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GOE 624 AIRFOIL (goe624-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 624 AIRFOIL (goe624-il)
Reynolds number: 100,000
Max Cl/Cd: 50.23 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe624-il-100000-n5.txt
Download as CSV file: xf-goe624-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 624 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.2077   0.09517   0.08999  -0.0713   0.9561   0.0543
  -9.750  -0.2078   0.08943   0.08425  -0.0757   0.9452   0.0536
  -9.500  -0.2134   0.08269   0.07748  -0.0810   0.9343   0.0530
  -9.250  -0.2804   0.06238   0.05707  -0.0995   0.9145   0.0519
  -9.000  -0.3273   0.05130   0.04547  -0.1063   0.8978   0.0519
  -8.750  -0.3284   0.04707   0.04094  -0.1074   0.8887   0.0524
  -8.500  -0.3182   0.04505   0.03877  -0.1072   0.8786   0.0530
  -8.250  -0.3078   0.04216   0.03557  -0.1073   0.8710   0.0536
  -8.000  -0.2991   0.03926   0.03232  -0.1068   0.8614   0.0542
  -7.750  -0.2851   0.03655   0.02922  -0.1065   0.8541   0.0549
  -7.500  -0.2695   0.03423   0.02651  -0.1058   0.8463   0.0557
  -7.250  -0.2515   0.03210   0.02397  -0.1052   0.8383   0.0568
  -7.000  -0.2302   0.03000   0.02134  -0.1047   0.8325   0.0584
  -6.750  -0.2080   0.02937   0.02071  -0.1040   0.8232   0.0596
  -6.500  -0.1832   0.02848   0.01968  -0.1036   0.8160   0.0612
  -6.250  -0.1604   0.02745   0.01843  -0.1029   0.8066   0.0631
  -6.000  -0.1357   0.02620   0.01687  -0.1022   0.7986   0.0650
  -5.750  -0.1112   0.02540   0.01599  -0.1017   0.7901   0.0667
  -5.500  -0.0860   0.02475   0.01526  -0.1012   0.7821   0.0689
  -5.250  -0.0596   0.02400   0.01432  -0.1007   0.7757   0.0726
  -5.000  -0.0349   0.02348   0.01378  -0.1003   0.7670   0.0761
  -4.750  -0.0081   0.02289   0.01307  -0.0999   0.7607   0.0808
  -4.500   0.0172   0.02236   0.01250  -0.0995   0.7528   0.0856
  -4.250   0.0435   0.02187   0.01192  -0.0991   0.7455   0.0922
  -4.000   0.0701   0.02142   0.01145  -0.0988   0.7391   0.0994
  -3.750   0.0957   0.02107   0.01103  -0.0983   0.7308   0.1077
  -3.500   0.1230   0.02070   0.01061  -0.0981   0.7245   0.1166
  -3.250   0.1485   0.02042   0.01035  -0.0977   0.7164   0.1260
  -3.000   0.1753   0.02014   0.01005  -0.0975   0.7093   0.1378
  -2.750   0.2023   0.01993   0.00977  -0.0972   0.7024   0.1505
  -2.500   0.2282   0.01965   0.00955  -0.0968   0.6942   0.1615
  -2.250   0.2558   0.01930   0.00917  -0.0966   0.6882   0.1729
  -2.000   0.2812   0.01912   0.00902  -0.0961   0.6793   0.1868
  -1.750   0.3084   0.01883   0.00875  -0.0958   0.6726   0.2053
  -1.500   0.3344   0.01861   0.00861  -0.0955   0.6650   0.2310
  -1.250   0.3608   0.01835   0.00846  -0.0952   0.6572   0.2700
  -1.000   0.3875   0.01804   0.00831  -0.0949   0.6503   0.3265
  -0.750   0.4125   0.01774   0.00829  -0.0945   0.6417   0.4094
  -0.500   0.4371   0.01722   0.00820  -0.0936   0.6354   0.5449
  -0.250   0.4566   0.01681   0.00841  -0.0913   0.6271   0.7234
   0.000   0.4969   0.01660   0.00843  -0.0924   0.6197   0.9026
   0.250   0.5506   0.01666   0.00838  -0.0974   0.6109   0.9874
   0.500   0.5832   0.01677   0.00831  -0.0985   0.6028   1.0000
   0.750   0.6070   0.01691   0.00829  -0.0977   0.5956   1.0000
   1.000   0.6301   0.01710   0.00837  -0.0969   0.5875   1.0000
   1.250   0.6556   0.01722   0.00831  -0.0964   0.5814   1.0000
   1.500   0.6782   0.01746   0.00849  -0.0956   0.5728   1.0000
   1.750   0.7032   0.01762   0.00852  -0.0950   0.5659   1.0000
   2.000   0.7274   0.01785   0.00865  -0.0944   0.5587   1.0000
   2.250   0.7516   0.01807   0.00880  -0.0938   0.5515   1.0000
   2.500   0.7781   0.01824   0.00882  -0.0935   0.5461   1.0000
   2.750   0.8009   0.01855   0.00911  -0.0928   0.5383   1.0000
   3.000   0.8260   0.01877   0.00924  -0.0924   0.5320   1.0000
   3.250   0.8513   0.01902   0.00941  -0.0920   0.5262   1.0000
   3.500   0.8748   0.01933   0.00970  -0.0914   0.5195   1.0000
   3.750   0.9005   0.01956   0.00985  -0.0910   0.5140   1.0000
   4.000   0.9249   0.01987   0.01011  -0.0906   0.5082   1.0000
   4.250   0.9485   0.02020   0.01044  -0.0900   0.5020   1.0000
   4.500   0.9742   0.02046   0.01062  -0.0897   0.4970   1.0000
   4.750   0.9983   0.02080   0.01094  -0.0892   0.4915   1.0000
   5.000   1.0212   0.02117   0.01132  -0.0886   0.4855   1.0000
   5.250   1.0465   0.02146   0.01156  -0.0883   0.4805   1.0000
   5.500   1.0707   0.02181   0.01189  -0.0878   0.4752   1.0000
   5.750   1.0923   0.02223   0.01235  -0.0870   0.4691   1.0000
   6.000   1.1169   0.02253   0.01260  -0.0866   0.4635   1.0000
   6.250   1.1393   0.02291   0.01298  -0.0859   0.4572   1.0000
   6.500   1.1596   0.02332   0.01342  -0.0849   0.4502   1.0000
   6.750   1.1849   0.02359   0.01361  -0.0846   0.4445   1.0000
   7.000   1.2031   0.02411   0.01421  -0.0833   0.4379   1.0000
   7.250   1.2238   0.02454   0.01467  -0.0824   0.4318   1.0000
   7.500   1.2490   0.02487   0.01493  -0.0821   0.4270   1.0000
   7.750   1.2654   0.02547   0.01565  -0.0807   0.4210   1.0000
   8.000   1.2841   0.02598   0.01623  -0.0796   0.4153   1.0000
   8.250   1.3075   0.02637   0.01659  -0.0791   0.4105   1.0000
   8.500   1.3238   0.02699   0.01729  -0.0777   0.4050   1.0000
   8.750   1.3383   0.02762   0.01803  -0.0760   0.3989   1.0000
   9.000   1.3588   0.02804   0.01845  -0.0751   0.3936   1.0000
   9.250   1.3709   0.02871   0.01920  -0.0731   0.3879   1.0000
   9.500   1.3797   0.02948   0.02008  -0.0707   0.3817   1.0000
   9.750   1.3974   0.02999   0.02061  -0.0695   0.3764   1.0000
  10.000   1.4072   0.03085   0.02157  -0.0675   0.3708   1.0000
  10.250   1.4141   0.03185   0.02270  -0.0652   0.3645   1.0000
  10.500   1.4305   0.03244   0.02329  -0.0641   0.3590   1.0000
  10.750   1.4340   0.03370   0.02471  -0.0618   0.3526   1.0000
  11.000   1.4402   0.03485   0.02595  -0.0598   0.3459   1.0000
  11.250   1.4537   0.03561   0.02672  -0.0586   0.3400   1.0000
  11.500   1.4499   0.03751   0.02881  -0.0562   0.3324   1.0000
  11.750   1.4613   0.03842   0.02972  -0.0549   0.3260   1.0000
  12.000   1.4571   0.04059   0.03205  -0.0529   0.3184   1.0000
  12.250   1.4628   0.04200   0.03350  -0.0516   0.3113   1.0000
  12.500   1.4600   0.04424   0.03586  -0.0500   0.3037   1.0000
  12.750   1.4621   0.04608   0.03774  -0.0488   0.2961   1.0000
  13.000   1.4586   0.04858   0.04035  -0.0476   0.2885   1.0000
  13.250   1.4592   0.05073   0.04256  -0.0465   0.2813   1.0000
  13.500   1.4573   0.05326   0.04516  -0.0456   0.2743   1.0000
  13.750   1.4542   0.05599   0.04796  -0.0448   0.2671   1.0000
  14.000   1.4575   0.05809   0.05009  -0.0442   0.2610   1.0000
  14.250   1.4495   0.06164   0.05378  -0.0437   0.2543   1.0000
  14.500   1.4600   0.06295   0.05507  -0.0431   0.2490   1.0000
  14.750   1.4490   0.06708   0.05936  -0.0429   0.2428   1.0000
  15.000   1.4479   0.06997   0.06232  -0.0427   0.2371   1.0000
  15.250   1.4553   0.07175   0.06411  -0.0423   0.2320   1.0000
  15.500   1.4405   0.07665   0.06917  -0.0426   0.2260   1.0000
  15.750   1.4464   0.07869   0.07124  -0.0423   0.2208   1.0000
  16.000   1.4431   0.08207   0.07472  -0.0425   0.2157   1.0000
  16.250   1.4308   0.08684   0.07964  -0.0431   0.2100   1.0000
  16.500   1.4423   0.08810   0.08088  -0.0428   0.2054   1.0000
  16.750   1.4296   0.09306   0.08599  -0.0436   0.2002   1.0000
  17.000   1.4187   0.09782   0.09087  -0.0446   0.1946   1.0000
  17.250   1.4370   0.09800   0.09102  -0.0441   0.1902   1.0000
  17.500   1.4095   0.10550   0.09873  -0.0461   0.1844   1.0000
  17.750   1.4042   0.10951   0.10283  -0.0471   0.1791   1.0000
  18.000   1.4293   0.10851   0.10175  -0.0462   0.1750   1.0000
  18.250   1.3849   0.11920   0.11274  -0.0500   0.1686   1.0000
  18.500   1.3909   0.12142   0.11499  -0.0506   0.1637   1.0000
  18.750   1.3899   0.12483   0.11846  -0.0517   0.1588   1.0000
  19.000   1.3573   0.13399   0.12779  -0.0555   0.1525   1.0000
  19.250   1.3829   0.13268   0.12642  -0.0547   0.1481   1.0000
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