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GOE 14K AIRFOIL (goe14k-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 14K AIRFOIL (goe14k-il)
Reynolds number: 500,000
Max Cl/Cd: 76.8 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe14k-il-500000-n5.txt
Download as CSV file: xf-goe14k-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 14K 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  -0.6106   0.09383   0.09120  -0.0825   0.9836   0.0071
 -14.250  -0.6734   0.07772   0.07497  -0.0909   0.9819   0.0069
 -14.000  -0.7592   0.05500   0.05192  -0.1070   0.9797   0.0065
 -13.750  -0.7892   0.04347   0.04000  -0.1192   0.9780   0.0064
 -13.500  -0.7974   0.04080   0.03723  -0.1183   0.9736   0.0066
 -13.250  -0.8083   0.03748   0.03369  -0.1178   0.9706   0.0065
 -13.000  -0.8012   0.03572   0.03179  -0.1175   0.9690   0.0069
 -12.750  -0.8158   0.03318   0.02902  -0.1134   0.9647   0.0067
 -12.500  -0.8134   0.03190   0.02758  -0.1106   0.9606   0.0070
 -12.250  -0.8080   0.03029   0.02578  -0.1086   0.9582   0.0071
 -12.000  -0.7999   0.02865   0.02394  -0.1068   0.9566   0.0072
 -11.750  -0.8043   0.02788   0.02301  -0.1012   0.9493   0.0076
 -11.500  -0.7948   0.02673   0.02169  -0.0988   0.9464   0.0077
 -11.250  -0.7835   0.02545   0.02023  -0.0967   0.9445   0.0079
 -11.000  -0.7888   0.02462   0.01930  -0.0907   0.9376   0.0080
 -10.750  -0.7775   0.02375   0.01832  -0.0881   0.9343   0.0082
 -10.500  -0.7609   0.02281   0.01727  -0.0867   0.9324   0.0086
 -10.250  -0.7410   0.02197   0.01632  -0.0858   0.9310   0.0089
 -10.000  -0.7299   0.02122   0.01544  -0.0828   0.9271   0.0091
  -9.750  -0.7192   0.02052   0.01461  -0.0796   0.9224   0.0096
  -9.500  -0.7008   0.01976   0.01371  -0.0782   0.9201   0.0098
  -9.250  -0.6799   0.01896   0.01280  -0.0772   0.9184   0.0105
  -9.000  -0.6570   0.01822   0.01197  -0.0767   0.9171   0.0108
  -8.750  -0.6317   0.01757   0.01124  -0.0766   0.9161   0.0114
  -8.500  -0.6176   0.01716   0.01074  -0.0739   0.9118   0.0121
  -8.250  -0.5986   0.01669   0.01017  -0.0723   0.9085   0.0128
  -8.000  -0.5764   0.01608   0.00949  -0.0715   0.9064   0.0138
  -7.750  -0.5511   0.01555   0.00889  -0.0713   0.9049   0.0147
  -7.500  -0.5236   0.01506   0.00832  -0.0716   0.9037   0.0159
  -7.250  -0.4951   0.01451   0.00772  -0.0721   0.9027   0.0179
  -7.000  -0.4652   0.01403   0.00718  -0.0729   0.9019   0.0199
  -6.750  -0.4343   0.01359   0.00668  -0.0739   0.9011   0.0227
  -6.500  -0.4236   0.01340   0.00651  -0.0703   0.8959   0.0264
  -6.250  -0.3996   0.01311   0.00623  -0.0697   0.8933   0.0317
  -6.000  -0.3718   0.01287   0.00598  -0.0699   0.8914   0.0380
  -5.750  -0.3416   0.01269   0.00574  -0.0707   0.8900   0.0419
  -5.500  -0.3104   0.01238   0.00542  -0.0718   0.8888   0.0465
  -5.250  -0.2778   0.01216   0.00516  -0.0731   0.8878   0.0508
  -5.000  -0.2441   0.01196   0.00490  -0.0747   0.8870   0.0540
  -4.750  -0.2097   0.01177   0.00466  -0.0764   0.8862   0.0559
  -4.500  -0.2045   0.01168   0.00456  -0.0715   0.8811   0.0584
  -4.250  -0.1809   0.01149   0.00436  -0.0707   0.8787   0.0623
  -4.000  -0.1536   0.01132   0.00416  -0.0708   0.8768   0.0655
  -3.750  -0.1242   0.01116   0.00395  -0.0714   0.8754   0.0674
  -3.500  -0.0928   0.01093   0.00371  -0.0724   0.8742   0.0706
  -3.250  -0.0601   0.01073   0.00351  -0.0738   0.8732   0.0749
  -3.000  -0.0259   0.01054   0.00331  -0.0755   0.8722   0.0809
  -2.750   0.0093   0.01025   0.00312  -0.0775   0.8713   0.1048
  -2.500   0.0147   0.01013   0.00317  -0.0726   0.8670   0.1465
  -2.250   0.0366   0.00995   0.00311  -0.0715   0.8647   0.1863
  -2.000   0.0631   0.00975   0.00305  -0.0715   0.8629   0.2233
  -1.750   0.0926   0.00952   0.00298  -0.0723   0.8615   0.2723
  -1.500   0.1227   0.00934   0.00293  -0.0731   0.8602   0.3105
  -1.250   0.1539   0.00908   0.00287  -0.0743   0.8590   0.3708
  -1.000   0.1864   0.00884   0.00281  -0.0756   0.8580   0.4249
  -0.750   0.2186   0.00848   0.00274  -0.0770   0.8569   0.5053
  -0.500   0.3150   0.00754   0.00314  -0.0935   0.8588   0.8532
  -0.250   0.4025   0.00799   0.00367  -0.1071   0.8593   0.8902
   0.000   0.4483   0.00817   0.00383  -0.1112   0.8574   0.9053
   0.250   0.4757   0.00838   0.00404  -0.1110   0.8547   0.9210
   0.750   0.5264   0.00893   0.00463  -0.1096   0.8469   0.9470
   1.000   0.5681   0.00897   0.00462  -0.1128   0.8414   0.9513
   1.500   0.6233   0.00916   0.00480  -0.1126   0.8248   0.9595
   1.750   0.6343   0.00933   0.00499  -0.1087   0.8156   0.9660
   2.000   0.6691   0.00935   0.00501  -0.1104   0.8063   0.9678
   2.250   0.6958   0.00939   0.00503  -0.1101   0.7907   0.9711
   2.500   0.7089   0.00957   0.00517  -0.1067   0.7708   0.9765
   2.750   0.7373   0.00960   0.00512  -0.1068   0.7367   0.9790
   3.000   0.7445   0.01003   0.00520  -0.1021   0.6561   0.9846
   3.250   0.7464   0.01071   0.00547  -0.0966   0.5740   0.9887
   3.500   0.7376   0.01186   0.00600  -0.0891   0.4455   0.9934
   3.750   0.7522   0.01240   0.00630  -0.0867   0.3935   0.9956
   4.000   0.7714   0.01274   0.00649  -0.0853   0.3535   0.9972
   4.250   0.7870   0.01330   0.00676  -0.0834   0.2857   0.9989
   4.500   0.8023   0.01385   0.00705  -0.0813   0.2289   1.0000
   4.750   0.8106   0.01435   0.00738  -0.0776   0.1889   1.0000
   5.000   0.8193   0.01491   0.00773  -0.0740   0.1473   1.0000
   5.250   0.8298   0.01542   0.00806  -0.0707   0.1100   1.0000
   5.500   0.8438   0.01576   0.00834  -0.0682   0.0959   1.0000
   5.750   0.8576   0.01613   0.00867  -0.0656   0.0829   1.0000
   6.000   0.8722   0.01648   0.00898  -0.0632   0.0732   1.0000
   6.250   0.8874   0.01683   0.00931  -0.0610   0.0662   1.0000
   6.500   0.9031   0.01715   0.00965  -0.0588   0.0610   1.0000
   6.750   0.9185   0.01749   0.00999  -0.0566   0.0553   1.0000
   7.000   0.9340   0.01784   0.01035  -0.0545   0.0484   1.0000
   7.250   0.9489   0.01825   0.01072  -0.0522   0.0375   1.0000
   7.500   0.9638   0.01868   0.01112  -0.0500   0.0300   1.0000
   7.750   0.9779   0.01917   0.01159  -0.0477   0.0246   1.0000
   8.000   0.9924   0.01964   0.01209  -0.0454   0.0208   1.0000
   8.250   1.0067   0.02015   0.01260  -0.0432   0.0186   1.0000
   8.500   1.0212   0.02067   0.01316  -0.0410   0.0167   1.0000
   8.750   1.0357   0.02119   0.01373  -0.0388   0.0153   1.0000
   9.000   1.0493   0.02179   0.01433  -0.0366   0.0134   1.0000
   9.250   1.0633   0.02235   0.01497  -0.0345   0.0134   1.0000
   9.500   1.0778   0.02289   0.01556  -0.0324   0.0125   1.0000
   9.750   1.0915   0.02350   0.01621  -0.0303   0.0114   1.0000
  10.000   1.1040   0.02421   0.01695  -0.0280   0.0106   1.0000
  10.250   1.1169   0.02487   0.01770  -0.0258   0.0104   1.0000
  10.500   1.1288   0.02564   0.01855  -0.0235   0.0100   1.0000
  10.750   1.1419   0.02631   0.01928  -0.0214   0.0093   1.0000
  11.000   1.1532   0.02711   0.02016  -0.0191   0.0092   1.0000
  11.250   1.1659   0.02781   0.02091  -0.0171   0.0087   1.0000
  11.500   1.1749   0.02881   0.02197  -0.0146   0.0084   1.0000
  11.750   1.1833   0.02985   0.02311  -0.0121   0.0081   1.0000
  12.000   1.1934   0.03077   0.02413  -0.0098   0.0079   1.0000
  12.250   1.2028   0.03176   0.02521  -0.0076   0.0075   1.0000
  12.500   1.2107   0.03287   0.02641  -0.0052   0.0072   1.0000
  12.750   1.2191   0.03394   0.02760  -0.0029   0.0070   1.0000
  13.000   1.2248   0.03524   0.02900  -0.0005   0.0069   1.0000
  13.250   1.2311   0.03649   0.03034   0.0018   0.0067   1.0000
  13.500   1.2358   0.03791   0.03188   0.0042   0.0068   1.0000
  13.750   1.2399   0.03938   0.03342   0.0065   0.0066   1.0000
  14.000   1.2403   0.04117   0.03529   0.0090   0.0063   1.0000
  14.250   1.2446   0.04271   0.03701   0.0110   0.0061   1.0000
  14.500   1.2410   0.04501   0.03943   0.0137   0.0062   1.0000
  14.750   1.2443   0.04674   0.04133   0.0155   0.0058   1.0000
  15.000   1.2468   0.04853   0.04325   0.0172   0.0056   1.0000
  15.250   1.2423   0.05107   0.04593   0.0192   0.0057   1.0000
  15.500   1.2369   0.05384   0.04886   0.0211   0.0057   1.0000
  15.750   1.2329   0.05655   0.05172   0.0224   0.0055   1.0000
  16.000   1.2307   0.05916   0.05443   0.0234   0.0052   1.0000
  16.250   1.2213   0.06277   0.05822   0.0243   0.0053   1.0000
  16.500   1.2117   0.06663   0.06222   0.0247   0.0052   1.0000
  16.750   1.1996   0.07107   0.06683   0.0247   0.0052   1.0000
  17.000   1.1738   0.07783   0.07384   0.0238   0.0054   1.0000
  17.250   1.1771   0.08054   0.07660   0.0230   0.0052   1.0000
  17.500   1.1570   0.08721   0.08347   0.0208   0.0052   1.0000
  17.750   1.1527   0.09161   0.08792   0.0188   0.0049   1.0000
  18.000   1.1187   0.10169   0.09829   0.0145   0.0052   1.0000
  18.250   1.0964   0.11007   0.10683   0.0104   0.0051   1.0000
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