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GOE 298 AIRFOIL (goe298-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 298 AIRFOIL (goe298-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.44 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe298-il-1000000.txt
Download as CSV file: xf-goe298-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 298 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.5330   0.19196   0.19007   0.0216   1.0000   0.0281
 -16.250  -0.5234   0.18924   0.18736   0.0200   1.0000   0.0286
 -15.000  -1.1854   0.03333   0.03012  -0.0883   1.0000   0.0376
 -14.750  -1.1752   0.03005   0.02663  -0.0900   1.0000   0.0379
 -14.500  -1.1589   0.02801   0.02443  -0.0907   1.0000   0.0381
 -14.250  -1.1394   0.02650   0.02278  -0.0910   1.0000   0.0384
 -14.000  -1.1229   0.02459   0.02077  -0.0913   1.0000   0.0390
 -13.750  -1.1015   0.02340   0.01952  -0.0913   1.0000   0.0395
 -13.500  -1.0784   0.02244   0.01850  -0.0913   1.0000   0.0399
 -13.250  -1.0545   0.02159   0.01758  -0.0913   1.0000   0.0403
 -13.000  -1.0300   0.02079   0.01673  -0.0913   1.0000   0.0408
 -12.750  -1.0051   0.02004   0.01590  -0.0912   1.0000   0.0413
 -12.500  -0.9798   0.01933   0.01511  -0.0912   1.0000   0.0418
 -12.250  -0.9541   0.01867   0.01438  -0.0911   1.0000   0.0423
 -12.000  -0.9205   0.01805   0.01365  -0.0925   0.9814   0.0427
 -11.750  -0.8902   0.01707   0.01260  -0.0937   0.9585   0.0435
 -11.500  -0.8638   0.01655   0.01200  -0.0935   0.9385   0.0442
 -11.250  -0.8384   0.01614   0.01150  -0.0929   0.9244   0.0448
 -11.000  -0.8124   0.01575   0.01103  -0.0925   0.9129   0.0455
 -10.750  -0.7861   0.01540   0.01058  -0.0921   0.9023   0.0462
 -10.500  -0.7588   0.01505   0.01014  -0.0919   0.8935   0.0469
 -10.250  -0.7319   0.01464   0.00962  -0.0916   0.8848   0.0476
 -10.000  -0.7048   0.01411   0.00906  -0.0915   0.8772   0.0486
  -9.750  -0.6771   0.01377   0.00868  -0.0913   0.8689   0.0495
  -9.500  -0.6491   0.01348   0.00833  -0.0912   0.8611   0.0504
  -9.250  -0.6208   0.01319   0.00797  -0.0911   0.8519   0.0513
  -9.000  -0.5925   0.01294   0.00763  -0.0909   0.8429   0.0520
  -8.750  -0.5644   0.01251   0.00715  -0.0908   0.8324   0.0532
  -8.500  -0.5360   0.01222   0.00682  -0.0907   0.8218   0.0543
  -8.250  -0.5074   0.01200   0.00655  -0.0906   0.8095   0.0554
  -8.000  -0.4785   0.01181   0.00629  -0.0905   0.7978   0.0566
  -7.750  -0.4497   0.01166   0.00604  -0.0904   0.7858   0.0575
  -7.500  -0.4210   0.01132   0.00567  -0.0904   0.7749   0.0591
  -7.250  -0.3920   0.01116   0.00546  -0.0904   0.7649   0.0604
  -7.000  -0.3628   0.01102   0.00526  -0.0903   0.7548   0.0616
  -6.750  -0.3337   0.01090   0.00506  -0.0903   0.7449   0.0628
  -6.500  -0.3045   0.01068   0.00479  -0.0903   0.7356   0.0642
  -6.250  -0.2753   0.01055   0.00463  -0.0903   0.7272   0.0658
  -6.000  -0.2457   0.01045   0.00453  -0.0903   0.7198   0.0673
  -5.750  -0.2163   0.01039   0.00439  -0.0902   0.7107   0.0687
  -5.500  -0.1868   0.01025   0.00421  -0.0902   0.7027   0.0700
  -5.250  -0.1573   0.01010   0.00406  -0.0903   0.6951   0.0718
  -5.000  -0.1278   0.01008   0.00400  -0.0903   0.6873   0.0733
  -4.750  -0.0979   0.01001   0.00393  -0.0903   0.6805   0.0749
  -4.500  -0.0683   0.00998   0.00384  -0.0903   0.6716   0.0762
  -4.250  -0.0388   0.00981   0.00365  -0.0904   0.6625   0.0780
  -4.000  -0.0091   0.00979   0.00362  -0.0904   0.6518   0.0795
  -3.750   0.0206   0.00979   0.00360  -0.0904   0.6415   0.0810
  -3.250   0.0800   0.00979   0.00348  -0.0904   0.6151   0.0837
  -3.000   0.1094   0.00963   0.00329  -0.0905   0.6027   0.0857
  -2.750   0.1389   0.00964   0.00326  -0.0905   0.5898   0.0871
  -2.500   0.1685   0.00964   0.00323  -0.0906   0.5788   0.0886
  -2.250   0.1981   0.00966   0.00320  -0.0906   0.5693   0.0901
  -2.000   0.2278   0.00968   0.00319  -0.0906   0.5620   0.0915
  -1.750   0.2573   0.00965   0.00311  -0.0907   0.5551   0.0926
  -1.500   0.2869   0.00947   0.00294  -0.0908   0.5495   0.0946
  -1.250   0.3165   0.00945   0.00292  -0.0908   0.5438   0.0962
  -1.000   0.3460   0.00945   0.00291  -0.0909   0.5376   0.0978
  -0.750   0.3756   0.00944   0.00288  -0.0909   0.5318   0.0993
  -0.500   0.4053   0.00942   0.00285  -0.0910   0.5269   0.1006
  -0.250   0.4349   0.00944   0.00286  -0.0910   0.5220   0.1015
   0.000   0.4644   0.00927   0.00267  -0.0912   0.5167   0.1037
   0.250   0.4940   0.00921   0.00263  -0.0913   0.5117   0.1054
   0.500   0.5236   0.00917   0.00261  -0.0913   0.5050   0.1071
   0.750   0.5529   0.00920   0.00260  -0.0914   0.4966   0.1087
   1.000   0.5825   0.00917   0.00258  -0.0914   0.4890   0.1101
   1.250   0.6119   0.00920   0.00258  -0.0915   0.4787   0.1115
   1.500   0.6413   0.00922   0.00258  -0.0915   0.4669   0.1123
   1.750   0.6705   0.00917   0.00248  -0.0916   0.4482   0.1149
   2.000   0.6984   0.00939   0.00250  -0.0915   0.3966   0.1170
   2.250   0.7243   0.00994   0.00274  -0.0913   0.3341   0.1191
   2.500   0.7523   0.01015   0.00287  -0.0912   0.3172   0.1209
   2.750   0.7810   0.01026   0.00295  -0.0912   0.3083   0.1227
   3.000   0.8095   0.01041   0.00306  -0.0912   0.3006   0.1242
   3.250   0.8382   0.01048   0.00313  -0.0912   0.2947   0.1282
   3.500   0.8671   0.01053   0.00321  -0.0912   0.2903   0.1325
   3.750   0.8956   0.01063   0.00332  -0.0912   0.2852   0.1366
   4.000   0.9239   0.01076   0.00345  -0.0911   0.2792   0.1458
   4.250   0.9528   0.01076   0.00357  -0.0912   0.2756   0.1839
   4.500   0.9821   0.01051   0.00377  -0.0916   0.2713   0.3815
   4.750   1.0016   0.00936   0.00398  -0.0899   0.2667   1.0000
   5.000   1.0296   0.00958   0.00414  -0.0898   0.2604   1.0000
   5.250   1.0582   0.00971   0.00425  -0.0897   0.2569   1.0000
   5.500   1.0866   0.00985   0.00438  -0.0897   0.2521   1.0000
   5.750   1.1144   0.01006   0.00453  -0.0896   0.2461   1.0000
   6.000   1.1423   0.01024   0.00469  -0.0895   0.2406   1.0000
   6.250   1.1702   0.01041   0.00483  -0.0894   0.2342   1.0000
   6.500   1.1973   0.01067   0.00502  -0.0892   0.2250   1.0000
   6.750   1.2245   0.01089   0.00520  -0.0891   0.2152   1.0000
   7.000   1.2511   0.01117   0.00541  -0.0888   0.2041   1.0000
   7.250   1.2768   0.01152   0.00567  -0.0885   0.1894   1.0000
   7.500   1.3015   0.01197   0.00599  -0.0880   0.1717   1.0000
   7.750   1.3255   0.01245   0.00636  -0.0874   0.1562   1.0000
   8.000   1.3496   0.01289   0.00672  -0.0869   0.1451   1.0000
   8.250   1.3738   0.01330   0.00709  -0.0863   0.1372   1.0000
   8.500   1.3980   0.01370   0.00744  -0.0857   0.1315   1.0000
   8.750   1.4219   0.01410   0.00781  -0.0851   0.1267   1.0000
   9.000   1.4463   0.01443   0.00814  -0.0846   0.1237   1.0000
   9.250   1.4697   0.01482   0.00851  -0.0839   0.1204   1.0000
   9.500   1.4920   0.01528   0.00895  -0.0831   0.1169   1.0000
   9.750   1.5154   0.01562   0.00931  -0.0824   0.1149   1.0000
  10.000   1.5385   0.01596   0.00967  -0.0817   0.1132   1.0000
  10.250   1.5606   0.01635   0.01006  -0.0808   0.1114   1.0000
  10.500   1.5816   0.01678   0.01050  -0.0798   0.1095   1.0000
  10.750   1.6011   0.01728   0.01100  -0.0786   0.1073   1.0000
  11.000   1.6187   0.01782   0.01155  -0.0771   0.1052   1.0000
  11.250   1.6386   0.01817   0.01194  -0.0759   0.1041   1.0000
  11.500   1.6554   0.01860   0.01241  -0.0743   0.1027   1.0000
  11.750   1.6714   0.01912   0.01295  -0.0726   0.1011   1.0000
  12.000   1.6865   0.01974   0.01359  -0.0709   0.0994   1.0000
  12.250   1.7005   0.02048   0.01434  -0.0693   0.0976   1.0000
  12.500   1.7126   0.02139   0.01528  -0.0677   0.0956   1.0000
  12.750   1.7298   0.02202   0.01595  -0.0666   0.0946   1.0000
  13.000   1.7463   0.02270   0.01668  -0.0656   0.0931   1.0000
  13.250   1.7612   0.02353   0.01754  -0.0645   0.0910   1.0000
  13.500   1.7742   0.02452   0.01854  -0.0633   0.0888   1.0000
  13.750   1.7856   0.02568   0.01972  -0.0620   0.0862   1.0000
  14.000   1.8009   0.02653   0.02062  -0.0612   0.0839   1.0000
  14.250   1.8122   0.02775   0.02184  -0.0601   0.0800   1.0000
  14.500   1.8223   0.02909   0.02319  -0.0591   0.0751   1.0000
  14.750   1.8282   0.03083   0.02490  -0.0579   0.0676   1.0000
  15.250   1.8067   0.03762   0.03151  -0.0547   0.0408   1.0000
  15.500   1.8014   0.04066   0.03459  -0.0537   0.0373   1.0000
  15.750   1.7998   0.04340   0.03738  -0.0530   0.0356   1.0000
  16.000   1.7969   0.04631   0.04036  -0.0523   0.0344   1.0000
  16.250   1.7929   0.04948   0.04360  -0.0518   0.0333   1.0000
  16.500   1.7912   0.05250   0.04669  -0.0515   0.0326   1.0000
  16.750   1.7895   0.05558   0.04986  -0.0514   0.0320   1.0000
  17.000   1.7862   0.05895   0.05331  -0.0514   0.0315   1.0000
  17.250   1.7815   0.06259   0.05703  -0.0515   0.0310   1.0000
  17.500   1.7749   0.06651   0.06105  -0.0518   0.0306   1.0000
  17.750   1.7661   0.07079   0.06541  -0.0523   0.0302   1.0000
  18.000   1.7556   0.07538   0.07010  -0.0530   0.0298   1.0000
  18.250   1.7429   0.08036   0.07519  -0.0538   0.0294   1.0000
  18.500   1.7277   0.08575   0.08069  -0.0549   0.0291   1.0000
  18.750   1.7176   0.09053   0.08557  -0.0560   0.0289   1.0000
  19.000   1.7059   0.09563   0.09078  -0.0573   0.0288   1.0000
  19.250   1.6924   0.10105   0.09632  -0.0588   0.0286   1.0000
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