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GOE 389 AIRFOIL (goe389-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 389 AIRFOIL (goe389-il)
Reynolds number: 1,000,000
Max Cl/Cd: 108.06 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe389-il-1000000-n5.txt
Download as CSV file: xf-goe389-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 389 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
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.9235   0.03616   0.03396  -0.0812   1.0000   0.0064
 -12.750  -0.9398   0.02981   0.02719  -0.0816   1.0000   0.0065
 -12.500  -0.9348   0.02699   0.02413  -0.0806   1.0000   0.0066
 -12.250  -0.9112   0.02454   0.02144  -0.0825   0.9979   0.0069
 -12.000  -0.8854   0.02269   0.01936  -0.0841   0.9957   0.0071
 -11.750  -0.8587   0.02120   0.01769  -0.0854   0.9937   0.0074
 -11.500  -0.8331   0.01971   0.01603  -0.0863   0.9903   0.0079
 -11.250  -0.8054   0.01848   0.01466  -0.0874   0.9874   0.0085
 -11.000  -0.7766   0.01746   0.01352  -0.0884   0.9850   0.0091
 -10.750  -0.7503   0.01661   0.01256  -0.0887   0.9797   0.0097
 -10.250  -0.6924   0.01525   0.01104  -0.0901   0.9700   0.0116
 -10.000  -0.6618   0.01473   0.01046  -0.0910   0.9643   0.0127
  -9.750  -0.6316   0.01424   0.00990  -0.0917   0.9562   0.0137
  -9.500  -0.5996   0.01414   0.00983  -0.0927   0.9474   0.0148
  -9.250  -0.5689   0.01403   0.00967  -0.0933   0.9357   0.0157
  -8.750  -0.5138   0.01358   0.00903  -0.0932   0.9092   0.0174
  -8.500  -0.4869   0.01340   0.00875  -0.0930   0.8976   0.0178
  -8.250  -0.4605   0.01308   0.00834  -0.0928   0.8873   0.0184
  -8.000  -0.4335   0.01293   0.00814  -0.0926   0.8766   0.0190
  -7.750  -0.4062   0.01284   0.00800  -0.0925   0.8652   0.0195
  -7.500  -0.3789   0.01277   0.00788  -0.0923   0.8521   0.0200
  -7.250  -0.3518   0.01270   0.00774  -0.0921   0.8363   0.0207
  -7.000  -0.3252   0.01253   0.00746  -0.0919   0.8160   0.0213
  -6.750  -0.2988   0.01237   0.00716  -0.0916   0.7914   0.0219
  -6.500  -0.2723   0.01219   0.00683  -0.0913   0.7710   0.0225
  -6.250  -0.2453   0.01202   0.00655  -0.0911   0.7559   0.0230
  -6.000  -0.2183   0.01183   0.00625  -0.0909   0.7431   0.0234
  -5.750  -0.1910   0.01161   0.00593  -0.0908   0.7324   0.0237
  -5.500  -0.1634   0.01144   0.00569  -0.0907   0.7234   0.0240
  -5.250  -0.1360   0.01117   0.00532  -0.0906   0.7155   0.0241
  -5.000  -0.1084   0.01089   0.00498  -0.0906   0.7093   0.0242
  -4.750  -0.0814   0.01035   0.00433  -0.0905   0.7028   0.0246
  -4.500  -0.0544   0.00980   0.00368  -0.0904   0.6969   0.0255
  -4.250  -0.0266   0.00948   0.00331  -0.0904   0.6911   0.0263
  -4.000   0.0012   0.00926   0.00303  -0.0903   0.6851   0.0268
  -3.750   0.0293   0.00906   0.00279  -0.0903   0.6789   0.0273
  -3.500   0.0573   0.00890   0.00258  -0.0903   0.6708   0.0278
  -3.250   0.0854   0.00874   0.00238  -0.0903   0.6629   0.0282
  -3.000   0.1134   0.00862   0.00220  -0.0903   0.6539   0.0286
  -2.750   0.1415   0.00850   0.00203  -0.0903   0.6423   0.0290
  -2.500   0.1694   0.00841   0.00188  -0.0902   0.6262   0.0294
  -2.250   0.1969   0.00838   0.00174  -0.0901   0.5998   0.0297
  -2.000   0.2228   0.00851   0.00164  -0.0897   0.5480   0.0300
  -1.750   0.2492   0.00864   0.00158  -0.0894   0.5082   0.0304
  -1.500   0.2763   0.00871   0.00153  -0.0893   0.4833   0.0308
  -1.250   0.3039   0.00873   0.00147  -0.0892   0.4676   0.0314
  -1.000   0.3317   0.00875   0.00143  -0.0892   0.4556   0.0321
  -0.750   0.3595   0.00877   0.00140  -0.0891   0.4442   0.0327
  -0.500   0.3875   0.00877   0.00136  -0.0891   0.4347   0.0354
  -0.250   0.4154   0.00876   0.00135  -0.0891   0.4268   0.0427
   0.000   0.4432   0.00870   0.00136  -0.0891   0.4191   0.0705
   0.250   0.4711   0.00870   0.00136  -0.0891   0.4119   0.0836
   0.500   0.4989   0.00857   0.00137  -0.0892   0.4057   0.1419
   0.750   0.5265   0.00853   0.00141  -0.0892   0.3981   0.1831
   1.000   0.5542   0.00844   0.00145  -0.0893   0.3902   0.2427
   1.250   0.5818   0.00840   0.00151  -0.0893   0.3838   0.2931
   1.500   0.6097   0.00837   0.00156  -0.0894   0.3785   0.3296
   1.750   0.6373   0.00830   0.00163  -0.0894   0.3720   0.3905
   2.000   0.6639   0.00794   0.00175  -0.0894   0.3668   0.5839
   2.250   0.6912   0.00706   0.00188  -0.0892   0.3618   1.0000
   2.500   0.7183   0.00719   0.00195  -0.0891   0.3529   1.0000
   2.750   0.7455   0.00732   0.00203  -0.0890   0.3417   1.0000
   3.000   0.7728   0.00745   0.00211  -0.0889   0.3336   1.0000
   3.250   0.8000   0.00758   0.00220  -0.0887   0.3258   1.0000
   3.500   0.8271   0.00772   0.00230  -0.0886   0.3160   1.0000
   3.750   0.8537   0.00790   0.00241  -0.0885   0.3028   1.0000
   4.000   0.8794   0.00819   0.00257  -0.0882   0.2793   1.0000
   4.250   0.9043   0.00855   0.00277  -0.0877   0.2500   1.0000
   4.500   0.9286   0.00897   0.00302  -0.0873   0.2180   1.0000
   4.750   0.9474   0.00998   0.00359  -0.0860   0.1343   1.0000
   5.000   0.9716   0.01042   0.00391  -0.0854   0.1124   1.0000
   5.250   0.9971   0.01070   0.00415  -0.0851   0.1026   1.0000
   5.500   1.0227   0.01098   0.00438  -0.0848   0.0945   1.0000
   5.750   1.0451   0.01158   0.00477  -0.0841   0.0589   1.0000
   6.000   1.0695   0.01196   0.00511  -0.0836   0.0458   1.0000
   6.250   1.0909   0.01265   0.00564  -0.0827   0.0173   1.0000
   6.500   1.1156   0.01297   0.00597  -0.0822   0.0133   1.0000
   6.750   1.1401   0.01330   0.00631  -0.0818   0.0118   1.0000
   7.000   1.1640   0.01367   0.00672  -0.0812   0.0101   1.0000
   7.250   1.1883   0.01400   0.00707  -0.0807   0.0094   1.0000
   7.500   1.2121   0.01434   0.00744  -0.0802   0.0088   1.0000
   7.750   1.2355   0.01472   0.00784  -0.0796   0.0082   1.0000
   8.000   1.2582   0.01514   0.00828  -0.0788   0.0076   1.0000
   8.250   1.2794   0.01567   0.00886  -0.0779   0.0070   1.0000
   8.500   1.3019   0.01606   0.00928  -0.0772   0.0067   1.0000
   8.750   1.3237   0.01649   0.00974  -0.0764   0.0063   1.0000
   9.000   1.3448   0.01696   0.01024  -0.0755   0.0060   1.0000
   9.250   1.3652   0.01746   0.01077  -0.0744   0.0057   1.0000
   9.500   1.3847   0.01798   0.01133  -0.0733   0.0054   1.0000
   9.750   1.4028   0.01858   0.01197  -0.0720   0.0051   1.0000
  10.000   1.4174   0.01937   0.01282  -0.0701   0.0049   1.0000
  10.250   1.4317   0.01999   0.01349  -0.0681   0.0048   1.0000
  10.500   1.4454   0.02066   0.01422  -0.0661   0.0046   1.0000
  10.750   1.4580   0.02140   0.01502  -0.0640   0.0045   1.0000
  11.000   1.4699   0.02220   0.01589  -0.0620   0.0044   1.0000
  11.250   1.4813   0.02307   0.01683  -0.0600   0.0042   1.0000
  11.500   1.4921   0.02400   0.01783  -0.0582   0.0041   1.0000
  11.750   1.5027   0.02500   0.01889  -0.0565   0.0039   1.0000
  12.000   1.5128   0.02609   0.02003  -0.0548   0.0038   1.0000
  12.250   1.5215   0.02733   0.02133  -0.0533   0.0037   1.0000
  12.500   1.5296   0.02868   0.02275  -0.0518   0.0036   1.0000
  12.750   1.5355   0.03028   0.02442  -0.0503   0.0035   1.0000
  13.000   1.5398   0.03212   0.02635  -0.0490   0.0034   1.0000
  13.250   1.5410   0.03435   0.02867  -0.0478   0.0033   1.0000
  13.500   1.5382   0.03714   0.03157  -0.0467   0.0032   1.0000
  13.750   1.5376   0.03985   0.03438  -0.0461   0.0032   1.0000
  14.000   1.5379   0.04252   0.03717  -0.0456   0.0032   1.0000
  14.250   1.5366   0.04549   0.04024  -0.0453   0.0031   1.0000
  14.500   1.5334   0.04873   0.04359  -0.0451   0.0031   1.0000
  14.750   1.5293   0.05221   0.04717  -0.0451   0.0031   1.0000
  15.000   1.5238   0.05604   0.05111  -0.0455   0.0031   1.0000
  15.250   1.5176   0.06010   0.05528  -0.0460   0.0030   1.0000
  15.500   1.5101   0.06449   0.05979  -0.0469   0.0030   1.0000
  15.750   1.5014   0.06919   0.06460  -0.0479   0.0030   1.0000
  16.000   1.4932   0.07390   0.06942  -0.0490   0.0029   1.0000
  16.250   1.4841   0.07878   0.07442  -0.0503   0.0029   1.0000
  16.500   1.4734   0.08397   0.07971  -0.0517   0.0029   1.0000
  16.750   1.4630   0.08917   0.08502  -0.0532   0.0029   1.0000
  17.000   1.4517   0.09451   0.09046  -0.0547   0.0028   1.0000
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