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GOE 676 (= M 12) AIRFOIL (goe676-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 676 (= M 12) AIRFOIL (goe676-il)
Reynolds number: 1,000,000
Max Cl/Cd: 85.93 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe676-il-1000000-n5.txt
Download as CSV file: xf-goe676-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 676 (= M 12) 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -1.3002   0.05011   0.04712  -0.0501   1.0000   0.0078
 -16.750  -1.3239   0.04369   0.04049  -0.0538   1.0000   0.0078
 -16.500  -1.3383   0.03950   0.03612  -0.0547   1.0000   0.0079
 -16.250  -1.3472   0.03637   0.03285  -0.0543   1.0000   0.0081
 -16.000  -1.3518   0.03392   0.03027  -0.0531   1.0000   0.0082
 -15.750  -1.3529   0.03193   0.02815  -0.0515   1.0000   0.0084
 -15.500  -1.3511   0.03027   0.02637  -0.0496   1.0000   0.0087
 -15.250  -1.3469   0.02884   0.02484  -0.0474   1.0000   0.0089
 -15.000  -1.3408   0.02761   0.02349  -0.0452   1.0000   0.0091
 -14.750  -1.3317   0.02651   0.02228  -0.0431   1.0000   0.0094
 -14.500  -1.3186   0.02548   0.02115  -0.0416   1.0000   0.0096
 -14.250  -1.3036   0.02454   0.02011  -0.0403   1.0000   0.0099
 -14.000  -1.2884   0.02352   0.01899  -0.0390   1.0000   0.0104
 -13.750  -1.2718   0.02258   0.01798  -0.0378   1.0000   0.0109
 -13.500  -1.2538   0.02174   0.01707  -0.0368   1.0000   0.0115
 -13.250  -1.2346   0.02098   0.01624  -0.0358   1.0000   0.0120
 -13.000  -1.2146   0.02029   0.01546  -0.0349   1.0000   0.0126
 -12.750  -1.1941   0.01961   0.01473  -0.0341   1.0000   0.0133
 -12.500  -1.1729   0.01900   0.01409  -0.0333   1.0000   0.0142
 -12.250  -1.1510   0.01846   0.01350  -0.0326   1.0000   0.0152
 -12.000  -1.1288   0.01795   0.01294  -0.0319   1.0000   0.0160
 -11.750  -1.1064   0.01745   0.01239  -0.0312   1.0000   0.0167
 -11.500  -1.0836   0.01703   0.01195  -0.0306   1.0000   0.0175
 -11.250  -1.0607   0.01665   0.01154  -0.0299   1.0000   0.0184
 -11.000  -1.0378   0.01627   0.01113  -0.0291   0.9997   0.0191
 -10.750  -1.0079   0.01587   0.01068  -0.0299   0.9952   0.0198
 -10.500  -0.9781   0.01551   0.01025  -0.0306   0.9901   0.0204
 -10.250  -0.9484   0.01504   0.00975  -0.0314   0.9843   0.0212
 -10.000  -0.9197   0.01469   0.00939  -0.0318   0.9767   0.0220
  -9.750  -0.8917   0.01437   0.00904  -0.0321   0.9685   0.0227
  -9.500  -0.8651   0.01408   0.00870  -0.0319   0.9594   0.0233
  -9.250  -0.8399   0.01381   0.00838  -0.0315   0.9493   0.0240
  -9.000  -0.8148   0.01355   0.00806  -0.0310   0.9394   0.0246
  -8.750  -0.7900   0.01330   0.00773  -0.0304   0.9291   0.0250
  -8.500  -0.7645   0.01307   0.00744  -0.0299   0.9180   0.0253
  -8.250  -0.7403   0.01266   0.00696  -0.0293   0.9063   0.0261
  -8.000  -0.7155   0.01232   0.00657  -0.0287   0.8938   0.0269
  -7.750  -0.6900   0.01207   0.00627  -0.0283   0.8813   0.0276
  -7.500  -0.6641   0.01185   0.00599  -0.0279   0.8696   0.0283
  -7.250  -0.6378   0.01161   0.00569  -0.0276   0.8596   0.0289
  -7.000  -0.6115   0.01139   0.00540  -0.0273   0.8502   0.0295
  -6.750  -0.5848   0.01117   0.00512  -0.0271   0.8407   0.0301
  -6.500  -0.5581   0.01095   0.00484  -0.0269   0.8323   0.0305
  -6.250  -0.5312   0.01075   0.00457  -0.0267   0.8240   0.0309
  -6.000  -0.5041   0.01056   0.00433  -0.0266   0.8164   0.0312
  -5.750  -0.4775   0.01030   0.00401  -0.0263   0.8082   0.0320
  -5.500  -0.4504   0.01006   0.00374  -0.0262   0.8006   0.0330
  -5.250  -0.4232   0.00988   0.00353  -0.0261   0.7920   0.0340
  -5.000  -0.3958   0.00971   0.00333  -0.0260   0.7833   0.0352
  -4.750  -0.3684   0.00956   0.00314  -0.0259   0.7730   0.0362
  -4.500  -0.3408   0.00942   0.00295  -0.0258   0.7607   0.0372
  -4.250  -0.3132   0.00930   0.00278  -0.0257   0.7469   0.0380
  -4.000  -0.2858   0.00916   0.00259  -0.0256   0.7308   0.0401
  -3.750  -0.2585   0.00906   0.00244  -0.0255   0.7103   0.0426
  -3.500  -0.2311   0.00899   0.00230  -0.0254   0.6870   0.0452
  -3.250  -0.2035   0.00894   0.00217  -0.0253   0.6676   0.0477
  -3.000  -0.1759   0.00885   0.00206  -0.0253   0.6535   0.0521
  -2.750  -0.1480   0.00878   0.00196  -0.0253   0.6417   0.0558
  -2.500  -0.1201   0.00871   0.00186  -0.0253   0.6315   0.0607
  -2.250  -0.0921   0.00863   0.00178  -0.0254   0.6220   0.0656
  -2.000  -0.0639   0.00858   0.00170  -0.0254   0.6140   0.0685
  -1.750  -0.0359   0.00851   0.00162  -0.0255   0.6053   0.0743
  -1.500  -0.0077   0.00844   0.00154  -0.0255   0.5982   0.0800
  -1.250   0.0204   0.00836   0.00148  -0.0256   0.5906   0.0894
  -1.000   0.0481   0.00822   0.00143  -0.0256   0.5832   0.1177
  -0.750   0.0759   0.00813   0.00139  -0.0257   0.5725   0.1431
  -0.500   0.1038   0.00804   0.00135  -0.0257   0.5603   0.1669
  -0.250   0.1311   0.00788   0.00130  -0.0257   0.5496   0.2110
   0.000   0.1569   0.00749   0.00124  -0.0255   0.5387   0.3250
   0.250   0.1824   0.00712   0.00120  -0.0253   0.5247   0.4431
   0.500   0.2078   0.00679   0.00116  -0.0250   0.5086   0.5510
   0.750   0.2322   0.00643   0.00115  -0.0245   0.4919   0.6751
   1.000   0.2575   0.00625   0.00118  -0.0240   0.4750   0.7509
   1.250   0.2823   0.00615   0.00126  -0.0232   0.4576   0.8242
   1.500   0.3083   0.00619   0.00134  -0.0227   0.4405   0.8629
   1.750   0.3355   0.00629   0.00141  -0.0225   0.4254   0.8787
   2.000   0.3625   0.00640   0.00149  -0.0223   0.4081   0.8917
   2.250   0.3889   0.00653   0.00158  -0.0219   0.3910   0.9070
   2.500   0.4153   0.00665   0.00168  -0.0215   0.3770   0.9205
   2.750   0.4423   0.00677   0.00176  -0.0214   0.3642   0.9291
   3.000   0.4694   0.00690   0.00185  -0.0212   0.3528   0.9351
   3.250   0.4967   0.00701   0.00193  -0.0211   0.3420   0.9414
   3.500   0.5239   0.00713   0.00203  -0.0209   0.3323   0.9472
   3.750   0.5505   0.00728   0.00214  -0.0206   0.3209   0.9549
   4.000   0.5774   0.00745   0.00226  -0.0204   0.3065   0.9624
   4.250   0.6052   0.00761   0.00238  -0.0205   0.2931   0.9676
   4.500   0.6327   0.00775   0.00248  -0.0205   0.2830   0.9717
   4.750   0.6624   0.00792   0.00262  -0.0210   0.2706   0.9744
   5.000   0.6914   0.00822   0.00279  -0.0215   0.2445   0.9778
   5.250   0.7180   0.00869   0.00305  -0.0216   0.1996   0.9820
   5.500   0.7444   0.00935   0.00343  -0.0219   0.1428   0.9850
   5.750   0.7744   0.00967   0.00367  -0.0227   0.1272   0.9867
   6.250   0.8347   0.01017   0.00412  -0.0242   0.1123   0.9906
   6.500   0.8642   0.01044   0.00436  -0.0248   0.1059   0.9926
   6.750   0.8940   0.01067   0.00459  -0.0255   0.1002   0.9942
   7.000   0.9248   0.01089   0.00481  -0.0264   0.0951   0.9953
   7.250   0.9547   0.01119   0.00507  -0.0273   0.0877   0.9967
   7.500   0.9847   0.01146   0.00532  -0.0281   0.0790   0.9983
   7.750   1.0126   0.01197   0.00569  -0.0286   0.0574   1.0000
   8.000   1.0294   0.01247   0.00608  -0.0268   0.0420   1.0000
   8.250   1.0483   0.01287   0.00645  -0.0253   0.0352   1.0000
   8.500   1.0683   0.01323   0.00680  -0.0240   0.0313   1.0000
   8.750   1.0894   0.01357   0.00714  -0.0230   0.0284   1.0000
   9.000   1.1107   0.01394   0.00751  -0.0221   0.0257   1.0000
   9.250   1.1320   0.01434   0.00791  -0.0211   0.0230   1.0000
   9.500   1.1538   0.01471   0.00829  -0.0203   0.0208   1.0000
   9.750   1.1746   0.01516   0.00873  -0.0194   0.0184   1.0000
  10.000   1.1960   0.01555   0.00916  -0.0186   0.0170   1.0000
  10.250   1.2164   0.01602   0.00963  -0.0177   0.0154   1.0000
  10.500   1.2363   0.01650   0.01013  -0.0167   0.0141   1.0000
  10.750   1.2562   0.01696   0.01061  -0.0157   0.0131   1.0000
  11.000   1.2750   0.01747   0.01115  -0.0146   0.0122   1.0000
  11.250   1.2923   0.01804   0.01174  -0.0132   0.0114   1.0000
  11.500   1.3071   0.01861   0.01235  -0.0115   0.0108   1.0000
  11.750   1.3223   0.01917   0.01296  -0.0098   0.0105   1.0000
  12.000   1.3369   0.01979   0.01363  -0.0082   0.0100   1.0000
  12.250   1.3509   0.02049   0.01437  -0.0067   0.0096   1.0000
  12.500   1.3640   0.02127   0.01520  -0.0052   0.0092   1.0000
  12.750   1.3762   0.02216   0.01613  -0.0037   0.0088   1.0000
  13.000   1.3869   0.02319   0.01721  -0.0022   0.0084   1.0000
  13.250   1.3983   0.02421   0.01830  -0.0010   0.0081   1.0000
  13.500   1.4100   0.02526   0.01942   0.0001   0.0079   1.0000
  13.750   1.4205   0.02645   0.02067   0.0011   0.0077   1.0000
  14.000   1.4302   0.02775   0.02203   0.0021   0.0075   1.0000
  14.250   1.4390   0.02919   0.02354   0.0029   0.0073   1.0000
  14.500   1.4467   0.03077   0.02519   0.0037   0.0071   1.0000
  14.750   1.4533   0.03251   0.02700   0.0043   0.0069   1.0000
  15.000   1.4588   0.03442   0.02898   0.0048   0.0067   1.0000
  15.250   1.4625   0.03656   0.03120   0.0052   0.0065   1.0000
  15.500   1.4647   0.03896   0.03368   0.0054   0.0064   1.0000
  15.750   1.4646   0.04170   0.03652   0.0055   0.0062   1.0000
  16.000   1.4638   0.04459   0.03949   0.0053   0.0061   1.0000
  16.250   1.4641   0.04744   0.04244   0.0050   0.0060   1.0000
  16.500   1.4629   0.05053   0.04563   0.0046   0.0060   1.0000
  16.750   1.4603   0.05386   0.04906   0.0040   0.0059   1.0000
  17.000   1.4563   0.05747   0.05278   0.0032   0.0058   1.0000
  17.250   1.4512   0.06135   0.05676   0.0023   0.0058   1.0000
  17.500   1.4445   0.06551   0.06103   0.0011   0.0057   1.0000
  17.750   1.4365   0.06998   0.06560  -0.0003   0.0057   1.0000
  18.000   1.4275   0.07471   0.07044  -0.0018   0.0056   1.0000
  18.250   1.4172   0.07972   0.07556  -0.0036   0.0055   1.0000
  18.500   1.4052   0.08506   0.08102  -0.0056   0.0055   1.0000
  18.750   1.3928   0.09060   0.08667  -0.0077   0.0055   1.0000
  19.000   1.3793   0.09638   0.09256  -0.0100   0.0054   1.0000
  19.250   1.3643   0.10244   0.09873  -0.0125   0.0054   1.0000
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