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GOE 776 AIRFOIL (goe776-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 776 AIRFOIL (goe776-il)
Reynolds number: 200,000
Max Cl/Cd: 35.06 at α=10°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe776-il-200000-n5.txt
Download as CSV file: xf-goe776-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -1.0546   0.09833   0.09157  -0.0463   1.0000   0.1122
 -19.000  -1.0590   0.09458   0.08773  -0.0477   1.0000   0.1144
 -18.750  -1.0635   0.09080   0.08382  -0.0490   1.0000   0.1167
 -18.500  -1.0617   0.08802   0.08104  -0.0498   1.0000   0.1186
 -18.250  -1.0612   0.08508   0.07809  -0.0507   1.0000   0.1206
 -18.000  -1.0630   0.08181   0.07476  -0.0517   1.0000   0.1229
 -17.750  -1.0640   0.07865   0.07150  -0.0525   1.0000   0.1253
 -17.500  -1.0637   0.07571   0.06850  -0.0533   1.0000   0.1275
 -17.250  -1.0620   0.07306   0.06587  -0.0538   1.0000   0.1296
 -17.000  -1.0617   0.07021   0.06298  -0.0544   1.0000   0.1320
 -16.750  -1.0607   0.06745   0.06014  -0.0550   1.0000   0.1345
 -16.500  -1.0587   0.06484   0.05742  -0.0554   1.0000   0.1371
 -16.250  -1.0566   0.06238   0.05499  -0.0557   1.0000   0.1393
 -16.000  -1.0546   0.05991   0.05250  -0.0559   1.0000   0.1418
 -15.750  -1.0523   0.05749   0.05003  -0.0561   1.0000   0.1446
 -15.500  -1.0480   0.05531   0.04776  -0.0562   1.0000   0.1475
 -15.250  -1.0451   0.05311   0.04556  -0.0561   1.0000   0.1499
 -15.000  -1.0422   0.05094   0.04339  -0.0560   1.0000   0.1527
 -14.750  -1.0383   0.04891   0.04131  -0.0558   1.0000   0.1558
 -14.500  -1.0327   0.04708   0.03940  -0.0555   1.0000   0.1590
 -14.250  -1.0288   0.04521   0.03754  -0.0550   1.0000   0.1618
 -14.000  -1.0257   0.04335   0.03569  -0.0544   1.0000   0.1649
 -13.750  -1.0208   0.04171   0.03401  -0.0536   1.0000   0.1684
 -13.500  -1.0144   0.04026   0.03248  -0.0528   1.0000   0.1719
 -13.250  -1.0121   0.03867   0.03092  -0.0516   1.0000   0.1750
 -13.000  -1.0093   0.03723   0.02949  -0.0501   1.0000   0.1785
 -12.750  -1.0056   0.03597   0.02820  -0.0485   1.0000   0.1823
 -12.500  -1.0018   0.03487   0.02706  -0.0467   1.0000   0.1859
 -12.250  -1.0025   0.03367   0.02590  -0.0443   1.0000   0.1892
 -12.000  -1.0030   0.03263   0.02486  -0.0416   1.0000   0.1929
 -11.750  -1.0026   0.03178   0.02398  -0.0388   1.0000   0.1967
 -11.500  -1.0040   0.03099   0.02317  -0.0356   1.0000   0.2000
 -11.250  -1.0024   0.03003   0.02224  -0.0331   0.9989   0.2038
 -11.000  -0.9783   0.02896   0.02115  -0.0346   0.9946   0.2093
 -10.750  -0.9520   0.02803   0.02018  -0.0362   0.9910   0.2147
 -10.500  -0.9303   0.02699   0.01918  -0.0370   0.9853   0.2199
 -10.250  -0.9043   0.02613   0.01830  -0.0383   0.9802   0.2259
 -10.000  -0.8761   0.02530   0.01745  -0.0399   0.9763   0.2316
  -9.750  -0.8546   0.02448   0.01666  -0.0402   0.9688   0.2373
  -9.500  -0.8275   0.02380   0.01594  -0.0413   0.9626   0.2435
  -9.250  -0.8033   0.02307   0.01523  -0.0418   0.9560   0.2492
  -9.000  -0.7819   0.02242   0.01459  -0.0416   0.9466   0.2554
  -8.500  -0.7371   0.02126   0.01343  -0.0412   0.9282   0.2673
  -8.250  -0.7125   0.02070   0.01285  -0.0413   0.9200   0.2739
  -8.000  -0.6938   0.02028   0.01239  -0.0401   0.9073   0.2799
  -7.750  -0.6738   0.01976   0.01189  -0.0391   0.8968   0.2860
  -7.500  -0.6551   0.01935   0.01146  -0.0377   0.8839   0.2925
  -7.250  -0.6348   0.01896   0.01103  -0.0366   0.8722   0.2986
  -7.000  -0.6168   0.01856   0.01064  -0.0350   0.8593   0.3049
  -6.750  -0.5976   0.01824   0.01027  -0.0336   0.8465   0.3118
  -6.500  -0.5777   0.01790   0.00990  -0.0322   0.8342   0.3182
  -6.250  -0.5601   0.01760   0.00960  -0.0305   0.8208   0.3250
  -6.000  -0.5395   0.01735   0.00927  -0.0291   0.8088   0.3322
  -5.750  -0.5221   0.01712   0.00904  -0.0273   0.7953   0.3386
  -5.500  -0.5038   0.01691   0.00879  -0.0255   0.7832   0.3457
  -5.250  -0.4843   0.01676   0.00858  -0.0239   0.7700   0.3528
  -5.000  -0.4646   0.01655   0.00837  -0.0223   0.7582   0.3594
  -4.750  -0.4443   0.01639   0.00818  -0.0209   0.7453   0.3667
  -4.250  -0.4014   0.01608   0.00781  -0.0185   0.7214   0.3809
  -4.000  -0.3794   0.01596   0.00764  -0.0173   0.7101   0.3886
  -3.750  -0.3570   0.01585   0.00749  -0.0162   0.6979   0.3959
  -3.500  -0.3352   0.01571   0.00735  -0.0150   0.6870   0.4034
  -3.250  -0.3128   0.01562   0.00722  -0.0139   0.6751   0.4113
  -3.000  -0.2898   0.01553   0.00708  -0.0129   0.6646   0.4189
  -2.750  -0.2677   0.01542   0.00700  -0.0118   0.6531   0.4268
  -2.500  -0.2443   0.01536   0.00687  -0.0109   0.6426   0.4352
  -2.250  -0.2217   0.01526   0.00680  -0.0098   0.6318   0.4430
  -2.000  -0.1989   0.01520   0.00671  -0.0088   0.6210   0.4517
  -1.750  -0.1754   0.01515   0.00664  -0.0079   0.6107   0.4602
  -1.500  -0.1528   0.01508   0.00659  -0.0068   0.6000   0.4689
  -1.250  -0.1293   0.01505   0.00653  -0.0058   0.5901   0.4783
  -1.000  -0.1063   0.01500   0.00650  -0.0048   0.5792   0.4870
  -0.750  -0.0832   0.01498   0.00645  -0.0038   0.5695   0.4969
  -0.500  -0.0598   0.01495   0.00643  -0.0029   0.5589   0.5061
  -0.250  -0.0369   0.01494   0.00641  -0.0018   0.5490   0.5160
   0.000  -0.0133   0.01493   0.00640  -0.0009   0.5388   0.5260
   0.250   0.0096   0.01492   0.00641   0.0001   0.5287   0.5357
   0.500   0.0331   0.01494   0.00641   0.0011   0.5191   0.5463
   0.750   0.0561   0.01494   0.00643   0.0021   0.5089   0.5559
   1.000   0.0793   0.01498   0.00644   0.0031   0.4999   0.5666
   1.250   0.1027   0.01499   0.00649   0.0040   0.4900   0.5764
   1.750   0.1490   0.01507   0.00657   0.0060   0.4719   0.5973
   2.000   0.1718   0.01512   0.00663   0.0070   0.4629   0.6078
   2.250   0.1950   0.01520   0.00669   0.0080   0.4546   0.6186
   2.500   0.2182   0.01524   0.00679   0.0090   0.4458   0.6290
   2.750   0.2405   0.01535   0.00684   0.0101   0.4378   0.6401
   3.000   0.2640   0.01539   0.00697   0.0110   0.4297   0.6504
   3.250   0.2864   0.01549   0.00706   0.0121   0.4215   0.6619
   3.500   0.3089   0.01560   0.00718   0.0132   0.4141   0.6725
   3.750   0.3317   0.01568   0.00732   0.0142   0.4061   0.6844
   4.000   0.3537   0.01581   0.00745   0.0153   0.3985   0.6954
   4.250   0.3758   0.01593   0.00760   0.0165   0.3913   0.7074
   4.500   0.3980   0.01605   0.00777   0.0176   0.3836   0.7188
   4.750   0.4189   0.01621   0.00793   0.0189   0.3764   0.7312
   5.000   0.4408   0.01635   0.00812   0.0201   0.3695   0.7429
   5.250   0.4619   0.01650   0.00833   0.0214   0.3621   0.7556
   5.500   0.4814   0.01671   0.00853   0.0229   0.3553   0.7676
   5.750   0.5013   0.01687   0.00875   0.0244   0.3484   0.7806
   6.000   0.5200   0.01706   0.00898   0.0261   0.3413   0.7928
   6.500   0.5576   0.01754   0.00953   0.0294   0.3279   0.8183
   6.750   0.5754   0.01781   0.00981   0.0312   0.3210   0.8322
   7.000   0.5947   0.01817   0.01019   0.0326   0.3147   0.8441
   7.250   0.6142   0.01846   0.01053   0.0340   0.3079   0.8573
   7.500   0.6334   0.01886   0.01094   0.0354   0.3011   0.8697
   7.750   0.6519   0.01926   0.01135   0.0369   0.2952   0.8821
   8.000   0.6724   0.01966   0.01179   0.0379   0.2886   0.8943
   8.250   0.6918   0.02013   0.01226   0.0390   0.2823   0.9055
   8.500   0.7110   0.02061   0.01274   0.0401   0.2766   0.9176
   8.750   0.7346   0.02112   0.01329   0.0403   0.2699   0.9267
   9.000   0.7533   0.02169   0.01383   0.0412   0.2640   0.9380
   9.250   0.7787   0.02228   0.01444   0.0409   0.2580   0.9455
   9.500   0.8022   0.02289   0.01507   0.0407   0.2517   0.9543
   9.750   0.8242   0.02363   0.01576   0.0406   0.2459   0.9620
  10.000   0.8520   0.02430   0.01647   0.0394   0.2398   0.9678
  10.250   0.8737   0.02506   0.01723   0.0392   0.2340   0.9759
  10.500   0.9010   0.02595   0.01809   0.0376   0.2283   0.9797
  10.750   0.9283   0.02675   0.01894   0.0361   0.2223   0.9846
  11.000   0.9507   0.02773   0.01990   0.0353   0.2168   0.9905
  11.250   0.9760   0.02871   0.02089   0.0338   0.2116   0.9942
  11.500   1.0012   0.02972   0.02193   0.0323   0.2060   0.9984
  11.750   1.0063   0.03067   0.02287   0.0342   0.2018   1.0000
  12.000   1.0025   0.03152   0.02369   0.0377   0.1987   1.0000
  12.250   1.0037   0.03232   0.02454   0.0405   0.1949   1.0000
  12.500   1.0041   0.03331   0.02553   0.0431   0.1911   1.0000
  12.750   1.0042   0.03444   0.02665   0.0455   0.1876   1.0000
  13.000   1.0060   0.03564   0.02783   0.0475   0.1842   1.0000
  13.250   1.0107   0.03681   0.02906   0.0491   0.1804   1.0000
  13.500   1.0144   0.03818   0.03044   0.0505   0.1767   1.0000
  13.750   1.0169   0.03976   0.03199   0.0517   0.1735   1.0000
  14.000   1.0225   0.04125   0.03352   0.0526   0.1701   1.0000
  14.250   1.0282   0.04283   0.03515   0.0533   0.1665   1.0000
  14.500   1.0321   0.04462   0.03696   0.0539   0.1633   1.0000
  14.750   1.0352   0.04653   0.03884   0.0545   0.1604   1.0000
  15.000   1.0409   0.04835   0.04072   0.0548   0.1573   1.0000
  15.250   1.0457   0.05030   0.04273   0.0550   0.1541   1.0000
  15.500   1.0488   0.05245   0.04490   0.0551   0.1512   1.0000
  15.750   1.0513   0.05467   0.04710   0.0552   0.1487   1.0000
  16.000   1.0557   0.05683   0.04934   0.0551   0.1459   1.0000
  16.250   1.0587   0.05919   0.05176   0.0549   0.1430   1.0000
  16.500   1.0609   0.06164   0.05424   0.0547   0.1404   1.0000
  16.750   1.0627   0.06416   0.05675   0.0544   0.1381   1.0000
  17.000   1.0652   0.06667   0.05933   0.0540   0.1356   1.0000
  17.250   1.0663   0.06943   0.06218   0.0535   0.1330   1.0000
  17.500   1.0668   0.07226   0.06505   0.0529   0.1305   1.0000
  17.750   1.0677   0.07504   0.06783   0.0523   0.1283   1.0000
  18.000   1.0692   0.07778   0.07059   0.0516   0.1262   1.0000
  18.250   1.0680   0.08098   0.07391   0.0507   0.1238   1.0000
  18.500   1.0664   0.08423   0.07723   0.0498   0.1214   1.0000
  18.750   1.0662   0.08729   0.08031   0.0489   0.1193   1.0000
  19.000   1.0693   0.08986   0.08284   0.0481   0.1174   1.0000
  19.250   1.0647   0.09366   0.08678   0.0468   0.1151   1.0000
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