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GOE 766 AIRFOIL (goe766-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 766 AIRFOIL (goe766-il)
Reynolds number: 1,000,000
Max Cl/Cd: 87.22 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe766-il-1000000-n5.txt
Download as CSV file: xf-goe766-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 766 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
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -1.1636   0.10619   0.10344  -0.0119   1.0000   0.0170
 -19.000  -1.2778   0.08261   0.07954  -0.0261   1.0000   0.0166
 -18.750  -1.3425   0.06779   0.06446  -0.0354   1.0000   0.0164
 -18.500  -1.3739   0.05888   0.05535  -0.0412   1.0000   0.0165
 -18.250  -1.3950   0.05209   0.04839  -0.0455   1.0000   0.0166
 -18.000  -1.4075   0.04702   0.04318  -0.0484   1.0000   0.0166
 -17.750  -1.4142   0.04309   0.03912  -0.0502   1.0000   0.0168
 -17.500  -1.4179   0.03977   0.03568  -0.0514   1.0000   0.0170
 -17.250  -1.4178   0.03713   0.03293  -0.0520   1.0000   0.0171
 -17.000  -1.4178   0.03466   0.03037  -0.0522   1.0000   0.0174
 -16.750  -1.4160   0.03256   0.02818  -0.0519   1.0000   0.0176
 -16.500  -1.4099   0.03099   0.02656  -0.0512   1.0000   0.0179
 -16.250  -1.4040   0.02953   0.02502  -0.0503   1.0000   0.0182
 -16.000  -1.3960   0.02831   0.02375  -0.0491   1.0000   0.0185
 -15.750  -1.3876   0.02721   0.02257  -0.0477   1.0000   0.0187
 -15.500  -1.3789   0.02620   0.02150  -0.0461   1.0000   0.0190
 -15.250  -1.3690   0.02531   0.02054  -0.0443   1.0000   0.0193
 -15.000  -1.3590   0.02448   0.01964  -0.0424   1.0000   0.0196
 -14.750  -1.3484   0.02373   0.01881  -0.0403   1.0000   0.0198
 -14.500  -1.3370   0.02307   0.01808  -0.0382   1.0000   0.0201
 -14.250  -1.3252   0.02247   0.01741  -0.0359   1.0000   0.0203
 -14.000  -1.3150   0.02183   0.01672  -0.0333   1.0000   0.0206
 -13.750  -1.3029   0.02123   0.01609  -0.0309   1.0000   0.0209
 -13.500  -1.2871   0.02068   0.01550  -0.0291   1.0000   0.0212
 -13.250  -1.2699   0.02018   0.01497  -0.0274   1.0000   0.0216
 -13.000  -1.2522   0.01970   0.01445  -0.0258   1.0000   0.0219
 -12.750  -1.2339   0.01923   0.01394  -0.0243   1.0000   0.0222
 -12.500  -1.2152   0.01877   0.01344  -0.0228   1.0000   0.0226
 -12.250  -1.1957   0.01835   0.01297  -0.0214   1.0000   0.0230
 -12.000  -1.1759   0.01795   0.01252  -0.0200   1.0000   0.0233
 -11.750  -1.1559   0.01754   0.01206  -0.0185   1.0000   0.0236
 -11.500  -1.1356   0.01715   0.01162  -0.0172   1.0000   0.0238
 -11.250  -1.1168   0.01663   0.01106  -0.0156   1.0000   0.0242
 -11.000  -1.0971   0.01617   0.01058  -0.0141   1.0000   0.0247
 -10.750  -1.0767   0.01576   0.01016  -0.0127   1.0000   0.0250
 -10.500  -1.0556   0.01540   0.00978  -0.0114   1.0000   0.0254
 -10.250  -1.0345   0.01505   0.00940  -0.0101   1.0000   0.0258
 -10.000  -1.0131   0.01472   0.00905  -0.0087   1.0000   0.0262
  -9.750  -0.9917   0.01440   0.00871  -0.0074   1.0000   0.0266
  -9.500  -0.9704   0.01408   0.00835  -0.0060   1.0000   0.0270
  -9.250  -0.9492   0.01376   0.00800  -0.0046   1.0000   0.0273
  -9.000  -0.9277   0.01347   0.00768  -0.0033   1.0000   0.0276
  -8.750  -0.9014   0.01315   0.00734  -0.0029   0.9992   0.0280
  -8.500  -0.8697   0.01270   0.00688  -0.0038   0.9964   0.0286
  -8.250  -0.8398   0.01234   0.00652  -0.0042   0.9922   0.0291
  -8.000  -0.8098   0.01203   0.00620  -0.0046   0.9871   0.0296
  -7.500  -0.7481   0.01144   0.00559  -0.0057   0.9764   0.0308
  -7.250  -0.7115   0.01115   0.00530  -0.0075   0.9703   0.0314
  -7.000  -0.6744   0.01088   0.00500  -0.0094   0.9597   0.0320
  -6.750  -0.6345   0.01056   0.00466  -0.0119   0.9448   0.0327
  -6.500  -0.5979   0.01027   0.00434  -0.0136   0.9203   0.0338
  -6.250  -0.5697   0.01012   0.00409  -0.0134   0.8871   0.0346
  -6.000  -0.5456   0.01004   0.00388  -0.0123   0.8419   0.0354
  -5.750  -0.5231   0.01003   0.00367  -0.0109   0.7836   0.0363
  -5.500  -0.5003   0.01005   0.00348  -0.0096   0.7266   0.0371
  -5.250  -0.4766   0.01002   0.00330  -0.0086   0.6797   0.0384
  -5.000  -0.4525   0.00999   0.00313  -0.0076   0.6308   0.0400
  -4.750  -0.4280   0.00999   0.00297  -0.0068   0.5826   0.0416
  -4.500  -0.4026   0.00997   0.00282  -0.0061   0.5452   0.0431
  -4.000  -0.3509   0.00981   0.00253  -0.0049   0.5006   0.0482
  -3.750  -0.3244   0.00973   0.00240  -0.0044   0.4851   0.0508
  -3.500  -0.2981   0.00961   0.00227  -0.0039   0.4725   0.0549
  -3.250  -0.2716   0.00952   0.00216  -0.0034   0.4600   0.0596
  -3.000  -0.2454   0.00942   0.00204  -0.0029   0.4475   0.0678
  -2.750  -0.2192   0.00926   0.00192  -0.0024   0.4372   0.0821
  -2.500  -0.1932   0.00911   0.00183  -0.0018   0.4282   0.1026
  -2.250  -0.1667   0.00898   0.00176  -0.0014   0.4199   0.1206
  -2.000  -0.1399   0.00891   0.00169  -0.0010   0.4117   0.1329
  -1.750  -0.1128   0.00884   0.00164  -0.0006   0.4040   0.1431
  -1.250  -0.0590   0.00870   0.00153   0.0002   0.3866   0.1675
  -0.750  -0.0072   0.00838   0.00141   0.0013   0.3703   0.2398
  -0.500   0.0166   0.00803   0.00134   0.0021   0.3619   0.3293
  -0.250   0.0417   0.00781   0.00130   0.0028   0.3542   0.3917
   0.000   0.0668   0.00762   0.00127   0.0035   0.3450   0.4469
   0.250   0.0904   0.00733   0.00125   0.0045   0.3368   0.5335
   0.500   0.1153   0.00721   0.00125   0.0052   0.3269   0.5889
   0.750   0.1414   0.00716   0.00127   0.0058   0.3164   0.6207
   1.000   0.1672   0.00713   0.00130   0.0064   0.3057   0.6533
   1.250   0.1924   0.00709   0.00133   0.0072   0.2950   0.6905
   1.500   0.2177   0.00704   0.00137   0.0080   0.2869   0.7265
   1.750   0.2435   0.00705   0.00142   0.0086   0.2781   0.7514
   2.000   0.2694   0.00704   0.00147   0.0093   0.2716   0.7762
   2.250   0.2950   0.00706   0.00153   0.0100   0.2636   0.8029
   2.500   0.3208   0.00706   0.00161   0.0107   0.2576   0.8288
   2.750   0.3467   0.00707   0.00169   0.0114   0.2511   0.8584
   3.000   0.3732   0.00712   0.00178   0.0119   0.2437   0.8875
   3.250   0.4023   0.00718   0.00188   0.0119   0.2362   0.9113
   3.500   0.4360   0.00730   0.00202   0.0109   0.2296   0.9323
   3.750   0.4719   0.00741   0.00214   0.0094   0.2247   0.9456
   4.000   0.5062   0.00759   0.00226   0.0081   0.2155   0.9542
   4.250   0.5413   0.00773   0.00238   0.0067   0.2088   0.9605
   4.500   0.5758   0.00787   0.00250   0.0053   0.2031   0.9655
   4.750   0.6053   0.00803   0.00262   0.0051   0.1972   0.9711
   5.000   0.6389   0.00816   0.00275   0.0040   0.1921   0.9733
   5.250   0.6706   0.00835   0.00288   0.0032   0.1841   0.9760
   5.500   0.7009   0.00850   0.00302   0.0028   0.1768   0.9795
   5.750   0.7292   0.00871   0.00317   0.0027   0.1672   0.9830
   6.000   0.7616   0.00894   0.00334   0.0017   0.1546   0.9847
   6.250   0.7929   0.00923   0.00355   0.0009   0.1392   0.9867
   6.500   0.8231   0.00957   0.00380   0.0003   0.1226   0.9890
   6.750   0.8525   0.00989   0.00406  -0.0002   0.1103   0.9914
   7.000   0.8813   0.01021   0.00432  -0.0005   0.1003   0.9936
   7.250   0.9125   0.01054   0.00460  -0.0014   0.0907   0.9952
   7.500   0.9432   0.01087   0.00488  -0.0021   0.0822   0.9969
   7.750   0.9741   0.01118   0.00516  -0.0029   0.0752   0.9984
   8.000   1.0048   0.01152   0.00546  -0.0037   0.0685   0.9996
   8.250   1.0295   0.01183   0.00576  -0.0032   0.0642   1.0000
   8.500   1.0505   0.01213   0.00605  -0.0020   0.0607   1.0000
   8.750   1.0720   0.01240   0.00633  -0.0007   0.0582   1.0000
   9.000   1.0930   0.01271   0.00664   0.0005   0.0558   1.0000
   9.250   1.1136   0.01306   0.00698   0.0018   0.0531   1.0000
   9.500   1.1351   0.01334   0.00728   0.0030   0.0518   1.0000
   9.750   1.1562   0.01364   0.00760   0.0042   0.0500   1.0000
  10.000   1.1767   0.01399   0.00796   0.0055   0.0483   1.0000
  10.250   1.1967   0.01438   0.00835   0.0068   0.0465   1.0000
  10.500   1.2172   0.01472   0.00872   0.0080   0.0454   1.0000
  10.750   1.2378   0.01505   0.00908   0.0092   0.0444   1.0000
  11.000   1.2579   0.01541   0.00946   0.0105   0.0434   1.0000
  11.250   1.2774   0.01580   0.00988   0.0118   0.0422   1.0000
  11.500   1.2962   0.01625   0.01034   0.0132   0.0410   1.0000
  11.750   1.3141   0.01673   0.01084   0.0147   0.0397   1.0000
  12.000   1.3330   0.01713   0.01129   0.0160   0.0392   1.0000
  12.250   1.3515   0.01754   0.01174   0.0174   0.0384   1.0000
  12.500   1.3690   0.01799   0.01222   0.0189   0.0375   1.0000
  12.750   1.3854   0.01848   0.01274   0.0205   0.0364   1.0000
  13.000   1.4001   0.01903   0.01332   0.0223   0.0354   1.0000
  13.250   1.4125   0.01965   0.01397   0.0244   0.0344   1.0000
  13.500   1.4228   0.02018   0.01455   0.0270   0.0340   1.0000
  13.750   1.4336   0.02072   0.01515   0.0293   0.0334   1.0000
  14.000   1.4437   0.02138   0.01585   0.0315   0.0327   1.0000
  14.250   1.4533   0.02213   0.01665   0.0334   0.0320   1.0000
  14.500   1.4620   0.02302   0.01761   0.0352   0.0316   1.0000
  14.750   1.4696   0.02408   0.01872   0.0367   0.0311   1.0000
  15.000   1.4755   0.02539   0.02008   0.0379   0.0304   1.0000
  15.250   1.4797   0.02699   0.02175   0.0387   0.0298   1.0000
  15.500   1.4843   0.02877   0.02361   0.0391   0.0294   1.0000
  15.750   1.4883   0.03084   0.02577   0.0389   0.0290   1.0000
  16.000   1.4916   0.03323   0.02826   0.0382   0.0286   1.0000
  16.250   1.4919   0.03616   0.03129   0.0371   0.0281   1.0000
  16.500   1.4899   0.03955   0.03477   0.0356   0.0277   1.0000
  16.750   1.4844   0.04346   0.03878   0.0338   0.0272   1.0000
  17.000   1.4744   0.04798   0.04341   0.0317   0.0269   1.0000
  17.250   1.4617   0.05282   0.04837   0.0296   0.0268   1.0000
  17.500   1.4447   0.05819   0.05383   0.0273   0.0263   1.0000
  17.750   1.4256   0.06380   0.05956   0.0250   0.0262   1.0000
  18.000   1.4045   0.06978   0.06566   0.0224   0.0261   1.0000
  18.250   1.3825   0.07606   0.07203   0.0197   0.0257   1.0000
  18.500   1.3634   0.08215   0.07823   0.0169   0.0257   1.0000
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