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GOE 285 AIRFOIL (goe285-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 285 AIRFOIL (goe285-il)
Reynolds number: 1,000,000
Max Cl/Cd: 103.52 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe285-il-1000000-n5.txt
Download as CSV file: xf-goe285-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 285 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
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.9706   0.04075   0.03811  -0.0815   1.0000   0.0197
 -13.750  -0.9965   0.03631   0.03345  -0.0813   1.0000   0.0198
 -13.500  -1.0026   0.03368   0.03065  -0.0797   1.0000   0.0199
 -13.250  -1.0026   0.03165   0.02846  -0.0777   1.0000   0.0200
 -13.000  -0.9986   0.02994   0.02661  -0.0756   1.0000   0.0201
 -12.750  -0.9918   0.02847   0.02499  -0.0735   1.0000   0.0202
 -12.500  -0.9828   0.02717   0.02356  -0.0713   1.0000   0.0203
 -12.250  -0.9621   0.02582   0.02207  -0.0714   0.9989   0.0204
 -12.000  -0.9360   0.02464   0.02075  -0.0723   0.9971   0.0205
 -11.750  -0.9081   0.02363   0.01962  -0.0733   0.9953   0.0207
 -11.500  -0.8791   0.02270   0.01857  -0.0745   0.9938   0.0208
 -11.250  -0.8546   0.02145   0.01718  -0.0749   0.9909   0.0209
 -11.000  -0.8290   0.02013   0.01573  -0.0755   0.9878   0.0211
 -10.750  -0.8008   0.01918   0.01470  -0.0763   0.9856   0.0213
 -10.500  -0.7715   0.01840   0.01385  -0.0771   0.9836   0.0215
 -10.250  -0.7460   0.01776   0.01314  -0.0770   0.9786   0.0216
 -10.000  -0.7175   0.01713   0.01245  -0.0774   0.9743   0.0218
  -9.750  -0.6892   0.01655   0.01180  -0.0778   0.9695   0.0219
  -9.500  -0.6617   0.01599   0.01119  -0.0779   0.9629   0.0221
  -9.250  -0.6334   0.01546   0.01058  -0.0782   0.9562   0.0223
  -9.000  -0.6055   0.01496   0.01002  -0.0783   0.9468   0.0225
  -8.750  -0.5781   0.01451   0.00949  -0.0782   0.9338   0.0227
  -8.500  -0.5515   0.01410   0.00898  -0.0779   0.9158   0.0230
  -8.250  -0.5261   0.01372   0.00847  -0.0774   0.8941   0.0232
  -8.000  -0.5008   0.01335   0.00798  -0.0768   0.8738   0.0233
  -7.750  -0.4751   0.01301   0.00752  -0.0763   0.8582   0.0235
  -7.500  -0.4491   0.01268   0.00708  -0.0759   0.8444   0.0237
  -7.250  -0.4228   0.01237   0.00667  -0.0755   0.8314   0.0239
  -7.000  -0.3962   0.01207   0.00629  -0.0752   0.8200   0.0240
  -6.750  -0.3695   0.01180   0.00593  -0.0748   0.8090   0.0242
  -6.500  -0.3426   0.01154   0.00560  -0.0746   0.7978   0.0243
  -6.250  -0.3155   0.01129   0.00528  -0.0743   0.7872   0.0244
  -6.000  -0.2886   0.01105   0.00496  -0.0740   0.7749   0.0246
  -5.750  -0.2623   0.01070   0.00452  -0.0736   0.7586   0.0250
  -5.500  -0.2356   0.01045   0.00419  -0.0733   0.7396   0.0253
  -5.250  -0.2087   0.01025   0.00391  -0.0730   0.7176   0.0256
  -5.000  -0.1817   0.01010   0.00366  -0.0727   0.6973   0.0259
  -4.750  -0.1544   0.00995   0.00345  -0.0724   0.6805   0.0263
  -4.500  -0.1270   0.00983   0.00325  -0.0722   0.6651   0.0267
  -4.250  -0.0995   0.00971   0.00307  -0.0720   0.6504   0.0271
  -4.000  -0.0720   0.00960   0.00289  -0.0718   0.6368   0.0275
  -3.500  -0.0164   0.00939   0.00257  -0.0715   0.6130   0.0282
  -3.250   0.0114   0.00931   0.00243  -0.0713   0.6014   0.0286
  -3.000   0.0390   0.00923   0.00229  -0.0712   0.5871   0.0290
  -2.750   0.0668   0.00913   0.00214  -0.0710   0.5726   0.0298
  -2.500   0.0946   0.00906   0.00203  -0.0709   0.5581   0.0306
  -2.250   0.1222   0.00903   0.00193  -0.0707   0.5379   0.0315
  -2.000   0.1496   0.00903   0.00184  -0.0705   0.5132   0.0326
  -1.500   0.2042   0.00907   0.00171  -0.0701   0.4657   0.0374
  -1.250   0.2313   0.00900   0.00167  -0.0699   0.4481   0.0578
  -1.000   0.2589   0.00900   0.00166  -0.0698   0.4339   0.0691
  -0.750   0.2867   0.00903   0.00165  -0.0697   0.4218   0.0746
  -0.500   0.3147   0.00904   0.00164  -0.0696   0.4122   0.0789
  -0.250   0.3425   0.00907   0.00164  -0.0695   0.4026   0.0834
   0.000   0.3707   0.00908   0.00164  -0.0694   0.3944   0.0872
   0.250   0.3984   0.00910   0.00166  -0.0693   0.3853   0.0952
   0.500   0.4264   0.00909   0.00167  -0.0693   0.3772   0.1072
   0.750   0.4541   0.00910   0.00170  -0.0692   0.3679   0.1255
   1.000   0.4819   0.00911   0.00173  -0.0691   0.3584   0.1425
   1.250   0.5095   0.00914   0.00177  -0.0690   0.3480   0.1604
   1.500   0.5368   0.00915   0.00182  -0.0689   0.3350   0.1921
   2.000   0.5891   0.00883   0.00198  -0.0685   0.3043   0.4262
   2.250   0.6138   0.00852   0.00209  -0.0681   0.2890   0.6058
   2.500   0.6295   0.00778   0.00229  -0.0652   0.2783   0.9429
   2.750   0.6742   0.00800   0.00244  -0.0688   0.2637   0.9907
   3.000   0.7178   0.00824   0.00257  -0.0723   0.2491   0.9984
   3.250   0.7481   0.00843   0.00269  -0.0729   0.2401   1.0000
   3.500   0.7730   0.00855   0.00278  -0.0722   0.2357   1.0000
   3.750   0.7977   0.00869   0.00288  -0.0716   0.2308   1.0000
   4.000   0.8222   0.00886   0.00300  -0.0708   0.2250   1.0000
   4.250   0.8473   0.00898   0.00311  -0.0702   0.2213   1.0000
   4.500   0.8724   0.00912   0.00322  -0.0696   0.2177   1.0000
   4.750   0.8976   0.00926   0.00334  -0.0691   0.2146   1.0000
   5.000   0.9228   0.00943   0.00348  -0.0685   0.2109   1.0000
   5.250   0.9483   0.00958   0.00362  -0.0680   0.2076   1.0000
   5.500   0.9743   0.00970   0.00375  -0.0677   0.2052   1.0000
   5.750   1.0001   0.00985   0.00389  -0.0673   0.2017   1.0000
   6.000   1.0253   0.01005   0.00405  -0.0668   0.1958   1.0000
   6.250   1.0510   0.01023   0.00422  -0.0664   0.1913   1.0000
   6.500   1.0766   0.01040   0.00438  -0.0660   0.1850   1.0000
   6.750   1.1015   0.01064   0.00457  -0.0655   0.1758   1.0000
   7.000   1.1177   0.01161   0.00517  -0.0638   0.1146   1.0000
   7.250   1.1398   0.01209   0.00556  -0.0629   0.0995   1.0000
   7.500   1.1624   0.01251   0.00593  -0.0620   0.0883   1.0000
   7.750   1.1842   0.01299   0.00633  -0.0611   0.0734   1.0000
   8.000   1.2006   0.01391   0.00702  -0.0594   0.0389   1.0000
   8.250   1.2228   0.01433   0.00742  -0.0586   0.0347   1.0000
   8.500   1.2457   0.01468   0.00777  -0.0578   0.0329   1.0000
   8.750   1.2683   0.01503   0.00813  -0.0571   0.0318   1.0000
   9.000   1.2903   0.01541   0.00852  -0.0562   0.0308   1.0000
   9.250   1.3117   0.01582   0.00894  -0.0553   0.0299   1.0000
   9.500   1.3324   0.01626   0.00939  -0.0543   0.0288   1.0000
   9.750   1.3534   0.01664   0.00981  -0.0533   0.0283   1.0000
  10.000   1.3739   0.01704   0.01024  -0.0523   0.0279   1.0000
  10.250   1.3935   0.01746   0.01069  -0.0511   0.0274   1.0000
  10.500   1.4111   0.01790   0.01115  -0.0496   0.0268   1.0000
  10.750   1.4275   0.01838   0.01167  -0.0479   0.0263   1.0000
  11.000   1.4433   0.01890   0.01222  -0.0461   0.0258   1.0000
  11.250   1.4583   0.01949   0.01285  -0.0444   0.0253   1.0000
  11.500   1.4720   0.02017   0.01356  -0.0426   0.0246   1.0000
  11.750   1.4844   0.02095   0.01439  -0.0407   0.0241   1.0000
  12.000   1.4994   0.02159   0.01507  -0.0392   0.0238   1.0000
  12.250   1.5137   0.02229   0.01582  -0.0377   0.0235   1.0000
  12.500   1.5274   0.02305   0.01663  -0.0363   0.0231   1.0000
  12.750   1.5403   0.02390   0.01754  -0.0349   0.0227   1.0000
  13.000   1.5524   0.02485   0.01853  -0.0336   0.0223   1.0000
  13.250   1.5636   0.02589   0.01963  -0.0323   0.0219   1.0000
  13.500   1.5740   0.02705   0.02084  -0.0311   0.0215   1.0000
  13.750   1.5833   0.02835   0.02219  -0.0299   0.0211   1.0000
  14.000   1.5908   0.02985   0.02374  -0.0288   0.0206   1.0000
  14.250   1.5959   0.03163   0.02559  -0.0278   0.0202   1.0000
  14.500   1.6034   0.03328   0.02730  -0.0270   0.0200   1.0000
  14.750   1.6103   0.03502   0.02912  -0.0263   0.0197   1.0000
  15.000   1.6159   0.03695   0.03113  -0.0257   0.0195   1.0000
  15.250   1.6206   0.03906   0.03331  -0.0253   0.0191   1.0000
  15.500   1.6244   0.04131   0.03564  -0.0250   0.0188   1.0000
  15.750   1.6265   0.04382   0.03823  -0.0248   0.0184   1.0000
  16.000   1.6275   0.04653   0.04101  -0.0248   0.0181   1.0000
  16.250   1.6270   0.04949   0.04405  -0.0249   0.0177   1.0000
  16.500   1.6241   0.05281   0.04745  -0.0252   0.0175   1.0000
  16.750   1.6194   0.05644   0.05116  -0.0256   0.0172   1.0000
  17.000   1.6125   0.06047   0.05529  -0.0263   0.0170   1.0000
  17.250   1.6027   0.06499   0.05991  -0.0272   0.0167   1.0000
  17.500   1.5943   0.06942   0.06445  -0.0282   0.0166   1.0000
  17.750   1.5846   0.07415   0.06928  -0.0294   0.0164   1.0000
  18.000   1.5736   0.07910   0.07435  -0.0307   0.0163   1.0000
  18.250   1.5610   0.08434   0.07969  -0.0322   0.0161   1.0000
  18.500   1.5485   0.08962   0.08508  -0.0337   0.0159   1.0000
  18.750   1.5358   0.09497   0.09054  -0.0354   0.0157   1.0000
  19.000   1.5226   0.10041   0.09607  -0.0371   0.0156   1.0000
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