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GOE 477 AIRFOIL (goe477-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 477 AIRFOIL (goe477-il)
Reynolds number: 1,000,000
Max Cl/Cd: 104.88 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe477-il-1000000-n5.txt
Download as CSV file: xf-goe477-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 477 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.3542   0.07701   0.07439  -0.0876   0.8150   0.0063
 -11.500  -0.3650   0.07203   0.06937  -0.0902   0.8124   0.0063
 -11.250  -0.6192   0.02712   0.02367  -0.1155   0.8030   0.0053
 -11.000  -0.6095   0.02375   0.02001  -0.1155   0.8011   0.0054
 -10.750  -0.5933   0.02176   0.01782  -0.1152   0.7993   0.0055
 -10.500  -0.5740   0.02035   0.01624  -0.1148   0.7978   0.0057
 -10.250  -0.5533   0.01913   0.01486  -0.1144   0.7964   0.0058
 -10.000  -0.5312   0.01816   0.01375  -0.1140   0.7950   0.0060
  -9.750  -0.5084   0.01725   0.01268  -0.1137   0.7938   0.0062
  -9.500  -0.4850   0.01642   0.01172  -0.1133   0.7926   0.0064
  -9.250  -0.4608   0.01570   0.01089  -0.1130   0.7913   0.0066
  -9.000  -0.4362   0.01505   0.01012  -0.1127   0.7900   0.0068
  -8.750  -0.4115   0.01440   0.00937  -0.1124   0.7885   0.0070
  -8.500  -0.3867   0.01373   0.00861  -0.1120   0.7869   0.0074
  -8.250  -0.3613   0.01321   0.00800  -0.1118   0.7851   0.0077
  -8.000  -0.3355   0.01274   0.00744  -0.1115   0.7833   0.0081
  -7.750  -0.3094   0.01232   0.00692  -0.1113   0.7817   0.0085
  -7.500  -0.2831   0.01194   0.00645  -0.1110   0.7802   0.0088
  -7.250  -0.2567   0.01152   0.00596  -0.1108   0.7788   0.0093
  -7.000  -0.2302   0.01111   0.00549  -0.1106   0.7776   0.0100
  -6.750  -0.2034   0.01077   0.00511  -0.1104   0.7763   0.0107
  -6.500  -0.1763   0.01048   0.00477  -0.1103   0.7750   0.0114
  -6.250  -0.1494   0.01016   0.00440  -0.1101   0.7735   0.0124
  -6.000  -0.1224   0.00985   0.00407  -0.1100   0.7719   0.0136
  -5.750  -0.0951   0.00961   0.00378  -0.1098   0.7703   0.0147
  -5.500  -0.0680   0.00933   0.00347  -0.1097   0.7683   0.0166
  -5.250  -0.0409   0.00910   0.00320  -0.1095   0.7659   0.0189
  -5.000  -0.0138   0.00886   0.00296  -0.1093   0.7633   0.0230
  -4.750   0.0136   0.00865   0.00278  -0.1092   0.7609   0.0287
  -4.500   0.0413   0.00849   0.00266  -0.1091   0.7583   0.0346
  -4.250   0.0691   0.00839   0.00259  -0.1091   0.7556   0.0412
  -4.000   0.0971   0.00832   0.00250  -0.1090   0.7529   0.0448
  -3.750   0.1250   0.00828   0.00242  -0.1089   0.7500   0.0470
  -3.500   0.1530   0.00822   0.00235  -0.1089   0.7455   0.0481
  -3.250   0.1809   0.00817   0.00228  -0.1088   0.7400   0.0486
  -3.000   0.2082   0.00806   0.00212  -0.1086   0.7344   0.0496
  -2.750   0.2356   0.00787   0.00192  -0.1085   0.7280   0.0521
  -2.500   0.2628   0.00776   0.00177  -0.1083   0.7206   0.0537
  -2.250   0.2903   0.00765   0.00164  -0.1081   0.7126   0.0544
  -2.000   0.3174   0.00756   0.00151  -0.1079   0.7030   0.0550
  -1.750   0.3445   0.00749   0.00139  -0.1076   0.6913   0.0557
  -1.500   0.3714   0.00745   0.00130  -0.1074   0.6781   0.0566
  -1.250   0.3976   0.00745   0.00122  -0.1070   0.6610   0.0579
  -1.000   0.4233   0.00748   0.00117  -0.1065   0.6402   0.0592
  -0.750   0.4485   0.00757   0.00114  -0.1059   0.6153   0.0604
  -0.500   0.4732   0.00771   0.00115  -0.1053   0.5868   0.0615
  -0.250   0.4969   0.00788   0.00119  -0.1044   0.5499   0.0665
   0.000   0.5179   0.00824   0.00130  -0.1031   0.4861   0.0710
   0.500   0.5643   0.00867   0.00150  -0.1015   0.4169   0.0984
   0.750   0.5890   0.00873   0.00158  -0.1009   0.3998   0.1331
   1.000   0.6141   0.00878   0.00166  -0.1005   0.3854   0.1663
   1.250   0.6393   0.00885   0.00174  -0.1000   0.3721   0.1933
   1.500   0.6644   0.00893   0.00183  -0.0995   0.3589   0.2206
   1.750   0.6890   0.00894   0.00193  -0.0990   0.3454   0.2787
   2.000   0.7124   0.00883   0.00206  -0.0983   0.3311   0.4015
   2.500   0.7899   0.00803   0.00248  -0.1039   0.2963   1.0000
   2.750   0.8132   0.00820   0.00259  -0.1030   0.2845   1.0000
   3.000   0.8365   0.00838   0.00271  -0.1022   0.2743   1.0000
   3.250   0.8597   0.00857   0.00284  -0.1013   0.2647   1.0000
   3.500   0.8833   0.00874   0.00297  -0.1005   0.2565   1.0000
   3.750   0.9067   0.00892   0.00311  -0.0997   0.2495   1.0000
   4.000   0.9305   0.00909   0.00325  -0.0989   0.2432   1.0000
   4.250   0.9537   0.00928   0.00340  -0.0981   0.2373   1.0000
   4.500   0.9777   0.00943   0.00355  -0.0974   0.2332   1.0000
   4.750   1.0014   0.00960   0.00371  -0.0967   0.2289   1.0000
   5.000   1.0247   0.00979   0.00388  -0.0959   0.2247   1.0000
   5.250   1.0477   0.00999   0.00406  -0.0950   0.2186   1.0000
   5.500   1.0701   0.01022   0.00426  -0.0941   0.2111   1.0000
   5.750   1.0924   0.01044   0.00446  -0.0932   0.2036   1.0000
   6.000   1.1144   0.01068   0.00467  -0.0922   0.1962   1.0000
   6.250   1.1363   0.01091   0.00489  -0.0912   0.1897   1.0000
   6.500   1.1579   0.01116   0.00511  -0.0902   0.1811   1.0000
   6.750   1.1783   0.01145   0.00536  -0.0890   0.1702   1.0000
   7.000   1.1970   0.01183   0.00566  -0.0875   0.1551   1.0000
   7.250   1.1998   0.01287   0.00635  -0.0832   0.0988   1.0000
   7.500   1.1964   0.01433   0.00747  -0.0780   0.0319   1.0000
   7.750   1.2127   0.01479   0.00790  -0.0761   0.0232   1.0000
   8.000   1.2295   0.01523   0.00834  -0.0745   0.0192   1.0000
   8.250   1.2466   0.01568   0.00879  -0.0728   0.0163   1.0000
   8.500   1.2635   0.01613   0.00925  -0.0713   0.0140   1.0000
   8.750   1.2803   0.01661   0.00973  -0.0698   0.0126   1.0000
   9.000   1.2970   0.01710   0.01025  -0.0682   0.0112   1.0000
   9.250   1.3134   0.01762   0.01079  -0.0668   0.0101   1.0000
   9.500   1.3290   0.01820   0.01139  -0.0652   0.0093   1.0000
   9.750   1.3452   0.01875   0.01198  -0.0638   0.0086   1.0000
  10.000   1.3607   0.01936   0.01262  -0.0623   0.0080   1.0000
  10.250   1.3753   0.02003   0.01333  -0.0609   0.0074   1.0000
  10.500   1.3894   0.02076   0.01409  -0.0593   0.0070   1.0000
  10.750   1.4039   0.02146   0.01485  -0.0579   0.0066   1.0000
  11.000   1.4174   0.02225   0.01568  -0.0565   0.0063   1.0000
  11.250   1.4303   0.02309   0.01656  -0.0550   0.0059   1.0000
  11.500   1.4422   0.02402   0.01753  -0.0536   0.0056   1.0000
  11.750   1.4531   0.02503   0.01860  -0.0520   0.0053   1.0000
  12.000   1.4648   0.02600   0.01965  -0.0506   0.0050   1.0000
  12.250   1.4744   0.02715   0.02086  -0.0491   0.0049   1.0000
  12.500   1.4853   0.02820   0.02196  -0.0478   0.0046   1.0000
  12.750   1.4939   0.02946   0.02328  -0.0463   0.0044   1.0000
  13.000   1.5014   0.03082   0.02471  -0.0449   0.0043   1.0000
  13.250   1.5081   0.03226   0.02622  -0.0434   0.0042   1.0000
  13.500   1.5130   0.03390   0.02792  -0.0420   0.0040   1.0000
  13.750   1.5148   0.03585   0.02995  -0.0404   0.0039   1.0000
  14.000   1.5182   0.03770   0.03189  -0.0392   0.0039   1.0000
  14.250   1.5213   0.03967   0.03395  -0.0380   0.0038   1.0000
  14.500   1.5215   0.04200   0.03638  -0.0369   0.0037   1.0000
  14.750   1.5242   0.04417   0.03863  -0.0361   0.0036   1.0000
  15.000   1.5245   0.04669   0.04124  -0.0353   0.0035   1.0000
  15.250   1.5204   0.04984   0.04453  -0.0347   0.0035   1.0000
  15.500   1.5202   0.05268   0.04745  -0.0345   0.0033   1.0000
  15.750   1.5166   0.05604   0.05092  -0.0344   0.0033   1.0000
  16.000   1.5121   0.05966   0.05464  -0.0345   0.0033   1.0000
  16.250   1.5051   0.06379   0.05888  -0.0350   0.0032   1.0000
  16.500   1.4974   0.06819   0.06339  -0.0357   0.0032   1.0000
  16.750   1.4893   0.07278   0.06810  -0.0368   0.0031   1.0000
  17.000   1.4807   0.07765   0.07307  -0.0381   0.0031   1.0000
  17.250   1.4664   0.08362   0.07918  -0.0399   0.0031   1.0000
  17.500   1.4557   0.08914   0.08480  -0.0418   0.0030   1.0000
  17.750   1.4425   0.09510   0.09088  -0.0440   0.0030   1.0000
  18.000   1.4294   0.10115   0.09704  -0.0462   0.0030   1.0000
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