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GOE 284 AIRFOIL (goe284-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 284 AIRFOIL (goe284-il)
Reynolds number: 1,000,000
Max Cl/Cd: 126.47 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe284-il-1000000.txt
Download as CSV file: xf-goe284-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.9089   0.08231   0.07935  -0.0568   1.0000   0.0301
 -16.750  -0.9416   0.07401   0.07095  -0.0622   1.0000   0.0301
 -16.500  -0.9867   0.06389   0.06069  -0.0691   1.0000   0.0301
 -16.250  -1.0397   0.05184   0.04844  -0.0781   1.0000   0.0300
 -16.000  -1.0738   0.04033   0.03666  -0.0894   1.0000   0.0299
 -15.750  -1.0857   0.03405   0.03020  -0.0964   1.0000   0.0300
 -15.500  -1.0886   0.03082   0.02685  -0.0987   1.0000   0.0301
 -15.250  -1.0870   0.02874   0.02468  -0.0989   1.0000   0.0303
 -15.000  -1.0757   0.02715   0.02298  -0.0992   0.9785   0.0304
 -14.750  -1.0702   0.02603   0.02176  -0.0972   0.9630   0.0306
 -14.500  -1.0610   0.02505   0.02068  -0.0953   0.9512   0.0308
 -14.250  -1.0480   0.02412   0.01966  -0.0938   0.9408   0.0310
 -14.000  -1.0328   0.02327   0.01872  -0.0925   0.9318   0.0312
 -13.750  -1.0160   0.02247   0.01783  -0.0913   0.9223   0.0314
 -13.500  -0.9971   0.02172   0.01699  -0.0904   0.9132   0.0316
 -13.250  -0.9776   0.02104   0.01621  -0.0894   0.9031   0.0318
 -13.000  -0.9562   0.02039   0.01547  -0.0886   0.8926   0.0320
 -12.750  -0.9345   0.01981   0.01479  -0.0878   0.8812   0.0322
 -12.500  -0.9121   0.01922   0.01411  -0.0872   0.8680   0.0323
 -12.250  -0.8921   0.01833   0.01311  -0.0863   0.8540   0.0328
 -12.000  -0.8701   0.01764   0.01232  -0.0856   0.8385   0.0331
 -11.750  -0.8467   0.01706   0.01164  -0.0851   0.8207   0.0336
 -11.500  -0.8223   0.01658   0.01104  -0.0846   0.8006   0.0340
 -11.250  -0.7973   0.01615   0.01049  -0.0842   0.7786   0.0345
 -11.000  -0.7718   0.01576   0.00997  -0.0838   0.7557   0.0349
 -10.750  -0.7458   0.01541   0.00949  -0.0835   0.7333   0.0353
 -10.500  -0.7194   0.01508   0.00904  -0.0833   0.7123   0.0357
 -10.250  -0.6926   0.01479   0.00862  -0.0831   0.6927   0.0361
 -10.000  -0.6663   0.01439   0.00811  -0.0829   0.6750   0.0368
  -9.750  -0.6398   0.01398   0.00762  -0.0827   0.6591   0.0376
  -9.500  -0.6127   0.01366   0.00721  -0.0826   0.6443   0.0385
  -9.250  -0.5852   0.01336   0.00683  -0.0825   0.6316   0.0394
  -9.000  -0.5573   0.01310   0.00650  -0.0824   0.6206   0.0403
  -8.750  -0.5299   0.01275   0.00609  -0.0823   0.6105   0.0421
  -8.500  -0.5022   0.01243   0.00574  -0.0823   0.6019   0.0446
  -8.250  -0.4747   0.01203   0.00535  -0.0822   0.5944   0.0505
  -8.000  -0.4470   0.01173   0.00510  -0.0822   0.5867   0.0641
  -7.750  -0.4177   0.01164   0.00503  -0.0823   0.5812   0.0719
  -7.500  -0.3882   0.01159   0.00498  -0.0825   0.5755   0.0760
  -7.250  -0.3585   0.01160   0.00495  -0.0826   0.5699   0.0790
  -7.000  -0.3290   0.01158   0.00487  -0.0828   0.5648   0.0810
  -6.750  -0.2994   0.01150   0.00481  -0.0829   0.5616   0.0832
  -6.500  -0.2697   0.01148   0.00477  -0.0831   0.5579   0.0849
  -6.250  -0.2399   0.01146   0.00473  -0.0833   0.5542   0.0866
  -6.000  -0.2102   0.01148   0.00468  -0.0834   0.5504   0.0878
  -5.750  -0.1812   0.01141   0.00456  -0.0836   0.5462   0.0892
  -5.500  -0.1518   0.01126   0.00444  -0.0837   0.5443   0.0910
  -5.250  -0.1220   0.01121   0.00440  -0.0839   0.5421   0.0925
  -5.000  -0.0922   0.01116   0.00434  -0.0841   0.5397   0.0938
  -4.750  -0.0626   0.01112   0.00427  -0.0843   0.5371   0.0952
  -4.500  -0.0329   0.01109   0.00421  -0.0845   0.5345   0.0963
  -4.250  -0.0032   0.01109   0.00417  -0.0847   0.5316   0.0970
  -4.000   0.0254   0.01090   0.00395  -0.0848   0.5284   0.0986
  -3.750   0.0546   0.01078   0.00383  -0.0850   0.5262   0.1001
  -3.500   0.0843   0.01068   0.00375  -0.0852   0.5249   0.1014
  -3.250   0.1141   0.01062   0.00369  -0.0854   0.5233   0.1029
  -3.000   0.1438   0.01055   0.00363  -0.0856   0.5212   0.1043
  -2.750   0.1736   0.01049   0.00355  -0.0859   0.5186   0.1055
  -2.500   0.2033   0.01046   0.00350  -0.0861   0.5156   0.1066
  -2.250   0.2325   0.01037   0.00338  -0.0863   0.5124   0.1081
  -2.000   0.2614   0.01029   0.00327  -0.0864   0.5086   0.1101
  -1.750   0.2910   0.01020   0.00320  -0.0866   0.5066   0.1117
  -1.500   0.3209   0.01010   0.00312  -0.0869   0.5043   0.1133
  -1.250   0.3507   0.01003   0.00306  -0.0872   0.5013   0.1149
  -1.000   0.3804   0.00997   0.00300  -0.0874   0.4984   0.1164
  -0.750   0.4100   0.00995   0.00295  -0.0877   0.4958   0.1177
  -0.500   0.4394   0.00991   0.00290  -0.0879   0.4933   0.1196
  -0.250   0.4686   0.00989   0.00287  -0.0881   0.4905   0.1228
   0.000   0.4981   0.00986   0.00286  -0.0883   0.4884   0.1256
   0.250   0.5279   0.00981   0.00284  -0.0886   0.4869   0.1284
   0.500   0.5577   0.00977   0.00281  -0.0889   0.4848   0.1314
   0.750   0.5873   0.00969   0.00279  -0.0892   0.4824   0.1384
   1.000   0.6169   0.00965   0.00278  -0.0895   0.4800   0.1462
   1.250   0.6461   0.00956   0.00278  -0.0897   0.4775   0.1693
   1.500   0.6747   0.00938   0.00281  -0.0900   0.4748   0.2464
   1.750   0.7032   0.00929   0.00288  -0.0902   0.4715   0.3095
   2.000   0.7321   0.00909   0.00293  -0.0905   0.4695   0.3879
   2.250   0.7602   0.00868   0.00299  -0.0908   0.4673   0.5485
   2.500   0.7869   0.00825   0.00307  -0.0907   0.4647   0.7249
   2.750   0.8108   0.00793   0.00318  -0.0896   0.4617   0.8642
   3.000   0.8344   0.00786   0.00326  -0.0883   0.4585   0.9458
   3.250   0.8704   0.00795   0.00333  -0.0899   0.4543   0.9819
   3.500   0.9130   0.00801   0.00339  -0.0931   0.4508   0.9979
   3.750   0.9443   0.00806   0.00343  -0.0938   0.4465   1.0000
   4.000   0.9712   0.00813   0.00347  -0.0936   0.4409   1.0000
   4.250   0.9979   0.00825   0.00353  -0.0934   0.4349   1.0000
   4.500   1.0258   0.00831   0.00359  -0.0934   0.4283   1.0000
   4.750   1.0525   0.00845   0.00367  -0.0932   0.4196   1.0000
   5.000   1.0801   0.00856   0.00375  -0.0932   0.4104   1.0000
   5.250   1.1066   0.00875   0.00387  -0.0931   0.3980   1.0000
   5.500   1.1323   0.00899   0.00402  -0.0928   0.3815   1.0000
   5.750   1.1570   0.00930   0.00423  -0.0924   0.3639   1.0000
   6.000   1.1814   0.00964   0.00447  -0.0920   0.3480   1.0000
   6.250   1.2054   0.00999   0.00474  -0.0915   0.3345   1.0000
   6.500   1.2297   0.01032   0.00500  -0.0910   0.3234   1.0000
   6.750   1.2544   0.01061   0.00525  -0.0907   0.3150   1.0000
   7.000   1.2781   0.01094   0.00553  -0.0901   0.3067   1.0000
   7.250   1.3026   0.01121   0.00578  -0.0897   0.2999   1.0000
   7.500   1.3261   0.01153   0.00606  -0.0892   0.2930   1.0000
   7.750   1.3491   0.01185   0.00636  -0.0886   0.2870   1.0000
   8.000   1.3735   0.01209   0.00660  -0.0882   0.2829   1.0000
   8.250   1.3964   0.01239   0.00689  -0.0875   0.2783   1.0000
   8.500   1.4172   0.01277   0.00723  -0.0866   0.2731   1.0000
   8.750   1.4397   0.01303   0.00751  -0.0859   0.2695   1.0000
   9.000   1.4609   0.01332   0.00780  -0.0850   0.2654   1.0000
   9.250   1.4783   0.01370   0.00817  -0.0834   0.2611   1.0000
   9.500   1.4938   0.01418   0.00864  -0.0817   0.2564   1.0000
   9.750   1.5141   0.01450   0.00899  -0.0807   0.2539   1.0000
  10.000   1.5336   0.01488   0.00939  -0.0797   0.2508   1.0000
  10.250   1.5514   0.01536   0.00987  -0.0785   0.2472   1.0000
  10.500   1.5673   0.01595   0.01046  -0.0772   0.2433   1.0000
  10.750   1.5837   0.01654   0.01106  -0.0760   0.2399   1.0000
  11.000   1.6030   0.01700   0.01156  -0.0752   0.2374   1.0000
  11.250   1.6205   0.01757   0.01216  -0.0742   0.2343   1.0000
  11.500   1.6358   0.01828   0.01289  -0.0731   0.2309   1.0000
  11.750   1.6488   0.01918   0.01378  -0.0718   0.2270   1.0000
  12.000   1.6647   0.01992   0.01456  -0.0709   0.2240   1.0000
  12.250   1.6809   0.02067   0.01534  -0.0701   0.2206   1.0000
  12.500   1.6934   0.02169   0.01638  -0.0690   0.2163   1.0000
  12.750   1.7022   0.02303   0.01771  -0.0677   0.2115   1.0000
  13.000   1.7165   0.02400   0.01873  -0.0670   0.2078   1.0000
  13.250   1.7267   0.02531   0.02007  -0.0660   0.2024   1.0000
  13.500   1.7318   0.02709   0.02185  -0.0649   0.1966   1.0000
  13.750   1.7407   0.02861   0.02339  -0.0640   0.1897   1.0000
  14.000   1.7401   0.03099   0.02575  -0.0628   0.1791   1.0000
  14.250   1.7275   0.03451   0.02920  -0.0612   0.1592   1.0000
  14.500   1.6920   0.04035   0.03489  -0.0591   0.1308   1.0000
  14.750   1.6730   0.04480   0.03931  -0.0578   0.1192   1.0000
  15.000   1.6624   0.04852   0.04304  -0.0569   0.1131   1.0000
  15.250   1.6578   0.05168   0.04625  -0.0564   0.1096   1.0000
  15.500   1.6520   0.05505   0.04966  -0.0558   0.1065   1.0000
  15.750   1.6466   0.05838   0.05303  -0.0554   0.1033   1.0000
  16.000   1.6475   0.06106   0.05576  -0.0551   0.1012   1.0000
  16.250   1.6448   0.06420   0.05896  -0.0549   0.0991   1.0000
  16.500   1.6420   0.06734   0.06214  -0.0546   0.0969   1.0000
  16.750   1.6360   0.07091   0.06575  -0.0545   0.0946   1.0000
  17.000   1.6374   0.07362   0.06853  -0.0544   0.0930   1.0000
  17.250   1.6379   0.07651   0.07148  -0.0544   0.0914   1.0000
  17.500   1.6381   0.07940   0.07442  -0.0544   0.0894   1.0000
  17.750   1.6331   0.08298   0.07804  -0.0545   0.0873   1.0000
  18.000   1.6280   0.08655   0.08166  -0.0547   0.0849   1.0000
  18.250   1.6286   0.08949   0.08467  -0.0549   0.0830   1.0000
  18.500   1.6278   0.09260   0.08782  -0.0551   0.0801   1.0000
  18.750   1.6201   0.09666   0.09190  -0.0555   0.0770   1.0000
  19.000   1.6184   0.09991   0.09520  -0.0559   0.0736   1.0000
  19.250   1.6082   0.10433   0.09965  -0.0566   0.0690   1.0000
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