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GOE 527 AIRFOIL (goe527-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 527 AIRFOIL (goe527-il)
Reynolds number: 500,000
Max Cl/Cd: 96.2 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe527-il-500000-n5.txt
Download as CSV file: xf-goe527-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 527 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.7041   0.04807   0.04454  -0.1064   0.9843   0.0267
 -14.250  -0.7136   0.03980   0.03603  -0.1174   0.9703   0.0268
 -14.000  -0.7036   0.03440   0.03040  -0.1269   0.9558   0.0270
 -13.750  -0.6772   0.03109   0.02691  -0.1347   0.9430   0.0273
 -13.500  -0.6458   0.02873   0.02435  -0.1408   0.9278   0.0276
 -13.250  -0.6209   0.02689   0.02228  -0.1442   0.9083   0.0279
 -13.000  -0.6081   0.02560   0.02078  -0.1439   0.8864   0.0282
 -12.750  -0.6023   0.02472   0.01971  -0.1415   0.8661   0.0285
 -12.250  -0.5830   0.02313   0.01776  -0.1373   0.8350   0.0290
 -12.000  -0.5700   0.02242   0.01687  -0.1354   0.8217   0.0293
 -11.750  -0.5556   0.02177   0.01603  -0.1336   0.8092   0.0295
 -11.500  -0.5412   0.02101   0.01516  -0.1319   0.7970   0.0298
 -11.250  -0.5253   0.02032   0.01438  -0.1303   0.7866   0.0301
 -11.000  -0.5076   0.01974   0.01371  -0.1288   0.7765   0.0303
 -10.750  -0.4887   0.01921   0.01309  -0.1275   0.7673   0.0306
 -10.500  -0.4693   0.01871   0.01249  -0.1262   0.7577   0.0309
 -10.250  -0.4488   0.01825   0.01194  -0.1251   0.7487   0.0313
 -10.000  -0.4280   0.01780   0.01138  -0.1239   0.7395   0.0316
  -9.750  -0.4063   0.01738   0.01087  -0.1229   0.7316   0.0321
  -9.500  -0.3843   0.01696   0.01035  -0.1219   0.7236   0.0325
  -9.250  -0.3621   0.01656   0.00984  -0.1209   0.7163   0.0329
  -9.000  -0.3392   0.01616   0.00936  -0.1200   0.7084   0.0333
  -8.750  -0.3164   0.01581   0.00890  -0.1190   0.7005   0.0336
  -8.500  -0.2940   0.01536   0.00839  -0.1181   0.6929   0.0340
  -8.250  -0.2711   0.01499   0.00797  -0.1172   0.6849   0.0345
  -8.000  -0.2474   0.01467   0.00759  -0.1164   0.6781   0.0350
  -7.750  -0.2232   0.01436   0.00723  -0.1156   0.6708   0.0355
  -7.500  -0.1990   0.01409   0.00689  -0.1148   0.6636   0.0361
  -7.250  -0.1743   0.01383   0.00657  -0.1141   0.6565   0.0367
  -7.000  -0.1497   0.01358   0.00625  -0.1134   0.6486   0.0374
  -6.750  -0.1250   0.01336   0.00595  -0.1127   0.6413   0.0382
  -6.500  -0.1003   0.01308   0.00565  -0.1120   0.6338   0.0390
  -6.250  -0.0756   0.01287   0.00539  -0.1113   0.6268   0.0400
  -6.000  -0.0501   0.01267   0.00514  -0.1107   0.6203   0.0410
  -5.750  -0.0247   0.01249   0.00491  -0.1101   0.6129   0.0421
  -5.500   0.0003   0.01233   0.00469  -0.1094   0.6060   0.0434
  -5.250   0.0260   0.01214   0.00449  -0.1089   0.5991   0.0451
  -5.000   0.0515   0.01200   0.00430  -0.1082   0.5924   0.0472
  -4.750   0.0771   0.01186   0.00414  -0.1077   0.5867   0.0500
  -4.500   0.1032   0.01173   0.00399  -0.1072   0.5805   0.0536
  -4.250   0.1288   0.01163   0.00388  -0.1066   0.5742   0.0581
  -4.000   0.1547   0.01155   0.00378  -0.1061   0.5687   0.0626
  -3.750   0.1812   0.01147   0.00368  -0.1057   0.5632   0.0675
  -3.500   0.2073   0.01141   0.00361  -0.1052   0.5580   0.0720
  -3.250   0.2332   0.01139   0.00353  -0.1046   0.5530   0.0759
  -3.000   0.2598   0.01131   0.00348  -0.1043   0.5482   0.0802
  -2.750   0.2863   0.01129   0.00342  -0.1039   0.5432   0.0842
  -2.500   0.3123   0.01124   0.00336  -0.1034   0.5387   0.0879
  -2.250   0.3382   0.01122   0.00331  -0.1029   0.5346   0.0917
  -2.000   0.3651   0.01118   0.00326  -0.1025   0.5304   0.0948
  -1.750   0.3912   0.01113   0.00321  -0.1021   0.5260   0.0987
  -1.500   0.4172   0.01110   0.00318  -0.1016   0.5219   0.1039
  -1.250   0.4430   0.01110   0.00315  -0.1011   0.5181   0.1093
  -1.000   0.4691   0.01104   0.00311  -0.1007   0.5146   0.1157
  -0.750   0.4955   0.01101   0.00309  -0.1003   0.5105   0.1207
  -0.500   0.5213   0.01097   0.00307  -0.0998   0.5063   0.1293
  -0.250   0.5463   0.01094   0.00306  -0.0992   0.5017   0.1442
   0.000   0.5709   0.01083   0.00307  -0.0986   0.4972   0.1868
   0.250   0.5958   0.01070   0.00309  -0.0980   0.4921   0.2372
   0.500   0.6200   0.01060   0.00313  -0.0973   0.4871   0.2890
   0.750   0.6432   0.01054   0.00317  -0.0964   0.4817   0.3437
   1.000   0.6674   0.01040   0.00323  -0.0957   0.4768   0.4102
   1.250   0.6907   0.01028   0.00330  -0.0948   0.4714   0.4806
   1.500   0.7128   0.01017   0.00338  -0.0937   0.4671   0.5553
   1.750   0.7342   0.01007   0.00347  -0.0924   0.4635   0.6252
   2.000   0.7544   0.00985   0.00357  -0.0908   0.4602   0.7240
   2.250   0.7890   0.00959   0.00382  -0.0918   0.4558   0.9185
   2.500   0.8518   0.00981   0.00400  -0.0992   0.4498   0.9726
   2.750   0.8930   0.00998   0.00411  -0.1021   0.4449   0.9843
   3.000   0.9351   0.01013   0.00424  -0.1052   0.4397   0.9981
   3.250   0.9617   0.01026   0.00434  -0.1051   0.4349   1.0000
   3.500   0.9803   0.01041   0.00444  -0.1033   0.4300   1.0000
   3.750   1.0005   0.01052   0.00453  -0.1018   0.4246   1.0000
   4.000   1.0193   0.01066   0.00464  -0.1000   0.4175   1.0000
   4.250   1.0368   0.01084   0.00476  -0.0980   0.4109   1.0000
   4.500   1.0563   0.01098   0.00489  -0.0964   0.4044   1.0000
   4.750   1.0722   0.01116   0.00503  -0.0941   0.3974   1.0000
   5.000   1.0885   0.01132   0.00517  -0.0919   0.3914   1.0000
   5.250   1.1047   0.01150   0.00532  -0.0897   0.3844   1.0000
   5.500   1.1196   0.01173   0.00551  -0.0873   0.3779   1.0000
   5.750   1.1373   0.01193   0.00569  -0.0855   0.3708   1.0000
   6.000   1.1520   0.01221   0.00593  -0.0831   0.3631   1.0000
   6.250   1.1693   0.01246   0.00616  -0.0814   0.3548   1.0000
   6.500   1.1834   0.01281   0.00646  -0.0791   0.3462   1.0000
   6.750   1.1994   0.01314   0.00676  -0.0772   0.3362   1.0000
   7.000   1.2135   0.01354   0.00712  -0.0750   0.3271   1.0000
   7.250   1.2269   0.01399   0.00753  -0.0729   0.3167   1.0000
   7.500   1.2413   0.01443   0.00794  -0.0709   0.3075   1.0000
   8.000   1.2686   0.01545   0.00891  -0.0670   0.2909   1.0000
   8.500   1.2953   0.01661   0.01003  -0.0634   0.2768   1.0000
   8.750   1.3080   0.01726   0.01068  -0.0616   0.2701   1.0000
   9.000   1.3209   0.01794   0.01135  -0.0600   0.2647   1.0000
   9.250   1.3345   0.01861   0.01203  -0.0585   0.2588   1.0000
   9.500   1.3455   0.01946   0.01286  -0.0568   0.2528   1.0000
   9.750   1.3578   0.02026   0.01367  -0.0553   0.2479   1.0000
  10.000   1.3712   0.02105   0.01448  -0.0540   0.2434   1.0000
  10.250   1.3823   0.02199   0.01543  -0.0526   0.2387   1.0000
  10.500   1.3924   0.02303   0.01647  -0.0512   0.2348   1.0000
  10.750   1.4053   0.02394   0.01742  -0.0501   0.2312   1.0000
  11.000   1.4178   0.02489   0.01840  -0.0491   0.2277   1.0000
  11.250   1.4286   0.02598   0.01952  -0.0480   0.2242   1.0000
  11.500   1.4374   0.02725   0.02080  -0.0468   0.2207   1.0000
  11.750   1.4465   0.02853   0.02211  -0.0457   0.2176   1.0000
  12.000   1.4590   0.02959   0.02323  -0.0449   0.2152   1.0000
  12.250   1.4699   0.03078   0.02447  -0.0441   0.2124   1.0000
  12.500   1.4795   0.03210   0.02584  -0.0432   0.2095   1.0000
  12.750   1.4873   0.03361   0.02738  -0.0423   0.2065   1.0000
  13.000   1.4935   0.03528   0.02907  -0.0414   0.2035   1.0000
  13.250   1.5027   0.03670   0.03055  -0.0407   0.2009   1.0000
  13.500   1.5127   0.03810   0.03202  -0.0401   0.1984   1.0000
  13.750   1.5213   0.03963   0.03361  -0.0395   0.1953   1.0000
  14.000   1.5249   0.04167   0.03566  -0.0388   0.1906   1.0000
  14.250   1.5283   0.04374   0.03777  -0.0381   0.1870   1.0000
  14.500   1.5365   0.04539   0.03947  -0.0377   0.1822   1.0000
  14.750   1.5390   0.04762   0.04174  -0.0371   0.1767   1.0000
  15.000   1.5408   0.04995   0.04410  -0.0366   0.1717   1.0000
  15.250   1.5423   0.05236   0.04653  -0.0362   0.1640   1.0000
  15.500   1.5408   0.05511   0.04929  -0.0358   0.1575   1.0000
  15.750   1.5379   0.05803   0.05222  -0.0354   0.1498   1.0000
  16.000   1.5334   0.06117   0.05536  -0.0351   0.1423   1.0000
  16.250   1.5283   0.06442   0.05862  -0.0349   0.1366   1.0000
  16.500   1.5248   0.06753   0.06176  -0.0347   0.1317   1.0000
  16.750   1.5223   0.07053   0.06479  -0.0346   0.1280   1.0000
  17.000   1.5196   0.07362   0.06792  -0.0346   0.1252   1.0000
  17.250   1.5179   0.07661   0.07096  -0.0346   0.1225   1.0000
  17.500   1.5189   0.07929   0.07371  -0.0347   0.1208   1.0000
  17.750   1.5187   0.08212   0.07660  -0.0348   0.1186   1.0000
  18.000   1.5151   0.08540   0.07992  -0.0350   0.1158   1.0000
  18.250   1.5113   0.08876   0.08332  -0.0353   0.1136   1.0000
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