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GOE 477 AIRFOIL (goe477-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 477 AIRFOIL (goe477-il)
Reynolds number: 1,000,000
Max Cl/Cd: 121.69 at α=1.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe477-il-1000000.txt
Download as CSV file: xf-goe477-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.2306   0.10760   0.10560  -0.0726   0.9093   0.0156
 -11.500  -0.6604   0.02915   0.02619  -0.1109   0.8481   0.0115
 -11.250  -0.6523   0.02631   0.02310  -0.1106   0.8451   0.0117
 -11.000  -0.6394   0.02425   0.02081  -0.1100   0.8423   0.0119
 -10.750  -0.6219   0.02284   0.01921  -0.1095   0.8396   0.0122
 -10.500  -0.6023   0.02171   0.01789  -0.1090   0.8371   0.0124
 -10.250  -0.5912   0.01922   0.01505  -0.1078   0.8345   0.0128
 -10.000  -0.5710   0.01808   0.01379  -0.1072   0.8329   0.0133
  -9.750  -0.5484   0.01728   0.01289  -0.1067   0.8312   0.0136
  -9.500  -0.5248   0.01661   0.01212  -0.1063   0.8293   0.0141
  -9.250  -0.5009   0.01593   0.01132  -0.1059   0.8275   0.0145
  -9.000  -0.4766   0.01530   0.01057  -0.1054   0.8257   0.0150
  -8.750  -0.4517   0.01477   0.00991  -0.1051   0.8239   0.0154
  -8.500  -0.4282   0.01396   0.00895  -0.1045   0.8219   0.0160
  -8.250  -0.4043   0.01325   0.00813  -0.1040   0.8196   0.0168
  -8.000  -0.3784   0.01284   0.00767  -0.1037   0.8180   0.0176
  -7.750  -0.3521   0.01249   0.00726  -0.1035   0.8164   0.0184
  -7.500  -0.3255   0.01217   0.00687  -0.1032   0.8147   0.0192
  -7.250  -0.3004   0.01155   0.00616  -0.1028   0.8129   0.0204
  -7.000  -0.2740   0.01118   0.00576  -0.1025   0.8112   0.0216
  -6.750  -0.2470   0.01093   0.00545  -0.1023   0.8096   0.0229
  -6.500  -0.2199   0.01070   0.00516  -0.1021   0.8081   0.0239
  -6.250  -0.1936   0.01031   0.00475  -0.1018   0.8064   0.0263
  -6.000  -0.1660   0.01021   0.00461  -0.1017   0.8045   0.0282
  -5.750  -0.1389   0.00995   0.00433  -0.1015   0.8030   0.0304
  -5.500  -0.1112   0.00982   0.00423  -0.1014   0.8010   0.0330
  -5.250  -0.0834   0.00974   0.00414  -0.1013   0.7984   0.0351
  -5.000  -0.0562   0.00953   0.00391  -0.1011   0.7956   0.0378
  -4.750  -0.0280   0.00952   0.00391  -0.1010   0.7931   0.0402
  -4.500   0.0002   0.00952   0.00389  -0.1009   0.7907   0.0423
  -4.250   0.0287   0.00960   0.00394  -0.1010   0.7885   0.0434
  -4.000   0.0549   0.00917   0.00351  -0.1006   0.7862   0.0468
  -3.750   0.0826   0.00906   0.00341  -0.1005   0.7829   0.0488
  -3.500   0.1103   0.00895   0.00327  -0.1003   0.7789   0.0509
  -3.250   0.1382   0.00891   0.00318  -0.1001   0.7750   0.0524
  -3.000   0.1657   0.00880   0.00306  -0.0999   0.7710   0.0534
  -2.750   0.1916   0.00835   0.00259  -0.0995   0.7665   0.0567
  -2.500   0.2189   0.00817   0.00241  -0.0993   0.7624   0.0588
  -2.250   0.2466   0.00807   0.00227  -0.0991   0.7589   0.0608
  -2.000   0.2741   0.00793   0.00214  -0.0989   0.7554   0.0626
  -1.750   0.3017   0.00781   0.00202  -0.0988   0.7515   0.0640
  -1.500   0.3294   0.00770   0.00189  -0.0986   0.7475   0.0648
  -1.250   0.3565   0.00752   0.00166  -0.0983   0.7429   0.0680
  -1.000   0.3838   0.00736   0.00154  -0.0981   0.7370   0.0720
  -0.750   0.4112   0.00725   0.00143  -0.0979   0.7309   0.0755
  -0.500   0.4388   0.00716   0.00134  -0.0977   0.7251   0.0797
  -0.250   0.4658   0.00700   0.00126  -0.0975   0.7179   0.0994
   0.000   0.4921   0.00676   0.00123  -0.0972   0.7099   0.1725
   0.250   0.5183   0.00661   0.00119  -0.0968   0.6993   0.2263
   0.500   0.5437   0.00640   0.00117  -0.0963   0.6848   0.3110
   0.750   0.5665   0.00604   0.00119  -0.0954   0.6639   0.4771
   1.000   0.5769   0.00513   0.00130  -0.0917   0.6419   0.8703
   1.250   0.6425   0.00528   0.00141  -0.1000   0.6004   0.9845
   1.500   0.6883   0.00566   0.00153  -0.1041   0.5462   0.9994
   1.750   0.7074   0.00618   0.00172  -0.1025   0.4760   1.0000
   2.000   0.7261   0.00658   0.00189  -0.1007   0.4335   1.0000
   2.250   0.7473   0.00685   0.00203  -0.0994   0.4092   1.0000
   2.500   0.7693   0.00708   0.00215  -0.0982   0.3895   1.0000
   2.750   0.7916   0.00730   0.00228  -0.0971   0.3715   1.0000
   3.000   0.8141   0.00752   0.00241  -0.0960   0.3545   1.0000
   3.250   0.8367   0.00773   0.00253  -0.0950   0.3385   1.0000
   3.500   0.8593   0.00794   0.00267  -0.0939   0.3225   1.0000
   3.750   0.8818   0.00816   0.00281  -0.0929   0.3069   1.0000
   4.000   0.9041   0.00839   0.00296  -0.0918   0.2923   1.0000
   4.500   0.9490   0.00884   0.00329  -0.0898   0.2669   1.0000
   4.750   0.9713   0.00907   0.00347  -0.0887   0.2551   1.0000
   5.000   0.9938   0.00930   0.00365  -0.0877   0.2463   1.0000
   5.250   1.0166   0.00951   0.00383  -0.0868   0.2388   1.0000
   5.500   1.0392   0.00974   0.00402  -0.0859   0.2311   1.0000
   5.750   1.0621   0.00993   0.00421  -0.0850   0.2252   1.0000
   6.000   1.0841   0.01019   0.00443  -0.0840   0.2186   1.0000
   6.250   1.1075   0.01036   0.00460  -0.0832   0.2129   1.0000
   6.500   1.1289   0.01063   0.00483  -0.0821   0.2053   1.0000
   6.750   1.1519   0.01081   0.00502  -0.0812   0.1990   1.0000
   7.000   1.1727   0.01111   0.00528  -0.0801   0.1900   1.0000
   7.250   1.1943   0.01135   0.00549  -0.0790   0.1796   1.0000
   7.500   1.2129   0.01175   0.00579  -0.0775   0.1604   1.0000
   7.750   1.2047   0.01353   0.00696  -0.0715   0.0618   1.0000
   8.000   1.2124   0.01442   0.00770  -0.0681   0.0341   1.0000
   8.250   1.2273   0.01495   0.00822  -0.0659   0.0282   1.0000
   8.500   1.2440   0.01539   0.00867  -0.0642   0.0256   1.0000
   8.750   1.2583   0.01600   0.00929  -0.0621   0.0227   1.0000
   9.000   1.2754   0.01643   0.00977  -0.0605   0.0216   1.0000
   9.250   1.2920   0.01691   0.01028  -0.0589   0.0205   1.0000
   9.500   1.3074   0.01747   0.01087  -0.0571   0.0190   1.0000
   9.750   1.3188   0.01832   0.01177  -0.0549   0.0175   1.0000
  10.000   1.3349   0.01885   0.01234  -0.0534   0.0169   1.0000
  10.250   1.3501   0.01945   0.01298  -0.0519   0.0162   1.0000
  10.500   1.3644   0.02013   0.01370  -0.0503   0.0156   1.0000
  10.750   1.3781   0.02085   0.01447  -0.0487   0.0149   1.0000
  11.000   1.3882   0.02184   0.01550  -0.0468   0.0141   1.0000
  11.250   1.3925   0.02326   0.01701  -0.0443   0.0135   1.0000
  11.500   1.4081   0.02391   0.01771  -0.0432   0.0131   1.0000
  11.750   1.4201   0.02483   0.01868  -0.0418   0.0126   1.0000
  12.000   1.4307   0.02587   0.01978  -0.0403   0.0122   1.0000
  12.250   1.4397   0.02705   0.02103  -0.0387   0.0119   1.0000
  12.500   1.4493   0.02821   0.02223  -0.0373   0.0114   1.0000
  12.750   1.4554   0.02965   0.02373  -0.0357   0.0112   1.0000
  13.000   1.4575   0.03145   0.02560  -0.0339   0.0108   1.0000
  13.250   1.4479   0.03429   0.02857  -0.0315   0.0104   1.0000
  13.500   1.4490   0.03632   0.03069  -0.0301   0.0103   1.0000
  13.750   1.4558   0.03792   0.03236  -0.0291   0.0101   1.0000
  14.000   1.4613   0.03968   0.03421  -0.0281   0.0099   1.0000
  14.250   1.4620   0.04198   0.03660  -0.0271   0.0097   1.0000
  14.500   1.4610   0.04458   0.03929  -0.0262   0.0095   1.0000
  14.750   1.4595   0.04735   0.04216  -0.0256   0.0094   1.0000
  15.000   1.4568   0.05039   0.04530  -0.0253   0.0093   1.0000
  15.250   1.4570   0.05326   0.04824  -0.0251   0.0090   1.0000
  15.500   1.4610   0.05576   0.05080  -0.0253   0.0087   1.0000
  15.750   1.4548   0.05964   0.05478  -0.0256   0.0086   1.0000
  16.000   1.4491   0.06360   0.05885  -0.0261   0.0086   1.0000
  16.250   1.4443   0.06763   0.06296  -0.0270   0.0084   1.0000
  16.500   1.4332   0.07270   0.06813  -0.0282   0.0082   1.0000
  16.750   1.4236   0.07765   0.07319  -0.0296   0.0081   1.0000
  17.000   1.4132   0.08287   0.07851  -0.0312   0.0081   1.0000
  17.250   1.3946   0.08928   0.08504  -0.0331   0.0079   1.0000
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