357  -0.1115   0.6605   0.0253
  -3.750   0.2314   0.02111   0.01671  -0.1100   0.6551   0.0282
  -3.250   0.2784   0.01941   0.01490  -0.1092   0.6409   0.0289
  -3.000   0.3023   0.01858   0.01395  -0.1087   0.6329   0.0295
  -2.750   0.3296   0.01806   0.01308  -0.1076   0.6248   0.0326
  -2.500   0.3498   0.01538   0.01011  -0.1065   0.6167   0.0335
  -2.250   0.3749   0.01468   0.00937  -0.1061   0.6077   0.0340
  -0.750   0.5284   0.01051   0.00415  -0.1017   0.5412   0.0336
  -0.500   0.5544   0.01036   0.00389  -0.1010   0.5259   0.0331
  -0.250   0.5801   0.01024   0.00369  -0.1004   0.5099   0.0329
   0.000   0.6048   0.00983   0.00320  -0.0997   0.4950   0.0332
   0.250   0.6294   0.00957   0.00288  -0.0989   0.4817   0.0336
   0.500   0.6542   0.00943   0.00268  -0.0982   0.4700   0.0339
   0.750   0.6797   0.00931   0.00254  -0.0976   0.4606   0.0344
   1.000   0.7050   0.00926   0.00245  -0.0969   0.4526   0.0350
   1.250   0.7308   0.00920   0.00237  -0.0964   0.4455   0.0355
   1.500   0.7561   0.00920   0.00233  -0.0958   0.4385   0.0360
   1.750   0.7824   0.00916   0.00229  -0.0953   0.4331   0.0368
   2.000   0.8082   0.00918   0.00228  -0.0949   0.4273   0.0379
   2.250   0.8336   0.00922   0.00228  -0.0943   0.4215   0.0389
   2.500   0.8598   0.00919   0.00226  -0.0939   0.4164   0.0407
   2.750   0.8856   0.00923   0.00229  -0.0933   0.4106   0.0431
   3.000   0.9110   0.00932   0.00234  -0.0928   0.4052   0.0468
   3.250   0.9301   0.00852   0.00258  -0.0914   0.4012   0.5473
   3.500   1.0114   0.00788   0.00285  -0.1035   0.3929   1.0000
   3.750   1.0359   0.00801   0.00294  -0.1028   0.3876   1.0000
   4.000   1.0609   0.00811   0.00302  -0.1022   0.3819   1.0000
   4.250   1.0847   0.00827   0.00313  -0.1014   0.3752   1.0000
   4.500   1.1095   0.00838   0.00323  -0.1007   0.3693   1.0000
   4.750   1.1336   0.00852   0.00334  -0.1000   0.3620   1.0000
   5.000   1.1576   0.00868   0.00346  -0.0992   0.3543   1.0000
   5.250   1.1809   0.00886   0.00360  -0.0984   0.3437   1.0000
   5.500   1.2040   0.00905   0.00374  -0.0975   0.3306   1.0000
   5.750   1.2255   0.00933   0.00392  -0.0963   0.3127   1.0000
   6.000   1.2461   0.00965   0.00413  -0.0950   0.2926   1.0000
   6.250   1.2662   0.01000   0.00438  -0.0937   0.2750   1.0000
   6.500   1.2866   0.01032   0.00463  -0.0923   0.2621   1.0000
   6.750   1.3065   0.01066   0.00490  -0.0910   0.2512   1.0000
   7.000   1.3279   0.01091   0.00513  -0.0898   0.2439   1.0000
   7.250   1.3477   0.01123   0.00541  -0.0885   0.2368   1.0000
   7.500   1.3694   0.01144   0.00564  -0.0874   0.2324   1.0000
   7.750   1.3898   0.01171   0.00589  -0.0862   0.2276   1.0000
   8.000   1.4086   0.01204   0.00620  -0.0846   0.2220   1.0000
   8.250   1.4298   0.01225   0.00644  -0.0835   0.2188   1.0000
   8.500   1.4485   0.01252   0.00671  -0.0820   0.2138   1.0000
   8.750   1.4643   0.01285   0.00703  -0.0799   0.2086   1.0000
   9.000   1.4822   0.01311   0.00730  -0.0782   0.2046   1.0000
   9.250   1.5006   0.01336   0.00757  -0.0767   0.2007   1.0000
   9.500   1.5176   0.01368   0.00790  -0.0749   0.1968   1.0000
   9.750   1.5331   0.01409   0.00830  -0.0730   0.1916   1.0000
  10.000   1.5526   0.01433   0.00859  -0.0718   0.1882   1.0000
  10.250   1.5699   0.01468   0.00894  -0.0703   0.1832   1.0000
  10.500   1.5848   0.01515   0.00939  -0.0684   0.1768   1.0000
  10.750   1.6025   0.01550   0.00977  -0.0671   0.1712   1.0000
  11.000   1.6163   0.01605   0.01030  -0.0652   0.1640   1.0000
  11.250   1.6319   0.01653   0.01079  -0.0637   0.1565   1.0000
  11.500   1.6442   0.01720   0.01142  -0.0618   0.1479   1.0000
  11.750   1.6547   0.01799   0.01218  -0.0597   0.1379   1.0000
  12.000   1.6650   0.01882   0.01299  -0.0578   0.1285   1.0000
  12.250   1.6730   0.01983   0.01397  -0.0557   0.1188   1.0000
  12.500   1.6799   0.02098   0.01509  -0.0537   0.1101   1.0000
  12.750   1.6841   0.02237   0.01644  -0.0516   0.1005   1.0000
  13.000   1.6892   0.02378   0.01784  -0.0498   0.0921   1.0000
  13.250   1.6938   0.02530   0.01936  -0.0482   0.0843   1.0000
  13.500   1.6961   0.02710   0.02114  -0.0465   0.0764   1.0000
  13.750   1.6951   0.02924   0.02325  -0.0449   0.0666   1.0000
  14.000   1.6888   0.03193   0.02588  -0.0433   0.0537   1.0000
  14.250   1.6648   0.03640   0.03023  -0.0412   0.0330   1.0000
  14.500   1.6437   0.04090   0.03471  -0.0398   0.0202   1.0000
  14.750   1.6376   0.04406   0.03794  -0.0391   0.0173   1.0000
  15.000   1.6331   0.04717   0.04112  -0.0386   0.0159   1.0000
  15.250   1.6268   0.05057   0.04460  -0.0382   0.0148   1.0000
  15.500   1.6236   0.05370   0.04782  -0.0380   0.0141   1.0000
  15.750   1.6204   0.05691   0.05113  -0.0380   0.0138   1.0000
  16.000   1.6156   0.06040   0.05471  -0.0381   0.0133   1.0000
  16.250   1.6093   0.06414   0.05854  -0.0383   0.0129   1.0000
  16.500   1.5995   0.06843   0.06292  -0.0387   0.0123   1.0000
  16.750   1.5890   0.07291   0.06751  -0.0393   0.0120   1.0000
  17.000   1.5751   0.07793   0.07265  -0.0401   0.0116   1.0000
  17.250   1.5682   0.08203   0.07685  -0.0407   0.0115   1.0000
  17.500   1.5596   0.08641   0.08133  -0.0415   0.0113   1.0000
  17.750   1.5505   0.09092   0.08593  -0.0425   0.0111   1.0000
  18.000   1.5393   0.09576   0.09089  -0.0435   0.0109   1.0000
  18.250   1.5273   0.10076   0.09598  -0.0448   0.0107   1.0000
  18.500   1.5161   0.10573   0.10105  -0.0461   0.0106   1.0000
  18.750   1.5035   0.11100   0.10642  -0.0476   0.0104   1.0000
  19.000   1.4909   0.11633   0.11185  -0.0493   0.0103   1.0000
  19.250   1.4787   0.12166   0.11728  -0.0511   0.0101   1.0000
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