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GOE 383 AIRFOIL (goe383-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 383 AIRFOIL (goe383-il)
Reynolds number: 1,000,000
Max Cl/Cd: 111.72 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe383-il-1000000.txt
Download as CSV file: xf-goe383-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 383 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.1690   0.14770   0.14579  -0.0512   0.9055   0.0314
 -16.500  -0.7485   0.06968   0.06678  -0.0884   1.0000   0.0304
 -16.250  -0.7869   0.05994   0.05681  -0.0962   1.0000   0.0304
 -16.000  -0.8076   0.05297   0.04963  -0.1025   0.9844   0.0304
 -15.750  -0.8223   0.04787   0.04434  -0.1062   0.9718   0.0304
 -15.500  -0.8352   0.04397   0.04027  -0.1077   0.9600   0.0305
 -15.250  -0.8447   0.04083   0.03697  -0.1082   0.9493   0.0305
 -15.000  -0.8504   0.03810   0.03408  -0.1084   0.9386   0.0306
 -14.750  -0.8525   0.03575   0.03158  -0.1084   0.9283   0.0306
 -14.500  -0.8528   0.03376   0.02945  -0.1078   0.9174   0.0307
 -14.250  -0.8500   0.03203   0.02757  -0.1071   0.9048   0.0308
 -14.000  -0.8454   0.03054   0.02595  -0.1060   0.8909   0.0309
 -13.750  -0.8392   0.02927   0.02452  -0.1047   0.8751   0.0309
 -13.500  -0.8311   0.02816   0.02325  -0.1032   0.8577   0.0310
 -13.250  -0.8213   0.02721   0.02214  -0.1016   0.8394   0.0311
 -13.000  -0.8101   0.02642   0.02118  -0.0999   0.8211   0.0312
 -12.750  -0.7989   0.02577   0.02040  -0.0980   0.8036   0.0312
 -12.500  -0.7871   0.02399   0.01845  -0.0967   0.7877   0.0315
 -12.250  -0.7706   0.02292   0.01727  -0.0956   0.7718   0.0317
 -12.000  -0.7522   0.02215   0.01639  -0.0947   0.7556   0.0319
 -11.750  -0.7325   0.02149   0.01565  -0.0938   0.7397   0.0320
 -11.500  -0.7118   0.02092   0.01500  -0.0930   0.7251   0.0322
 -11.250  -0.6905   0.02041   0.01439  -0.0923   0.7114   0.0324
 -11.000  -0.6683   0.01994   0.01385  -0.0916   0.6999   0.0326
 -10.750  -0.6456   0.01950   0.01334  -0.0910   0.6900   0.0328
 -10.500  -0.6223   0.01907   0.01284  -0.0904   0.6821   0.0331
 -10.250  -0.5989   0.01864   0.01233  -0.0898   0.6743   0.0334
 -10.000  -0.5752   0.01817   0.01180  -0.0893   0.6680   0.0336
  -9.750  -0.5510   0.01770   0.01129  -0.0888   0.6624   0.0338
  -9.500  -0.5268   0.01727   0.01079  -0.0883   0.6561   0.0340
  -9.250  -0.5024   0.01689   0.01032  -0.0878   0.6490   0.0342
  -9.000  -0.4772   0.01646   0.00987  -0.0874   0.6454   0.0345
  -8.750  -0.4518   0.01609   0.00946  -0.0870   0.6415   0.0347
  -8.500  -0.4262   0.01575   0.00907  -0.0867   0.6372   0.0349
  -8.250  -0.4004   0.01546   0.00872  -0.0863   0.6323   0.0351
  -8.000  -0.3756   0.01505   0.00825  -0.0858   0.6272   0.0353
  -7.750  -0.3518   0.01442   0.00762  -0.0853   0.6248   0.0357
  -7.500  -0.3263   0.01402   0.00721  -0.0849   0.6223   0.0361
  -7.250  -0.2999   0.01371   0.00690  -0.0846   0.6196   0.0365
  -7.000  -0.2732   0.01345   0.00662  -0.0844   0.6166   0.0368
  -6.750  -0.2464   0.01321   0.00635  -0.0842   0.6134   0.0373
  -6.500  -0.2196   0.01300   0.00610  -0.0840   0.6097   0.0377
  -6.250  -0.1926   0.01281   0.00587  -0.0838   0.6059   0.0382
  -6.000  -0.1649   0.01257   0.00563  -0.0837   0.6042   0.0386
  -5.750  -0.1371   0.01237   0.00542  -0.0836   0.6021   0.0391
  -5.500  -0.1096   0.01213   0.00517  -0.0835   0.5997   0.0396
  -5.250  -0.0829   0.01181   0.00485  -0.0832   0.5972   0.0404
  -5.000  -0.0552   0.01162   0.00466  -0.0831   0.5944   0.0411
  -4.750  -0.0274   0.01147   0.00448  -0.0831   0.5912   0.0418
  -4.500   0.0004   0.01135   0.00433  -0.0830   0.5874   0.0426
  -4.250   0.0286   0.01123   0.00419  -0.0830   0.5843   0.0434
  -4.000   0.0567   0.01102   0.00398  -0.0829   0.5822   0.0444
  -3.750   0.0849   0.01082   0.00381  -0.0829   0.5798   0.0457
  -3.500   0.1134   0.01068   0.00368  -0.0830   0.5770   0.0471
  -3.250   0.1421   0.01057   0.00356  -0.0830   0.5739   0.0485
  -3.000   0.1699   0.01041   0.00339  -0.0829   0.5707   0.0509
  -2.750   0.1980   0.01034   0.00329  -0.0829   0.5667   0.0534
  -2.500   0.2261   0.01019   0.00317  -0.0829   0.5634   0.0580
  -2.250   0.2541   0.00996   0.00302  -0.0829   0.5605   0.0700
  -2.000   0.2806   0.00957   0.00290  -0.0828   0.5570   0.1317
  -1.500   0.3354   0.00919   0.00273  -0.0826   0.5487   0.1948
  -1.250   0.3619   0.00897   0.00270  -0.0825   0.5440   0.2545
  -1.000   0.3903   0.00880   0.00267  -0.0826   0.5406   0.2923
  -0.750   0.4186   0.00867   0.00264  -0.0827   0.5359   0.3255
  -0.500   0.4459   0.00852   0.00261  -0.0826   0.5304   0.3681
  -0.250   0.4722   0.00833   0.00259  -0.0824   0.5244   0.4337
   0.000   0.4994   0.00810   0.00258  -0.0824   0.5187   0.5047
   0.250   0.5255   0.00791   0.00260  -0.0821   0.5114   0.5789
   0.500   0.5518   0.00781   0.00265  -0.0818   0.5043   0.6389
   0.750   0.5792   0.00778   0.00270  -0.0817   0.4960   0.6793
   1.000   0.6055   0.00780   0.00277  -0.0813   0.4867   0.7144
   1.250   0.6326   0.00782   0.00283  -0.0812   0.4773   0.7421
   1.500   0.6590   0.00791   0.00291  -0.0808   0.4678   0.7615
   1.750   0.6859   0.00797   0.00300  -0.0807   0.4594   0.7811
   2.000   0.7119   0.00809   0.00310  -0.0803   0.4504   0.7985
   2.750   0.7891   0.00837   0.00346  -0.0790   0.4275   0.8674
   3.000   0.8134   0.00848   0.00361  -0.0782   0.4216   0.8941
   3.250   0.8368   0.00865   0.00377  -0.0773   0.4157   0.9179
   3.500   0.8625   0.00873   0.00390  -0.0768   0.4125   0.9395
   3.750   0.8898   0.00886   0.00403  -0.0766   0.4087   0.9568
   4.000   0.9198   0.00904   0.00419  -0.0772   0.4043   0.9700
   4.250   0.9517   0.00927   0.00438  -0.0782   0.3994   0.9809
   4.500   0.9881   0.00946   0.00455  -0.0802   0.3960   0.9875
   4.750   1.0255   0.00961   0.00470  -0.0824   0.3929   0.9924
   5.000   1.0657   0.00980   0.00486  -0.0853   0.3890   0.9951
   5.250   1.1061   0.01003   0.00506  -0.0882   0.3848   0.9985
   5.500   1.1313   0.01026   0.00525  -0.0881   0.3806   1.0000
   5.750   1.1458   0.01036   0.00535  -0.0856   0.3782   1.0000
   6.000   1.1633   0.01045   0.00545  -0.0837   0.3760   1.0000
   6.250   1.1798   0.01056   0.00557  -0.0817   0.3732   1.0000
   6.500   1.1957   0.01072   0.00572  -0.0795   0.3700   1.0000
   6.750   1.2128   0.01094   0.00592  -0.0777   0.3664   1.0000
   7.000   1.2294   0.01126   0.00620  -0.0760   0.3618   1.0000
   7.250   1.2534   0.01139   0.00636  -0.0755   0.3591   1.0000
   7.500   1.2759   0.01158   0.00657  -0.0748   0.3555   1.0000
   7.750   1.2969   0.01185   0.00682  -0.0740   0.3513   1.0000
   8.000   1.3156   0.01221   0.00716  -0.0728   0.3464   1.0000
   8.250   1.3373   0.01249   0.00744  -0.0721   0.3429   1.0000
   8.500   1.3602   0.01273   0.00770  -0.0717   0.3393   1.0000
   8.750   1.3808   0.01306   0.00803  -0.0709   0.3348   1.0000
   9.000   1.3988   0.01352   0.00847  -0.0698   0.3295   1.0000
   9.250   1.4199   0.01387   0.00883  -0.0692   0.3246   1.0000
   9.500   1.4393   0.01429   0.00925  -0.0684   0.3180   1.0000
   9.750   1.4550   0.01491   0.00982  -0.0671   0.3107   1.0000
  10.000   1.4736   0.01541   0.01032  -0.0663   0.3026   1.0000
  10.250   1.4875   0.01617   0.01104  -0.0650   0.2935   1.0000
  10.500   1.5019   0.01693   0.01177  -0.0638   0.2839   1.0000
  10.750   1.5147   0.01781   0.01263  -0.0625   0.2749   1.0000
  11.250   1.5379   0.01983   0.01460  -0.0600   0.2577   1.0000
  11.500   1.5459   0.02113   0.01587  -0.0585   0.2497   1.0000
  11.750   1.5580   0.02220   0.01694  -0.0575   0.2430   1.0000
  12.250   1.5754   0.02489   0.01962  -0.0552   0.2300   1.0000
  12.500   1.5817   0.02648   0.02120  -0.0540   0.2238   1.0000
  12.750   1.5906   0.02791   0.02265  -0.0530   0.2189   1.0000
  13.000   1.5995   0.02939   0.02414  -0.0522   0.2143   1.0000
  13.250   1.6042   0.03122   0.02598  -0.0511   0.2095   1.0000
  13.500   1.6124   0.03281   0.02760  -0.0504   0.2056   1.0000
  13.750   1.6201   0.03447   0.02929  -0.0497   0.2014   1.0000
  14.000   1.6234   0.03653   0.03136  -0.0488   0.1969   1.0000
  14.250   1.6287   0.03842   0.03326  -0.0480   0.1930   1.0000
  14.500   1.6357   0.04021   0.03510  -0.0474   0.1893   1.0000
  14.750   1.6393   0.04231   0.03721  -0.0467   0.1850   1.0000
  15.000   1.6398   0.04473   0.03965  -0.0460   0.1807   1.0000
  15.250   1.6465   0.04658   0.04154  -0.0455   0.1767   1.0000
  15.500   1.6466   0.04908   0.04405  -0.0448   0.1718   1.0000
  15.750   1.6471   0.05157   0.04657  -0.0442   0.1671   1.0000
  16.000   1.6481   0.05405   0.04906  -0.0437   0.1614   1.0000
  16.250   1.6440   0.05704   0.05206  -0.0431   0.1556   1.0000
  16.500   1.6404   0.06001   0.05503  -0.0426   0.1481   1.0000
  16.750   1.6321   0.06357   0.05859  -0.0420   0.1393   1.0000
  17.000   1.6162   0.06797   0.06296  -0.0414   0.1268   1.0000
  17.250   1.5833   0.07433   0.06923  -0.0408   0.1055   1.0000
  17.500   1.5448   0.08158   0.07639  -0.0404   0.0852   1.0000
  17.750   1.5220   0.08718   0.08200  -0.0404   0.0773   1.0000
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