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GOE 646 AIRFOIL (goe646-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 646 AIRFOIL (goe646-il)
Reynolds number: 500,000
Max Cl/Cd: 95.93 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe646-il-500000.txt
Download as CSV file: xf-goe646-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 646 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.8181   0.10661   0.10281  -0.0766   1.0000   0.0407
 -19.250  -0.8367   0.10035   0.09641  -0.0800   1.0000   0.0409
 -19.000  -0.8510   0.09506   0.09100  -0.0827   1.0000   0.0412
 -18.750  -0.8478   0.09288   0.08884  -0.0831   1.0000   0.0417
 -18.500  -0.8473   0.09011   0.08606  -0.0840   1.0000   0.0421
 -18.250  -0.8483   0.08712   0.08304  -0.0851   1.0000   0.0424
 -18.000  -0.8510   0.08388   0.07977  -0.0864   1.0000   0.0429
 -17.750  -0.8550   0.08048   0.07633  -0.0877   1.0000   0.0433
 -17.500  -0.8599   0.07705   0.07285  -0.0890   1.0000   0.0437
 -17.250  -0.8661   0.07352   0.06925  -0.0903   1.0000   0.0442
 -17.000  -0.8731   0.06998   0.06564  -0.0916   1.0000   0.0447
 -16.750  -0.8796   0.06666   0.06224  -0.0926   1.0000   0.0450
 -16.500  -0.8864   0.06346   0.05897  -0.0935   1.0000   0.0453
 -16.250  -0.8955   0.06012   0.05553  -0.0944   1.0000   0.0457
 -16.000  -0.9013   0.05766   0.05304  -0.0942   1.0000   0.0461
 -15.750  -0.9057   0.05576   0.05117  -0.0933   1.0000   0.0465
 -15.500  -0.9161   0.05342   0.04883  -0.0924   1.0000   0.0469
 -15.250  -0.9319   0.05115   0.04655  -0.0908   1.0000   0.0471
 -15.000  -0.9307   0.04825   0.04361  -0.0930   0.9987   0.0476
 -14.750  -0.9177   0.04501   0.04032  -0.0975   0.9961   0.0484
 -14.500  -0.9030   0.04196   0.03718  -0.1021   0.9934   0.0491
 -14.250  -0.8901   0.03888   0.03400  -0.1063   0.9901   0.0501
 -14.000  -0.8756   0.03602   0.03103  -0.1103   0.9860   0.0508
 -13.750  -0.8598   0.03306   0.02802  -0.1150   0.9825   0.0518
 -13.500  -0.8378   0.03024   0.02517  -0.1205   0.9800   0.0529
 -13.250  -0.8249   0.02784   0.02270  -0.1233   0.9718   0.0538
 -13.000  -0.7989   0.02564   0.02041  -0.1282   0.9683   0.0552
 -12.750  -0.7840   0.02389   0.01854  -0.1302   0.9604   0.0563
 -12.500  -0.7650   0.02234   0.01694  -0.1318   0.9554   0.0578
 -12.250  -0.7357   0.02120   0.01577  -0.1341   0.9531   0.0597
 -12.000  -0.7180   0.02041   0.01491  -0.1335   0.9458   0.0614
 -11.750  -0.6903   0.01950   0.01394  -0.1348   0.9422   0.0636
 -11.500  -0.6578   0.01862   0.01306  -0.1371   0.9397   0.0663
 -11.250  -0.6205   0.01801   0.01235  -0.1396   0.9379   0.0693
 -11.000  -0.6002   0.01724   0.01160  -0.1393   0.9314   0.0721
 -10.750  -0.5703   0.01673   0.01104  -0.1403   0.9268   0.0754
 -10.500  -0.5376   0.01604   0.01031  -0.1421   0.9232   0.0790
 -10.250  -0.5061   0.01557   0.00980  -0.1433   0.9188   0.0828
 -10.000  -0.4845   0.01515   0.00934  -0.1425   0.9118   0.0860
  -9.750  -0.4559   0.01465   0.00882  -0.1432   0.9068   0.0898
  -9.500  -0.4231   0.01434   0.00842  -0.1444   0.9025   0.0933
  -9.250  -0.4066   0.01390   0.00801  -0.1425   0.8953   0.0968
  -9.000  -0.3804   0.01359   0.00765  -0.1424   0.8896   0.1007
  -8.750  -0.3501   0.01322   0.00724  -0.1431   0.8846   0.1052
  -8.500  -0.3317   0.01295   0.00697  -0.1413   0.8776   0.1094
  -8.250  -0.3067   0.01269   0.00666  -0.1408   0.8714   0.1140
  -8.000  -0.2781   0.01236   0.00632  -0.1411   0.8661   0.1201
  -7.750  -0.2573   0.01212   0.00608  -0.1397   0.8596   0.1258
  -7.500  -0.2336   0.01184   0.00582  -0.1389   0.8532   0.1333
  -7.250  -0.2058   0.01157   0.00553  -0.1389   0.8476   0.1425
  -7.000  -0.1831   0.01135   0.00532  -0.1379   0.8410   0.1519
  -6.750  -0.1588   0.01114   0.00511  -0.1371   0.8339   0.1622
  -6.500  -0.1309   0.01091   0.00488  -0.1370   0.8276   0.1744
  -6.250  -0.1087   0.01071   0.00472  -0.1358   0.8196   0.1856
  -6.000  -0.0831   0.01054   0.00454  -0.1352   0.8119   0.1964
  -5.750  -0.0566   0.01042   0.00439  -0.1348   0.8044   0.2066
  -5.500  -0.0329   0.01026   0.00426  -0.1338   0.7954   0.2160
  -5.000   0.0182   0.01005   0.00401  -0.1325   0.7770   0.2337
  -4.500   0.0688   0.00990   0.00380  -0.1311   0.7560   0.2505
  -4.250   0.0945   0.00988   0.00370  -0.1304   0.7447   0.2584
  -4.000   0.1189   0.00981   0.00360  -0.1295   0.7320   0.2657
  -3.750   0.1432   0.00979   0.00354  -0.1285   0.7186   0.2732
  -3.500   0.1681   0.00980   0.00347  -0.1277   0.7060   0.2800
  -3.250   0.1923   0.00978   0.00342  -0.1268   0.6935   0.2873
  -3.000   0.2173   0.00981   0.00339  -0.1260   0.6820   0.2939
  -2.750   0.2421   0.00984   0.00334  -0.1252   0.6713   0.3003
  -2.500   0.2666   0.00985   0.00334  -0.1243   0.6606   0.3074
  -2.250   0.2918   0.00994   0.00334  -0.1236   0.6507   0.3146
  -2.000   0.3163   0.00994   0.00332  -0.1228   0.6410   0.3220
  -1.750   0.3416   0.01001   0.00334  -0.1221   0.6330   0.3290
  -1.500   0.3673   0.01006   0.00336  -0.1215   0.6255   0.3352
  -1.250   0.3924   0.01007   0.00334  -0.1208   0.6183   0.3415
  -1.000   0.4177   0.01010   0.00337  -0.1201   0.6114   0.3475
  -0.750   0.4432   0.01014   0.00338  -0.1194   0.6047   0.3534
  -0.500   0.4687   0.01019   0.00338  -0.1188   0.5985   0.3595
  -0.250   0.4946   0.01022   0.00342  -0.1183   0.5932   0.3662
   0.000   0.5199   0.01023   0.00345  -0.1176   0.5878   0.3725
   0.250   0.5456   0.01029   0.00347  -0.1170   0.5825   0.3785
   0.500   0.5713   0.01032   0.00351  -0.1165   0.5776   0.3862
   0.750   0.5974   0.01037   0.00357  -0.1160   0.5732   0.3938
   1.000   0.6224   0.01038   0.00360  -0.1153   0.5687   0.4013
   1.250   0.6470   0.01038   0.00365  -0.1145   0.5638   0.4101
   1.500   0.6724   0.01047   0.00370  -0.1139   0.5587   0.4188
   1.750   0.6976   0.01050   0.00377  -0.1133   0.5541   0.4288
   2.000   0.7215   0.01050   0.00383  -0.1124   0.5496   0.4396
   2.250   0.7453   0.01050   0.00389  -0.1114   0.5449   0.4520
   2.500   0.7693   0.01055   0.00395  -0.1106   0.5400   0.4664
   2.750   0.7931   0.01060   0.00405  -0.1097   0.5347   0.4857
   3.000   0.8135   0.01055   0.00413  -0.1080   0.5291   0.5104
   3.250   0.8327   0.01054   0.00421  -0.1062   0.5228   0.5422
   3.500   0.8527   0.01059   0.00433  -0.1045   0.5163   0.5785
   3.750   0.8700   0.01057   0.00444  -0.1022   0.5098   0.6125
   4.000   0.8885   0.01062   0.00455  -0.1002   0.5031   0.6416
   4.250   0.9079   0.01074   0.00469  -0.0984   0.4968   0.6664
   4.500   0.9270   0.01078   0.00482  -0.0965   0.4905   0.6881
   4.750   0.9453   0.01086   0.00495  -0.0945   0.4836   0.7092
   5.000   0.9633   0.01095   0.00510  -0.0925   0.4768   0.7330
   5.250   0.9798   0.01094   0.00526  -0.0901   0.4690   0.7680
   5.500   1.0071   0.01084   0.00550  -0.0900   0.4600   0.9017
   5.750   1.0619   0.01107   0.00575  -0.0959   0.4470   1.0000
   6.000   1.0792   0.01129   0.00593  -0.0940   0.4361   1.0000
   6.250   1.0939   0.01158   0.00614  -0.0916   0.4230   1.0000
   6.500   1.1087   0.01190   0.00639  -0.0892   0.4075   1.0000
   6.750   1.1231   0.01227   0.00669  -0.0869   0.3914   1.0000
   7.000   1.1357   0.01273   0.00705  -0.0843   0.3748   1.0000
   7.250   1.1493   0.01320   0.00744  -0.0820   0.3606   1.0000
   7.500   1.1627   0.01371   0.00788  -0.0798   0.3487   1.0000
   7.750   1.1767   0.01424   0.00834  -0.0776   0.3378   1.0000
   8.000   1.1927   0.01471   0.00878  -0.0759   0.3292   1.0000
   8.250   1.2075   0.01525   0.00928  -0.0740   0.3209   1.0000
   8.500   1.2233   0.01577   0.00978  -0.0724   0.3136   1.0000
   8.750   1.2398   0.01628   0.01027  -0.0709   0.3065   1.0000
   9.000   1.2524   0.01698   0.01092  -0.0689   0.2991   1.0000
   9.250   1.2714   0.01742   0.01139  -0.0678   0.2932   1.0000
   9.500   1.2860   0.01806   0.01201  -0.0663   0.2865   1.0000
   9.750   1.3003   0.01874   0.01267  -0.0647   0.2804   1.0000
  10.000   1.3178   0.01929   0.01325  -0.0636   0.2741   1.0000
  10.250   1.3312   0.02006   0.01399  -0.0620   0.2674   1.0000
  10.500   1.3463   0.02076   0.01470  -0.0607   0.2619   1.0000
  10.750   1.3622   0.02144   0.01540  -0.0596   0.2558   1.0000
  11.000   1.3740   0.02236   0.01629  -0.0581   0.2494   1.0000
  11.250   1.3891   0.02313   0.01710  -0.0569   0.2433   1.0000
  11.500   1.4027   0.02400   0.01798  -0.0557   0.2368   1.0000
  11.750   1.4126   0.02513   0.01908  -0.0542   0.2305   1.0000
  12.000   1.4277   0.02595   0.01995  -0.0533   0.2247   1.0000
  12.250   1.4376   0.02715   0.02113  -0.0519   0.2183   1.0000
  12.500   1.4490   0.02827   0.02227  -0.0508   0.2121   1.0000
  12.750   1.4600   0.02945   0.02347  -0.0497   0.2061   1.0000
  13.000   1.4667   0.03097   0.02496  -0.0484   0.2004   1.0000
  13.250   1.4790   0.03211   0.02616  -0.0475   0.1951   1.0000
  13.500   1.4871   0.03362   0.02767  -0.0464   0.1894   1.0000
  13.750   1.4935   0.03527   0.02933  -0.0454   0.1842   1.0000
  14.000   1.5030   0.03673   0.03083  -0.0445   0.1785   1.0000
  14.250   1.5071   0.03867   0.03277  -0.0435   0.1728   1.0000
  14.500   1.5146   0.04036   0.03449  -0.0427   0.1673   1.0000
  14.750   1.5188   0.04239   0.03654  -0.0419   0.1611   1.0000
  15.000   1.5218   0.04456   0.03872  -0.0411   0.1549   1.0000
  15.250   1.5250   0.04675   0.04093  -0.0404   0.1478   1.0000
  15.500   1.5262   0.04917   0.04337  -0.0398   0.1402   1.0000
  15.750   1.5229   0.05211   0.04629  -0.0391   0.1306   1.0000
  16.000   1.5191   0.05514   0.04930  -0.0386   0.1201   1.0000
  16.250   1.5129   0.05846   0.05259  -0.0381   0.1092   1.0000
  16.500   1.5062   0.06190   0.05601  -0.0377   0.1006   1.0000
  16.750   1.4992   0.06542   0.05954  -0.0374   0.0946   1.0000
  17.000   1.4906   0.06917   0.06330  -0.0372   0.0907   1.0000
  17.250   1.4862   0.07252   0.06670  -0.0371   0.0880   1.0000
  17.500   1.4817   0.07590   0.07013  -0.0371   0.0858   1.0000
  17.750   1.4737   0.07975   0.07402  -0.0372   0.0837   1.0000
  18.000   1.4639   0.08384   0.07814  -0.0375   0.0819   1.0000
  18.250   1.4623   0.08698   0.08136  -0.0377   0.0806   1.0000
  18.500   1.4591   0.09035   0.08481  -0.0380   0.0794   1.0000
  18.750   1.4565   0.09367   0.08819  -0.0383   0.0781   1.0000
  19.000   1.4518   0.09726   0.09184  -0.0388   0.0771   1.0000
  19.250   1.4465   0.10092   0.09554  -0.0394   0.0759   1.0000
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