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GOE 14K AIRFOIL (goe14k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 14K AIRFOIL (goe14k-il)
Reynolds number: 1,000,000
Max Cl/Cd: 86.07 at α=1.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe14k-il-1000000-n5.txt
Download as CSV file: xf-goe14k-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.6069   0.10688   0.10473  -0.0881   0.9833   0.0051
 -16.000  -0.6798   0.08976   0.08748  -0.0965   0.9823   0.0049
 -15.750  -0.8279   0.06021   0.05757  -0.1126   0.9809   0.0045
 -15.500  -0.8648   0.04685   0.04392  -0.1242   0.9800   0.0043
 -15.250  -0.8959   0.03805   0.03485  -0.1319   0.9788   0.0045
 -15.000  -0.9006   0.03485   0.03148  -0.1330   0.9781   0.0042
 -14.750  -0.9193   0.03260   0.02910  -0.1287   0.9742   0.0045
 -14.500  -0.9173   0.03109   0.02745  -0.1270   0.9720   0.0043
 -14.250  -0.9182   0.02917   0.02540  -0.1250   0.9704   0.0044
 -14.000  -0.9148   0.02746   0.02354  -0.1232   0.9691   0.0045
 -13.750  -0.9066   0.02599   0.02193  -0.1218   0.9683   0.0046
 -13.500  -0.9085   0.02534   0.02123  -0.1168   0.9638   0.0048
 -13.250  -0.9028   0.02435   0.02013  -0.1138   0.9607   0.0048
 -13.000  -0.8881   0.02350   0.01919  -0.1124   0.9590   0.0050
 -12.750  -0.8757   0.02237   0.01793  -0.1107   0.9576   0.0050
 -12.500  -0.8557   0.02167   0.01715  -0.1101   0.9567   0.0053
 -12.250  -0.8620   0.02120   0.01659  -0.1035   0.9494   0.0053
 -12.000  -0.8496   0.02037   0.01563  -0.1012   0.9468   0.0054
 -11.750  -0.8319   0.01970   0.01486  -0.0998   0.9452   0.0056
 -11.500  -0.8137   0.01901   0.01409  -0.0985   0.9439   0.0057
 -11.250  -0.8166   0.01866   0.01365  -0.0923   0.9359   0.0058
 -11.000  -0.8017   0.01794   0.01283  -0.0902   0.9332   0.0059
 -10.750  -0.7808   0.01723   0.01204  -0.0893   0.9316   0.0063
 -10.500  -0.7576   0.01651   0.01124  -0.0890   0.9303   0.0065
 -10.250  -0.7444   0.01616   0.01084  -0.0862   0.9248   0.0068
 -10.000  -0.7230   0.01561   0.01022  -0.0853   0.9216   0.0070
  -9.750  -0.6974   0.01506   0.00959  -0.0852   0.9196   0.0074
  -9.500  -0.6693   0.01456   0.00899  -0.0858   0.9179   0.0077
  -9.250  -0.6405   0.01398   0.00835  -0.0865   0.9164   0.0082
  -9.000  -0.6155   0.01352   0.00784  -0.0863   0.9136   0.0085
  -8.750  -0.5927   0.01315   0.00741  -0.0856   0.9098   0.0089
  -8.500  -0.5651   0.01275   0.00695  -0.0859   0.9070   0.0096
  -8.250  -0.5346   0.01237   0.00650  -0.0869   0.9049   0.0102
  -8.000  -0.5027   0.01192   0.00602  -0.0883   0.9030   0.0115
  -7.750  -0.4696   0.01155   0.00560  -0.0899   0.9013   0.0124
  -7.500  -0.4475   0.01131   0.00530  -0.0889   0.8973   0.0129
  -7.250  -0.4226   0.01097   0.00495  -0.0885   0.8936   0.0148
  -7.000  -0.3937   0.01070   0.00464  -0.0891   0.8908   0.0164
  -6.750  -0.3628   0.01039   0.00430  -0.0902   0.8884   0.0188
  -6.500  -0.3300   0.01008   0.00399  -0.0917   0.8865   0.0236
  -6.250  -0.3099   0.00988   0.00381  -0.0902   0.8826   0.0287
  -6.000  -0.2860   0.00970   0.00367  -0.0895   0.8790   0.0370
  -5.750  -0.2583   0.00955   0.00351  -0.0898   0.8761   0.0407
  -5.500  -0.2277   0.00942   0.00333  -0.0906   0.8737   0.0419
  -5.250  -0.1950   0.00923   0.00312  -0.0920   0.8717   0.0460
  -5.000  -0.1744   0.00912   0.00301  -0.0905   0.8687   0.0492
  -4.750  -0.1531   0.00902   0.00290  -0.0892   0.8656   0.0512
  -4.500  -0.1286   0.00893   0.00278  -0.0887   0.8630   0.0533
  -4.250  -0.1017   0.00886   0.00267  -0.0887   0.8607   0.0551
  -4.000  -0.0723   0.00873   0.00253  -0.0892   0.8587   0.0573
  -3.750  -0.0406   0.00858   0.00236  -0.0904   0.8571   0.0603
  -3.500  -0.0159   0.00848   0.00226  -0.0898   0.8550   0.0619
  -3.250   0.0029   0.00841   0.00219  -0.0879   0.8524   0.0636
  -3.000   0.0250   0.00834   0.00211  -0.0867   0.8500   0.0653
  -2.750   0.0496   0.00827   0.00203  -0.0862   0.8478   0.0673
  -2.500   0.0769   0.00815   0.00194  -0.0862   0.8458   0.0745
  -2.250   0.1070   0.00797   0.00184  -0.0870   0.8441   0.0958
  -2.000   0.1392   0.00771   0.00175  -0.0884   0.8428   0.1468
  -1.750   0.1718   0.00750   0.00168  -0.0899   0.8415   0.1911
  -1.500   0.1889   0.00739   0.00167  -0.0876   0.8386   0.2188
  -1.250   0.2064   0.00725   0.00166  -0.0854   0.8352   0.2567
  -1.000   0.2294   0.00713   0.00164  -0.0844   0.8321   0.2909
  -0.750   0.2561   0.00701   0.00161  -0.0844   0.8289   0.3233
  -0.250   0.3010   0.00674   0.00161  -0.0823   0.8226   0.4093
   0.000   0.3204   0.00661   0.00162  -0.0806   0.8198   0.4530
   0.250   0.3413   0.00643   0.00162  -0.0792   0.8165   0.5112
   0.500   0.3516   0.00585   0.00160  -0.0755   0.8134   0.6841
   1.000   0.5242   0.00616   0.00269  -0.1029   0.7998   0.9257
   1.250   0.5372   0.00638   0.00291  -0.0993   0.7920   0.9417
   1.500   0.5629   0.00654   0.00304  -0.0989   0.7823   0.9454
   1.750   0.5690   0.00673   0.00321  -0.0937   0.7688   0.9544
   2.000   0.5939   0.00695   0.00336  -0.0931   0.7444   0.9570
   2.250   0.5770   0.00743   0.00361  -0.0826   0.6858   0.9656
   2.500   0.5827   0.00827   0.00404  -0.0779   0.5967   0.9684
   2.750   0.5736   0.00942   0.00462  -0.0701   0.4636   0.9730
   3.000   0.5806   0.01005   0.00501  -0.0657   0.4069   0.9770
   3.250   0.6091   0.01042   0.00523  -0.0664   0.3688   0.9782
   3.500   0.6335   0.01081   0.00545  -0.0661   0.3272   0.9796
   3.750   0.6543   0.01128   0.00571  -0.0650   0.2765   0.9816
   4.000   0.6694   0.01189   0.00616  -0.0626   0.2371   0.9860
   4.250   0.6960   0.01231   0.00636  -0.0629   0.1875   0.9868
   4.500   0.7230   0.01260   0.00654  -0.0633   0.1606   0.9877
   4.750   0.7429   0.01304   0.00678  -0.0621   0.1181   0.9886
   5.000   0.7630   0.01342   0.00702  -0.0610   0.0895   0.9895
   5.250   0.7848   0.01372   0.00726  -0.0601   0.0743   0.9905
   5.750   0.8283   0.01422   0.00772  -0.0582   0.0621   0.9923
   6.000   0.8486   0.01450   0.00797  -0.0571   0.0569   0.9931
   6.250   0.8691   0.01479   0.00825  -0.0559   0.0496   0.9941
   6.500   0.8912   0.01506   0.00852  -0.0551   0.0462   0.9949
   6.750   0.9132   0.01532   0.00875  -0.0543   0.0365   0.9953
   7.000   0.9326   0.01572   0.00906  -0.0531   0.0247   0.9957
   7.250   0.9531   0.01603   0.00937  -0.0521   0.0204   0.9962
   7.500   0.9742   0.01638   0.00970  -0.0512   0.0174   0.9968
   7.750   0.9960   0.01669   0.01004  -0.0505   0.0157   0.9975
   8.000   1.0154   0.01710   0.01043  -0.0493   0.0132   0.9980
   8.250   1.0354   0.01743   0.01079  -0.0482   0.0123   0.9984
   8.500   1.0557   0.01783   0.01120  -0.0472   0.0112   0.9989
   8.750   1.0769   0.01823   0.01163  -0.0464   0.0100   0.9995
   9.000   1.0972   0.01865   0.01208  -0.0455   0.0091   0.9999
   9.250   1.1144   0.01906   0.01252  -0.0440   0.0091   1.0000
   9.500   1.1294   0.01952   0.01299  -0.0419   0.0085   1.0000
   9.750   1.1438   0.02002   0.01354  -0.0398   0.0079   1.0000
  10.000   1.1590   0.02046   0.01402  -0.0378   0.0073   1.0000
  10.250   1.1736   0.02096   0.01456  -0.0358   0.0073   1.0000
  10.500   1.1878   0.02150   0.01514  -0.0337   0.0069   1.0000
  10.750   1.2003   0.02217   0.01584  -0.0314   0.0063   1.0000
  11.000   1.2145   0.02270   0.01642  -0.0294   0.0063   1.0000
  11.250   1.2279   0.02331   0.01709  -0.0273   0.0062   1.0000
  11.500   1.2405   0.02398   0.01782  -0.0251   0.0060   1.0000
  11.750   1.2540   0.02455   0.01844  -0.0232   0.0056   1.0000
  12.000   1.2669   0.02519   0.01915  -0.0212   0.0054   1.0000
  12.250   1.2783   0.02594   0.01996  -0.0189   0.0052   1.0000
  12.500   1.2889   0.02674   0.02081  -0.0167   0.0050   1.0000
  12.750   1.2985   0.02766   0.02179  -0.0143   0.0048   1.0000
  13.000   1.3064   0.02867   0.02289  -0.0118   0.0048   1.0000
  13.250   1.3173   0.02947   0.02375  -0.0098   0.0046   1.0000
  13.500   1.3278   0.03028   0.02462  -0.0077   0.0046   1.0000
  13.750   1.3323   0.03158   0.02603  -0.0050   0.0046   1.0000
  14.000   1.3413   0.03254   0.02707  -0.0029   0.0045   1.0000
  14.250   1.3509   0.03347   0.02807  -0.0010   0.0042   1.0000
  14.500   1.3595   0.03450   0.02917   0.0010   0.0041   1.0000
  14.750   1.3627   0.03598   0.03075   0.0035   0.0040   1.0000
  15.000   1.3700   0.03713   0.03198   0.0055   0.0039   1.0000
  15.250   1.3715   0.03878   0.03374   0.0079   0.0040   1.0000
  15.500   1.3771   0.04013   0.03518   0.0098   0.0039   1.0000
  15.750   1.3811   0.04165   0.03679   0.0117   0.0037   1.0000
  16.000   1.3816   0.04352   0.03876   0.0138   0.0036   1.0000
  16.250   1.3843   0.04523   0.04055   0.0155   0.0036   1.0000
  16.500   1.3791   0.04774   0.04318   0.0176   0.0036   1.0000
  16.750   1.3714   0.05062   0.04617   0.0195   0.0034   1.0000
  17.000   1.3694   0.05306   0.04874   0.0210   0.0035   1.0000
  17.250   1.3649   0.05584   0.05162   0.0221   0.0034   1.0000
  17.500   1.3567   0.05921   0.05511   0.0231   0.0034   1.0000
  17.750   1.3579   0.06160   0.05762   0.0236   0.0032   1.0000
  18.000   1.3344   0.06727   0.06345   0.0238   0.0034   1.0000
  18.250   1.3288   0.07092   0.06723   0.0236   0.0033   1.0000
  18.500   1.3182   0.07541   0.07185   0.0228   0.0032   1.0000
  18.750   1.2971   0.08186   0.07848   0.0211   0.0032   1.0000
  19.000   1.2818   0.08774   0.08448   0.0190   0.0032   1.0000
  19.250   1.2563   0.09586   0.09278   0.0155   0.0032   1.0000
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