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GOE 776 AIRFOIL (goe776-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 776 AIRFOIL (goe776-il)
Reynolds number: 500,000
Max Cl/Cd: 48.52 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe776-il-500000-n5.txt
Download as CSV file: xf-goe776-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 776 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -1.1566   0.09063   0.08519  -0.0439   1.0000   0.0899
 -19.250  -1.1557   0.08769   0.08219  -0.0448   1.0000   0.0914
 -19.000  -1.1604   0.08408   0.07855  -0.0458   1.0000   0.0930
 -18.750  -1.1643   0.08058   0.07500  -0.0468   1.0000   0.0947
 -18.500  -1.1651   0.07750   0.07187  -0.0475   1.0000   0.0964
 -18.250  -1.1653   0.07450   0.06881  -0.0482   1.0000   0.0981
 -18.000  -1.1628   0.07186   0.06611  -0.0488   1.0000   0.0997
 -17.750  -1.1669   0.06847   0.06269  -0.0495   1.0000   0.1014
 -17.500  -1.1677   0.06552   0.05970  -0.0500   1.0000   0.1032
 -17.250  -1.1670   0.06274   0.05687  -0.0505   1.0000   0.1051
 -17.000  -1.1640   0.06025   0.05433  -0.0508   1.0000   0.1069
 -16.750  -1.1611   0.05778   0.05181  -0.0511   1.0000   0.1085
 -16.500  -1.1622   0.05493   0.04893  -0.0514   1.0000   0.1104
 -16.250  -1.1600   0.05247   0.04644  -0.0515   1.0000   0.1124
 -16.000  -1.1565   0.05018   0.04410  -0.0516   1.0000   0.1145
 -15.750  -1.1506   0.04816   0.04204  -0.0516   1.0000   0.1164
 -15.500  -1.1468   0.04598   0.03982  -0.0515   1.0000   0.1183
 -15.250  -1.1443   0.04372   0.03754  -0.0513   1.0000   0.1204
 -15.000  -1.1389   0.04180   0.03559  -0.0510   1.0000   0.1228
 -14.750  -1.1322   0.04003   0.03379  -0.0507   1.0000   0.1251
 -14.500  -1.1246   0.03842   0.03213  -0.0502   1.0000   0.1272
 -14.250  -1.1203   0.03659   0.03029  -0.0496   1.0000   0.1296
 -14.000  -1.1149   0.03493   0.02862  -0.0488   1.0000   0.1322
 -13.750  -1.1074   0.03355   0.02721  -0.0479   1.0000   0.1349
 -13.500  -1.0995   0.03231   0.02594  -0.0468   1.0000   0.1372
 -13.250  -1.0969   0.03088   0.02451  -0.0452   1.0000   0.1398
 -13.000  -1.0939   0.02968   0.02330  -0.0432   1.0000   0.1426
 -12.750  -1.0911   0.02864   0.02225  -0.0410   1.0000   0.1454
 -12.500  -1.0766   0.02761   0.02119  -0.0406   0.9983   0.1484
 -12.250  -1.0570   0.02631   0.01990  -0.0416   0.9951   0.1523
 -12.000  -1.0342   0.02523   0.01881  -0.0428   0.9924   0.1566
 -11.750  -1.0106   0.02428   0.01785  -0.0439   0.9892   0.1606
 -11.500  -0.9916   0.02322   0.01681  -0.0442   0.9833   0.1651
 -11.250  -0.9682   0.02236   0.01594  -0.0450   0.9782   0.1700
 -11.000  -0.9472   0.02152   0.01510  -0.0453   0.9717   0.1744
 -10.750  -0.9273   0.02069   0.01429  -0.0453   0.9638   0.1794
 -10.500  -0.9053   0.02004   0.01362  -0.0453   0.9563   0.1841
 -10.250  -0.8882   0.01931   0.01289  -0.0445   0.9456   0.1886
 -10.000  -0.8704   0.01868   0.01226  -0.0436   0.9353   0.1936
  -9.750  -0.8519   0.01816   0.01170  -0.0426   0.9235   0.1981
  -9.500  -0.8358   0.01759   0.01112  -0.0412   0.9110   0.2028
  -9.250  -0.8189   0.01708   0.01058  -0.0398   0.8984   0.2078
  -9.000  -0.8001   0.01667   0.01013  -0.0386   0.8844   0.2124
  -8.750  -0.7828   0.01621   0.00965  -0.0373   0.8708   0.2174
  -8.500  -0.7649   0.01580   0.00919  -0.0359   0.8560   0.2229
  -8.250  -0.7445   0.01548   0.00883  -0.0349   0.8415   0.2280
  -8.000  -0.7259   0.01511   0.00842  -0.0336   0.8273   0.2330
  -7.750  -0.7066   0.01479   0.00806  -0.0324   0.8124   0.2387
  -7.500  -0.6851   0.01453   0.00775  -0.0315   0.7987   0.2442
  -7.250  -0.6659   0.01423   0.00741  -0.0302   0.7845   0.2500
  -7.000  -0.6452   0.01396   0.00712  -0.0291   0.7705   0.2561
  -6.750  -0.6229   0.01377   0.00686  -0.0282   0.7573   0.2613
  -6.500  -0.6028   0.01351   0.00658  -0.0270   0.7433   0.2673
  -6.250  -0.5814   0.01330   0.00634  -0.0260   0.7306   0.2740
  -6.000  -0.5589   0.01314   0.00613  -0.0251   0.7173   0.2796
  -5.750  -0.5383   0.01292   0.00589  -0.0238   0.7053   0.2860
  -5.500  -0.5166   0.01276   0.00570  -0.0228   0.6925   0.2926
  -5.250  -0.4943   0.01262   0.00553  -0.0218   0.6812   0.2987
  -5.000  -0.4748   0.01246   0.00536  -0.0202   0.6691   0.3057
  -4.750  -0.4536   0.01236   0.00523  -0.0190   0.6583   0.3128
  -4.500  -0.4338   0.01226   0.00510  -0.0174   0.6469   0.3193
  -4.250  -0.4138   0.01215   0.00499  -0.0159   0.6367   0.3266
  -4.000  -0.3909   0.01209   0.00489  -0.0149   0.6256   0.3331
  -3.750  -0.3693   0.01199   0.00478  -0.0137   0.6159   0.3399
  -3.500  -0.3463   0.01189   0.00468  -0.0128   0.6056   0.3473
  -3.000  -0.2999   0.01175   0.00451  -0.0109   0.5855   0.3608
  -2.750  -0.2766   0.01170   0.00444  -0.0100   0.5752   0.3683
  -2.500  -0.2521   0.01166   0.00437  -0.0093   0.5654   0.3748
  -2.250  -0.2294   0.01158   0.00430  -0.0082   0.5548   0.3824
  -2.000  -0.2055   0.01155   0.00425  -0.0074   0.5454   0.3900
  -1.750  -0.1809   0.01151   0.00420  -0.0067   0.5350   0.3968
  -1.500  -0.1583   0.01148   0.00415  -0.0056   0.5247   0.4048
  -1.250  -0.1333   0.01144   0.00411  -0.0050   0.5149   0.4126
  -1.000  -0.1099   0.01143   0.00408  -0.0041   0.5046   0.4199
  -0.750  -0.0858   0.01139   0.00405  -0.0033   0.4951   0.4286
  -0.500  -0.0614   0.01141   0.00404  -0.0025   0.4847   0.4364
  -0.250  -0.0380   0.01137   0.00402  -0.0016   0.4757   0.4450
   0.000  -0.0138   0.01137   0.00401  -0.0008   0.4658   0.4542
   0.250   0.0098   0.01138   0.00401   0.0001   0.4569   0.4627
   0.500   0.0340   0.01136   0.00401   0.0009   0.4480   0.4728
   0.750   0.0578   0.01141   0.00403   0.0017   0.4390   0.4818
   1.000   0.0817   0.01139   0.00404   0.0025   0.4314   0.4920
   1.250   0.1062   0.01142   0.00407   0.0033   0.4228   0.5019
   1.500   0.1290   0.01144   0.00411   0.0043   0.4149   0.5119
   1.750   0.1541   0.01146   0.00414   0.0049   0.4076   0.5221
   2.000   0.1774   0.01149   0.00418   0.0059   0.3995   0.5320
   2.250   0.2011   0.01154   0.00424   0.0067   0.3924   0.5427
   2.500   0.2256   0.01157   0.00429   0.0074   0.3851   0.5520
   2.750   0.2485   0.01163   0.00435   0.0084   0.3774   0.5627
   3.000   0.2726   0.01170   0.00442   0.0092   0.3706   0.5724
   3.250   0.2961   0.01173   0.00449   0.0101   0.3635   0.5829
   3.500   0.3190   0.01183   0.00458   0.0111   0.3560   0.5926
   3.750   0.3424   0.01188   0.00466   0.0120   0.3498   0.6028
   4.000   0.3657   0.01195   0.00475   0.0129   0.3427   0.6136
   4.250   0.3872   0.01207   0.00486   0.0141   0.3354   0.6230
   4.500   0.4102   0.01213   0.00496   0.0151   0.3293   0.6341
   4.750   0.4312   0.01223   0.00507   0.0164   0.3221   0.6444
   5.000   0.4498   0.01234   0.00520   0.0182   0.3153   0.6556
   5.500   0.4919   0.01256   0.00548   0.0207   0.3017   0.6786
   6.000   0.5352   0.01286   0.00585   0.0229   0.2888   0.7026
   6.250   0.5564   0.01308   0.00606   0.0240   0.2822   0.7149
   6.500   0.5780   0.01325   0.00629   0.0251   0.2766   0.7279
   6.750   0.6002   0.01344   0.00652   0.0260   0.2703   0.7407
   7.000   0.6203   0.01370   0.00679   0.0272   0.2638   0.7547
   7.250   0.6421   0.01391   0.00705   0.0282   0.2585   0.7677
   7.500   0.6634   0.01415   0.00733   0.0292   0.2526   0.7822
   7.750   0.6826   0.01446   0.00767   0.0304   0.2466   0.7960
   8.000   0.7040   0.01472   0.00798   0.0314   0.2412   0.8100
   8.250   0.7239   0.01502   0.00833   0.0325   0.2354   0.8246
   8.500   0.7421   0.01540   0.00874   0.0338   0.2300   0.8388
   8.750   0.7626   0.01572   0.00910   0.0349   0.2252   0.8537
   9.000   0.7812   0.01610   0.00953   0.0361   0.2197   0.8681
   9.250   0.7979   0.01658   0.01003   0.0376   0.2143   0.8821
   9.500   0.8169   0.01697   0.01047   0.0387   0.2099   0.8962
   9.750   0.8346   0.01745   0.01098   0.0400   0.2049   0.9087
  10.000   0.8501   0.01804   0.01157   0.0415   0.1999   0.9218
  10.250   0.8687   0.01855   0.01213   0.0425   0.1955   0.9333
  10.500   0.8867   0.01914   0.01272   0.0434   0.1906   0.9441
  10.750   0.9037   0.01989   0.01346   0.0442   0.1859   0.9547
  11.000   0.9251   0.02052   0.01412   0.0443   0.1813   0.9629
  11.250   0.9464   0.02129   0.01488   0.0442   0.1763   0.9705
  11.500   0.9656   0.02219   0.01576   0.0442   0.1718   0.9776
  11.750   0.9902   0.02298   0.01656   0.0432   0.1671   0.9826
  12.000   1.0103   0.02397   0.01754   0.0428   0.1625   0.9885
  12.250   1.0324   0.02499   0.01856   0.0419   0.1585   0.9922
  12.500   1.0563   0.02601   0.01960   0.0407   0.1543   0.9948
  12.750   1.0771   0.02720   0.02079   0.0396   0.1502   0.9980
  13.000   1.0909   0.02836   0.02196   0.0398   0.1471   1.0000
  13.250   1.0947   0.02933   0.02295   0.0421   0.1443   1.0000
  13.500   1.0986   0.03046   0.02409   0.0440   0.1415   1.0000
  13.750   1.1020   0.03183   0.02546   0.0456   0.1387   1.0000
  14.000   1.1083   0.03317   0.02681   0.0468   0.1363   1.0000
  14.250   1.1164   0.03451   0.02819   0.0477   0.1336   1.0000
  14.500   1.1231   0.03605   0.02975   0.0484   0.1310   1.0000
  14.750   1.1284   0.03779   0.03150   0.0490   0.1284   1.0000
  15.000   1.1340   0.03959   0.03332   0.0495   0.1262   1.0000
  15.250   1.1419   0.04123   0.03501   0.0499   0.1240   1.0000
  15.500   1.1477   0.04313   0.03694   0.0501   0.1216   1.0000
  15.750   1.1512   0.04528   0.03911   0.0503   0.1193   1.0000
  16.000   1.1537   0.04757   0.04143   0.0504   0.1172   1.0000
  16.250   1.1599   0.04957   0.04348   0.0504   0.1153   1.0000
  16.500   1.1645   0.05174   0.04569   0.0504   0.1132   1.0000
  16.750   1.1668   0.05420   0.04819   0.0502   0.1111   1.0000
  17.000   1.1665   0.05697   0.05099   0.0500   0.1092   1.0000
  17.250   1.1687   0.05950   0.05355   0.0497   0.1075   1.0000
  17.500   1.1716   0.06201   0.05612   0.0493   0.1057   1.0000
  17.750   1.1733   0.06467   0.05883   0.0489   0.1038   1.0000
  18.000   1.1722   0.06767   0.06187   0.0484   0.1019   1.0000
  18.250   1.1688   0.07098   0.06521   0.0477   0.1002   1.0000
  18.500   1.1704   0.07372   0.06800   0.0471   0.0986   1.0000
  18.750   1.1706   0.07668   0.07103   0.0464   0.0968   1.0000
  19.000   1.1703   0.07970   0.07410   0.0457   0.0951   1.0000
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