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GOE 284 AIRFOIL (goe284-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 284 AIRFOIL (goe284-il)
Reynolds number: 1,000,000
Max Cl/Cd: 107.08 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe284-il-1000000-n5.txt
Download as CSV file: xf-goe284-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 284 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.8108   0.09511   0.09223  -0.0481   1.0000   0.0260
 -16.500  -0.8420   0.08673   0.08376  -0.0537   0.9754   0.0260
 -16.250  -1.1302   0.03625   0.03227  -0.0937   0.9477   0.0254
 -16.000  -1.1459   0.03171   0.02752  -0.0966   0.9328   0.0255
 -15.750  -1.1503   0.02938   0.02502  -0.0962   0.9201   0.0256
 -15.500  -1.1496   0.02777   0.02329  -0.0946   0.9075   0.0257
 -15.250  -1.1435   0.02655   0.02196  -0.0928   0.8961   0.0258
 -15.000  -1.1313   0.02546   0.02076  -0.0917   0.8839   0.0259
 -14.750  -1.1161   0.02450   0.01970  -0.0907   0.8707   0.0261
 -14.500  -1.0990   0.02364   0.01873  -0.0898   0.8564   0.0263
 -14.250  -1.0805   0.02287   0.01784  -0.0890   0.8398   0.0265
 -14.000  -1.0608   0.02216   0.01701  -0.0882   0.8210   0.0266
 -13.750  -1.0401   0.02150   0.01622  -0.0876   0.8006   0.0268
 -13.500  -1.0185   0.02089   0.01547  -0.0870   0.7798   0.0270
 -13.250  -0.9960   0.02032   0.01477  -0.0864   0.7587   0.0271
 -13.000  -0.9730   0.01979   0.01411  -0.0860   0.7378   0.0273
 -12.750  -0.9493   0.01929   0.01349  -0.0856   0.7176   0.0275
 -12.500  -0.9250   0.01882   0.01290  -0.0852   0.6986   0.0277
 -12.250  -0.9003   0.01838   0.01234  -0.0849   0.6810   0.0279
 -12.000  -0.8752   0.01797   0.01181  -0.0846   0.6645   0.0280
 -11.750  -0.8497   0.01757   0.01131  -0.0843   0.6496   0.0282
 -11.500  -0.8237   0.01719   0.01084  -0.0841   0.6368   0.0283
 -11.250  -0.7978   0.01681   0.01036  -0.0839   0.6242   0.0285
 -11.000  -0.7721   0.01634   0.00981  -0.0836   0.6131   0.0289
 -10.750  -0.7459   0.01593   0.00933  -0.0834   0.6027   0.0292
 -10.500  -0.7193   0.01555   0.00888  -0.0833   0.5935   0.0295
 -10.250  -0.6924   0.01521   0.00847  -0.0831   0.5848   0.0298
 -10.000  -0.6651   0.01487   0.00808  -0.0830   0.5786   0.0302
  -9.750  -0.6376   0.01456   0.00772  -0.0830   0.5719   0.0306
  -9.500  -0.6100   0.01429   0.00737  -0.0829   0.5656   0.0310
  -9.250  -0.5820   0.01401   0.00705  -0.0829   0.5610   0.0314
  -9.000  -0.5539   0.01376   0.00676  -0.0828   0.5562   0.0318
  -8.750  -0.5257   0.01350   0.00645  -0.0828   0.5513   0.0324
  -8.500  -0.4978   0.01322   0.00612  -0.0828   0.5466   0.0331
  -8.250  -0.4695   0.01295   0.00582  -0.0828   0.5431   0.0339
  -8.000  -0.4410   0.01270   0.00555  -0.0828   0.5399   0.0349
  -7.750  -0.4124   0.01247   0.00529  -0.0829   0.5366   0.0359
  -7.500  -0.3839   0.01221   0.00501  -0.0829   0.5333   0.0378
  -7.250  -0.3555   0.01195   0.00473  -0.0830   0.5299   0.0409
  -7.000  -0.3278   0.01157   0.00440  -0.0830   0.5263   0.0512
  -6.750  -0.2992   0.01132   0.00421  -0.0831   0.5237   0.0638
  -6.500  -0.2699   0.01118   0.00410  -0.0832   0.5214   0.0691
  -6.250  -0.2404   0.01108   0.00399  -0.0834   0.5191   0.0724
  -6.000  -0.2109   0.01099   0.00390  -0.0835   0.5168   0.0752
  -5.750  -0.1813   0.01091   0.00380  -0.0837   0.5145   0.0773
  -5.500  -0.1517   0.01084   0.00371  -0.0839   0.5122   0.0791
  -5.250  -0.1222   0.01076   0.00363  -0.0840   0.5098   0.0812
  -5.000  -0.0926   0.01071   0.00356  -0.0842   0.5074   0.0829
  -4.750  -0.0630   0.01065   0.00349  -0.0844   0.5052   0.0843
  -4.500  -0.0332   0.01058   0.00341  -0.0846   0.5041   0.0856
  -4.250  -0.0034   0.01052   0.00334  -0.0848   0.5028   0.0865
  -4.000   0.0263   0.01043   0.00325  -0.0850   0.5012   0.0876
  -3.750   0.0560   0.01034   0.00317  -0.0852   0.4994   0.0888
  -3.500   0.0857   0.01028   0.00310  -0.0854   0.4975   0.0900
  -3.250   0.1155   0.01023   0.00305  -0.0857   0.4955   0.0916
  -3.000   0.1452   0.01019   0.00300  -0.0859   0.4930   0.0930
  -2.750   0.1748   0.01016   0.00295  -0.0861   0.4901   0.0941
  -2.500   0.2043   0.01016   0.00291  -0.0863   0.4866   0.0949
  -2.250   0.2342   0.01010   0.00285  -0.0866   0.4848   0.0959
  -2.000   0.2639   0.01001   0.00279  -0.0868   0.4825   0.0980
  -1.750   0.2937   0.00996   0.00275  -0.0871   0.4799   0.0997
  -1.500   0.3234   0.00992   0.00271  -0.0873   0.4765   0.1011
  -1.250   0.3529   0.00990   0.00267  -0.0875   0.4724   0.1023
  -1.000   0.3823   0.00991   0.00264  -0.0877   0.4679   0.1034
  -0.750   0.4122   0.00987   0.00261  -0.0880   0.4657   0.1045
  -0.500   0.4420   0.00985   0.00259  -0.0883   0.4634   0.1053
  -0.250   0.4716   0.00980   0.00257  -0.0886   0.4611   0.1073
   0.000   0.5012   0.00977   0.00255  -0.0888   0.4587   0.1096
   0.250   0.5308   0.00976   0.00255  -0.0891   0.4561   0.1118
   0.500   0.5602   0.00976   0.00255  -0.0893   0.4533   0.1138
   0.750   0.5895   0.00978   0.00256  -0.0895   0.4504   0.1157
   1.000   0.6192   0.00976   0.00257  -0.0898   0.4481   0.1184
   1.250   0.6488   0.00974   0.00258  -0.0901   0.4450   0.1226
   1.500   0.6782   0.00974   0.00260  -0.0904   0.4409   0.1272
   1.750   0.7073   0.00975   0.00262  -0.0906   0.4365   0.1352
   2.000   0.7362   0.00975   0.00266  -0.0908   0.4324   0.1491
   2.250   0.7654   0.00969   0.00270  -0.0911   0.4285   0.1793
   2.500   0.7943   0.00962   0.00275  -0.0914   0.4230   0.2285
   2.750   0.8226   0.00961   0.00282  -0.0916   0.4166   0.2688
   3.000   0.8515   0.00959   0.00289  -0.0918   0.4099   0.3048
   3.500   0.9061   0.00956   0.00312  -0.0920   0.3834   0.4506
   3.750   0.9314   0.00948   0.00332  -0.0918   0.3634   0.5972
   4.000   0.9552   0.00943   0.00358  -0.0913   0.3440   0.7440
   4.250   0.9745   0.00934   0.00385  -0.0895   0.3298   0.8967
   4.500   1.0027   0.00953   0.00408  -0.0895   0.3174   0.9796
   4.750   1.0371   0.00977   0.00427  -0.0911   0.3078   1.0000
   5.000   1.0629   0.01000   0.00445  -0.0908   0.3010   1.0000
   5.250   1.0891   0.01021   0.00462  -0.0906   0.2949   1.0000
   5.500   1.1145   0.01046   0.00482  -0.0903   0.2885   1.0000
   5.750   1.1405   0.01067   0.00500  -0.0901   0.2836   1.0000
   6.000   1.1661   0.01089   0.00520  -0.0899   0.2776   1.0000
   6.500   1.2160   0.01141   0.00565  -0.0892   0.2658   1.0000
   6.750   1.2412   0.01164   0.00586  -0.0888   0.2614   1.0000
   7.000   1.2653   0.01191   0.00610  -0.0884   0.2568   1.0000
   7.250   1.2894   0.01218   0.00635  -0.0879   0.2528   1.0000
   7.500   1.3141   0.01239   0.00657  -0.0876   0.2500   1.0000
   7.750   1.3381   0.01264   0.00681  -0.0871   0.2469   1.0000
   8.000   1.3610   0.01292   0.00709  -0.0864   0.2432   1.0000
   8.250   1.3821   0.01326   0.00740  -0.0855   0.2389   1.0000
   8.500   1.4032   0.01356   0.00771  -0.0846   0.2349   1.0000
   8.750   1.4222   0.01388   0.00802  -0.0833   0.2309   1.0000
   9.000   1.4402   0.01426   0.00839  -0.0819   0.2272   1.0000
   9.250   1.4581   0.01468   0.00882  -0.0806   0.2241   1.0000
   9.500   1.4761   0.01512   0.00927  -0.0793   0.2209   1.0000
   9.750   1.4955   0.01553   0.00969  -0.0784   0.2185   1.0000
  10.000   1.5137   0.01601   0.01018  -0.0773   0.2149   1.0000
  10.250   1.5296   0.01663   0.01079  -0.0760   0.2103   1.0000
  10.500   1.5447   0.01732   0.01148  -0.0747   0.2060   1.0000
  10.750   1.5624   0.01789   0.01208  -0.0738   0.2031   1.0000
  11.000   1.5781   0.01860   0.01280  -0.0727   0.1987   1.0000
  11.250   1.5899   0.01958   0.01377  -0.0713   0.1931   1.0000
  11.500   1.6041   0.02045   0.01465  -0.0703   0.1881   1.0000
  11.750   1.6127   0.02174   0.01592  -0.0688   0.1796   1.0000
  12.000   1.6158   0.02350   0.01762  -0.0671   0.1647   1.0000
  12.250   1.5880   0.02785   0.02177  -0.0637   0.1268   1.0000
  12.500   1.5775   0.03112   0.02500  -0.0619   0.1135   1.0000
  12.750   1.5790   0.03343   0.02734  -0.0610   0.1087   1.0000
  13.000   1.5821   0.03567   0.02961  -0.0602   0.1056   1.0000
  13.250   1.5839   0.03805   0.03202  -0.0594   0.1026   1.0000
  13.500   1.5878   0.04027   0.03429  -0.0588   0.1004   1.0000
  13.750   1.5927   0.04242   0.03649  -0.0583   0.0987   1.0000
  14.000   1.5962   0.04474   0.03886  -0.0578   0.0969   1.0000
  14.250   1.5972   0.04734   0.04150  -0.0573   0.0949   1.0000
  14.500   1.5970   0.05008   0.04428  -0.0568   0.0926   1.0000
  14.750   1.5991   0.05259   0.04684  -0.0564   0.0908   1.0000
  15.000   1.6028   0.05499   0.04930  -0.0561   0.0896   1.0000
  15.250   1.6067   0.05734   0.05170  -0.0558   0.0882   1.0000
  15.500   1.6081   0.06002   0.05443  -0.0556   0.0867   1.0000
  15.750   1.6093   0.06270   0.05716  -0.0553   0.0849   1.0000
  16.000   1.6076   0.06578   0.06027  -0.0552   0.0829   1.0000
  16.250   1.6091   0.06846   0.06300  -0.0550   0.0811   1.0000
  16.500   1.6099   0.07128   0.06588  -0.0549   0.0791   1.0000
  16.750   1.6110   0.07405   0.06868  -0.0548   0.0768   1.0000
  17.000   1.6072   0.07747   0.07214  -0.0549   0.0744   1.0000
  17.250   1.6075   0.08038   0.07509  -0.0549   0.0717   1.0000
  17.500   1.6020   0.08405   0.07879  -0.0550   0.0677   1.0000
  17.750   1.5976   0.08757   0.08233  -0.0552   0.0630   1.0000
  18.000   1.5874   0.09192   0.08670  -0.0555   0.0577   1.0000
  18.250   1.5750   0.09661   0.09139  -0.0560   0.0509   1.0000
  18.500   1.5585   0.10187   0.09666  -0.0567   0.0438   1.0000
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