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GOE 367 AIRFOIL (goe367-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 367 AIRFOIL (goe367-il)
Reynolds number: 1,000,000
Max Cl/Cd: 111.26 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe367-il-1000000.txt
Download as CSV file: xf-goe367-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 367 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.9174   0.04620   0.04328  -0.1083   1.0000   0.0290
 -15.750  -0.9365   0.04050   0.03741  -0.1127   1.0000   0.0291
 -15.500  -0.9502   0.03750   0.03431  -0.1128   1.0000   0.0292
 -15.250  -0.9463   0.03523   0.03194  -0.1140   0.9972   0.0294
 -15.000  -0.9317   0.03329   0.02990  -0.1160   0.9940   0.0296
 -14.750  -0.9190   0.03158   0.02810  -0.1170   0.9878   0.0298
 -14.500  -0.9052   0.02999   0.02639  -0.1176   0.9812   0.0301
 -14.250  -0.8990   0.02864   0.02491  -0.1162   0.9696   0.0303
 -14.000  -0.8948   0.02751   0.02365  -0.1137   0.9575   0.0305
 -13.750  -0.8891   0.02652   0.02254  -0.1110   0.9468   0.0307
 -13.250  -0.8687   0.02474   0.02051  -0.1068   0.9282   0.0311
 -13.000  -0.8545   0.02393   0.01955  -0.1051   0.9200   0.0313
 -12.750  -0.8377   0.02315   0.01866  -0.1039   0.9115   0.0316
 -12.250  -0.8003   0.02188   0.01715  -0.1017   0.8951   0.0319
 -12.000  -0.7863   0.02053   0.01562  -0.1001   0.8868   0.0323
 -11.750  -0.7676   0.01962   0.01463  -0.0991   0.8792   0.0327
 -11.500  -0.7459   0.01910   0.01405  -0.0984   0.8714   0.0331
 -11.250  -0.7231   0.01863   0.01353  -0.0977   0.8642   0.0334
 -11.000  -0.7000   0.01818   0.01301  -0.0972   0.8565   0.0337
 -10.750  -0.6768   0.01773   0.01247  -0.0965   0.8495   0.0341
 -10.500  -0.6528   0.01727   0.01195  -0.0961   0.8427   0.0344
 -10.250  -0.6289   0.01684   0.01142  -0.0956   0.8354   0.0348
 -10.000  -0.6046   0.01640   0.01090  -0.0951   0.8280   0.0352
  -9.750  -0.5800   0.01600   0.01041  -0.0946   0.8201   0.0356
  -9.500  -0.5550   0.01564   0.00995  -0.0942   0.8130   0.0359
  -9.250  -0.5293   0.01530   0.00955  -0.0939   0.8069   0.0362
  -9.000  -0.5048   0.01479   0.00894  -0.0935   0.8009   0.0366
  -8.750  -0.4813   0.01413   0.00823  -0.0929   0.7953   0.0373
  -8.500  -0.4552   0.01380   0.00789  -0.0927   0.7901   0.0379
  -8.250  -0.4289   0.01353   0.00758  -0.0925   0.7847   0.0384
  -8.000  -0.4026   0.01327   0.00726  -0.0923   0.7795   0.0390
  -7.750  -0.3758   0.01299   0.00695  -0.0922   0.7750   0.0396
  -7.500  -0.3490   0.01272   0.00664  -0.0920   0.7701   0.0402
  -7.250  -0.3221   0.01249   0.00635  -0.0919   0.7653   0.0407
  -7.000  -0.2950   0.01231   0.00610  -0.0917   0.7605   0.0412
  -6.750  -0.2695   0.01181   0.00559  -0.0914   0.7564   0.0420
  -6.500  -0.2429   0.01150   0.00527  -0.0912   0.7517   0.0429
  -6.250  -0.2158   0.01130   0.00504  -0.0911   0.7472   0.0437
  -6.000  -0.1885   0.01114   0.00484  -0.0910   0.7425   0.0446
  -5.750  -0.1607   0.01095   0.00464  -0.0910   0.7384   0.0456
  -5.500  -0.1328   0.01081   0.00446  -0.0910   0.7338   0.0464
  -5.250  -0.1064   0.01051   0.00413  -0.0908   0.7292   0.0476
  -5.000  -0.0795   0.01029   0.00389  -0.0906   0.7243   0.0489
  -4.750  -0.0517   0.01011   0.00371  -0.0906   0.7196   0.0502
  -4.500  -0.0242   0.00996   0.00354  -0.0906   0.7134   0.0515
  -4.250   0.0033   0.00988   0.00339  -0.0905   0.7069   0.0526
  -4.000   0.0304   0.00961   0.00314  -0.0904   0.7013   0.0549
  -3.750   0.0580   0.00946   0.00299  -0.0903   0.6957   0.0570
  -3.500   0.0855   0.00938   0.00286  -0.0902   0.6900   0.0589
  -3.250   0.1132   0.00919   0.00269  -0.0902   0.6851   0.0620
  -3.000   0.1409   0.00906   0.00257  -0.0902   0.6794   0.0655
  -2.750   0.1682   0.00894   0.00245  -0.0901   0.6736   0.0711
  -2.500   0.1959   0.00880   0.00237  -0.0901   0.6678   0.0829
  -2.250   0.2235   0.00869   0.00233  -0.0901   0.6609   0.0993
  -2.000   0.2511   0.00867   0.00230  -0.0900   0.6538   0.1091
  -1.750   0.2793   0.00860   0.00227  -0.0901   0.6466   0.1168
  -1.500   0.3069   0.00860   0.00223  -0.0901   0.6387   0.1223
  -1.250   0.3348   0.00854   0.00220  -0.0901   0.6309   0.1289
  -1.000   0.3622   0.00856   0.00217  -0.0900   0.6217   0.1331
  -0.750   0.3899   0.00853   0.00214  -0.0900   0.6125   0.1387
  -0.500   0.4166   0.00853   0.00212  -0.0898   0.6021   0.1451
  -0.250   0.4441   0.00854   0.00210  -0.0898   0.5910   0.1498
   0.000   0.4707   0.00854   0.00210  -0.0896   0.5801   0.1594
   0.500   0.5233   0.00853   0.00211  -0.0891   0.5578   0.1927
   0.750   0.5467   0.00823   0.00213  -0.0885   0.5473   0.3175
   1.000   0.5669   0.00765   0.00217  -0.0874   0.5368   0.5421
   1.250   0.5801   0.00684   0.00232  -0.0844   0.5284   0.8518
   1.500   0.6029   0.00697   0.00249  -0.0831   0.5190   0.8970
   1.750   0.6266   0.00710   0.00262  -0.0821   0.5104   0.9189
   2.000   0.6479   0.00729   0.00277  -0.0805   0.5005   0.9342
   2.250   0.6698   0.00742   0.00289  -0.0790   0.4917   0.9453
   2.500   0.6915   0.00760   0.00300  -0.0777   0.4818   0.9534
   2.750   0.7155   0.00770   0.00309  -0.0767   0.4735   0.9597
   3.250   0.7652   0.00799   0.00330  -0.0754   0.4571   0.9718
   3.750   0.8199   0.00831   0.00353  -0.0754   0.4397   0.9809
   4.000   0.8582   0.00857   0.00372  -0.0779   0.4295   0.9834
   4.250   0.8964   0.00876   0.00387  -0.0804   0.4199   0.9848
   4.500   0.9284   0.00897   0.00402  -0.0816   0.4102   0.9862
   4.750   0.9630   0.00918   0.00418  -0.0834   0.4004   0.9881
   5.000   1.0024   0.00943   0.00439  -0.0861   0.3919   0.9914
   5.250   1.0352   0.00965   0.00456  -0.0875   0.3837   0.9933
   5.500   1.0651   0.00983   0.00471  -0.0883   0.3767   0.9941
   5.750   1.0952   0.01000   0.00487  -0.0892   0.3698   0.9951
   6.000   1.1240   0.01025   0.00506  -0.0898   0.3622   0.9964
   6.250   1.1532   0.01042   0.00522  -0.0905   0.3556   0.9976
   6.500   1.1807   0.01066   0.00543  -0.0909   0.3487   0.9989
   6.750   1.2083   0.01086   0.00562  -0.0913   0.3436   1.0000
   7.000   1.2079   0.01093   0.00571  -0.0857   0.3401   1.0000
   7.250   1.1988   0.01097   0.00577  -0.0784   0.3368   1.0000
   7.500   1.2050   0.01115   0.00594  -0.0744   0.3324   1.0000
   7.750   1.2228   0.01137   0.00616  -0.0728   0.3280   1.0000
   8.000   1.2434   0.01160   0.00639  -0.0718   0.3231   1.0000
   8.250   1.2629   0.01191   0.00669  -0.0707   0.3174   1.0000
   8.500   1.2828   0.01224   0.00701  -0.0697   0.3122   1.0000
   8.750   1.3041   0.01252   0.00730  -0.0689   0.3063   1.0000
   9.000   1.3221   0.01296   0.00770  -0.0677   0.2982   1.0000
   9.250   1.3428   0.01330   0.00805  -0.0670   0.2910   1.0000
   9.500   1.3598   0.01382   0.00852  -0.0657   0.2813   1.0000
   9.750   1.3782   0.01429   0.00897  -0.0646   0.2699   1.0000
  10.000   1.3908   0.01507   0.00964  -0.0628   0.2501   1.0000
  10.250   1.3884   0.01668   0.01098  -0.0592   0.2012   1.0000
  10.500   1.3814   0.01867   0.01272  -0.0552   0.1640   1.0000
  10.750   1.3895   0.01986   0.01385  -0.0532   0.1511   1.0000
  11.000   1.4007   0.02089   0.01486  -0.0518   0.1404   1.0000
  11.250   1.4086   0.02216   0.01606  -0.0500   0.1251   1.0000
  11.500   1.4050   0.02425   0.01796  -0.0472   0.0944   1.0000
  11.750   1.4117   0.02571   0.01939  -0.0456   0.0874   1.0000
  12.000   1.4200   0.02708   0.02077  -0.0442   0.0840   1.0000
  12.250   1.4289   0.02845   0.02216  -0.0430   0.0806   1.0000
  12.500   1.4408   0.02963   0.02340  -0.0421   0.0792   1.0000
  12.750   1.4515   0.03094   0.02475  -0.0412   0.0777   1.0000
  13.000   1.4604   0.03240   0.02625  -0.0402   0.0760   1.0000
  13.250   1.4672   0.03408   0.02797  -0.0391   0.0742   1.0000
  13.500   1.4725   0.03593   0.02986  -0.0380   0.0721   1.0000
  13.750   1.4806   0.03758   0.03156  -0.0372   0.0706   1.0000
  14.000   1.4914   0.03901   0.03305  -0.0366   0.0694   1.0000
  14.250   1.5008   0.04057   0.03466  -0.0360   0.0679   1.0000
  14.500   1.5072   0.04245   0.03659  -0.0353   0.0661   1.0000
  14.750   1.5111   0.04460   0.03877  -0.0345   0.0641   1.0000
  15.000   1.5147   0.04683   0.04105  -0.0338   0.0621   1.0000
  15.250   1.5248   0.04846   0.04273  -0.0335   0.0603   1.0000
  15.500   1.5307   0.05048   0.04479  -0.0330   0.0577   1.0000
  15.750   1.5323   0.05301   0.04733  -0.0325   0.0548   1.0000
  16.000   1.5375   0.05521   0.04959  -0.0321   0.0517   1.0000
  16.250   1.5372   0.05803   0.05241  -0.0317   0.0478   1.0000
  16.500   1.5368   0.06090   0.05530  -0.0314   0.0438   1.0000
  16.750   1.5337   0.06410   0.05853  -0.0311   0.0406   1.0000
  17.000   1.5290   0.06755   0.06201  -0.0309   0.0379   1.0000
  17.250   1.5244   0.07105   0.06556  -0.0308   0.0358   1.0000
  17.500   1.5195   0.07464   0.06920  -0.0308   0.0342   1.0000
  17.750   1.5121   0.07854   0.07315  -0.0309   0.0327   1.0000
  18.000   1.5077   0.08211   0.07680  -0.0311   0.0315   1.0000
  18.250   1.5039   0.08564   0.08039  -0.0313   0.0305   1.0000
  18.500   1.4975   0.08957   0.08438  -0.0317   0.0295   1.0000
  18.750   1.4895   0.09371   0.08858  -0.0321   0.0286   1.0000
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