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GOE 493 AIRFOIL (goe493-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 493 AIRFOIL (goe493-il)
Reynolds number: 500,000
Max Cl/Cd: 105.9 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe493-il-500000.txt
Download as CSV file: xf-goe493-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 493 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.6573   0.11018   0.10726  -0.0638   1.0000   0.0171
 -16.750  -0.7004   0.09796   0.09485  -0.0704   1.0000   0.0168
 -16.500  -0.7283   0.08921   0.08594  -0.0752   1.0000   0.0167
 -16.250  -0.7502   0.08197   0.07857  -0.0791   1.0000   0.0167
 -16.000  -0.7685   0.07566   0.07213  -0.0825   1.0000   0.0167
 -15.750  -0.7859   0.06983   0.06618  -0.0855   1.0000   0.0168
 -15.500  -0.8017   0.06467   0.06090  -0.0879   1.0000   0.0169
 -15.250  -0.8153   0.06010   0.05621  -0.0899   1.0000   0.0169
 -15.000  -0.8283   0.05589   0.05189  -0.0914   1.0000   0.0170
 -14.750  -0.8412   0.05200   0.04789  -0.0925   1.0000   0.0171
 -14.500  -0.8517   0.04870   0.04450  -0.0930   1.0000   0.0172
 -14.250  -0.8650   0.04558   0.04127  -0.0929   1.0000   0.0174
 -14.000  -0.8789   0.04303   0.03864  -0.0917   1.0000   0.0174
 -13.750  -0.8972   0.04076   0.03630  -0.0894   1.0000   0.0175
 -13.500  -0.9022   0.03827   0.03369  -0.0898   0.9990   0.0176
 -13.250  -0.8865   0.03542   0.03065  -0.0943   0.9960   0.0179
 -13.000  -0.8766   0.03218   0.02730  -0.0977   0.9926   0.0184
 -12.750  -0.8611   0.03004   0.02509  -0.1004   0.9882   0.0190
 -12.500  -0.8403   0.02835   0.02331  -0.1032   0.9849   0.0196
 -12.250  -0.8197   0.02681   0.02167  -0.1052   0.9818   0.0200
 -12.000  -0.8046   0.02556   0.02030  -0.1053   0.9757   0.0206
 -11.750  -0.7811   0.02436   0.01897  -0.1066   0.9726   0.0212
 -11.500  -0.7543   0.02301   0.01749  -0.1084   0.9707   0.0219
 -11.250  -0.7417   0.02169   0.01613  -0.1074   0.9637   0.0226
 -11.000  -0.7152   0.02069   0.01507  -0.1086   0.9609   0.0236
 -10.750  -0.6841   0.01986   0.01417  -0.1104   0.9591   0.0250
 -10.500  -0.6510   0.01906   0.01326  -0.1124   0.9577   0.0261
 -10.250  -0.6316   0.01791   0.01208  -0.1122   0.9529   0.0278
 -10.000  -0.6080   0.01723   0.01136  -0.1121   0.9481   0.0293
  -9.750  -0.5778   0.01661   0.01063  -0.1132   0.9451   0.0310
  -9.500  -0.5502   0.01564   0.00965  -0.1141   0.9423   0.0342
  -9.250  -0.5298   0.01523   0.00916  -0.1130   0.9363   0.0369
  -9.000  -0.5072   0.01451   0.00845  -0.1126   0.9312   0.0420
  -8.750  -0.4802   0.01386   0.00780  -0.1130   0.9276   0.0492
  -8.500  -0.4589   0.01339   0.00735  -0.1120   0.9221   0.0582
  -8.250  -0.4358   0.01299   0.00697  -0.1114   0.9166   0.0693
  -8.000  -0.4082   0.01264   0.00662  -0.1116   0.9125   0.0806
  -7.750  -0.3827   0.01236   0.00635  -0.1113   0.9079   0.0904
  -7.500  -0.3596   0.01213   0.00610  -0.1105   0.9021   0.0979
  -7.250  -0.3324   0.01190   0.00584  -0.1105   0.8976   0.1060
  -7.000  -0.3053   0.01163   0.00555  -0.1105   0.8934   0.1138
  -6.750  -0.2825   0.01148   0.00537  -0.1096   0.8874   0.1206
  -6.500  -0.2570   0.01120   0.00509  -0.1092   0.8824   0.1287
  -6.250  -0.2283   0.01102   0.00485  -0.1095   0.8784   0.1373
  -6.000  -0.2065   0.01078   0.00466  -0.1084   0.8723   0.1471
  -5.750  -0.1810   0.01055   0.00442  -0.1080   0.8670   0.1570
  -5.500  -0.1533   0.01033   0.00418  -0.1081   0.8628   0.1694
  -5.250  -0.1302   0.01012   0.00401  -0.1072   0.8568   0.1836
  -5.000  -0.1052   0.00987   0.00380  -0.1067   0.8513   0.2018
  -4.750  -0.0781   0.00962   0.00359  -0.1067   0.8468   0.2235
  -4.500  -0.0550   0.00939   0.00345  -0.1058   0.8406   0.2476
  -4.250  -0.0299   0.00916   0.00328  -0.1053   0.8349   0.2757
  -4.000  -0.0028   0.00893   0.00312  -0.1053   0.8301   0.3082
  -3.750   0.0203   0.00874   0.00303  -0.1044   0.8235   0.3385
  -3.500   0.0463   0.00858   0.00292  -0.1040   0.8178   0.3672
  -3.250   0.0728   0.00845   0.00283  -0.1037   0.8123   0.3942
  -3.000   0.0976   0.00834   0.00278  -0.1031   0.8055   0.4187
  -2.750   0.1252   0.00826   0.00269  -0.1030   0.7999   0.4407
  -2.500   0.1505   0.00820   0.00266  -0.1024   0.7933   0.4591
  -2.250   0.1767   0.00813   0.00260  -0.1021   0.7868   0.4768
  -2.000   0.2038   0.00809   0.00256  -0.1019   0.7807   0.4941
  -1.750   0.2291   0.00804   0.00253  -0.1013   0.7732   0.5098
  -1.500   0.2572   0.00803   0.00247  -0.1013   0.7671   0.5245
  -1.000   0.3088   0.00797   0.00243  -0.1003   0.7517   0.5542
  -0.750   0.3331   0.00793   0.00243  -0.0995   0.7426   0.5694
  -0.500   0.3596   0.00791   0.00240  -0.0991   0.7348   0.5858
  -0.250   0.3841   0.00788   0.00241  -0.0984   0.7257   0.6007
   0.000   0.4098   0.00787   0.00239  -0.0979   0.7174   0.6153
   0.250   0.4345   0.00785   0.00240  -0.0972   0.7081   0.6305
   0.500   0.4595   0.00784   0.00241  -0.0965   0.6995   0.6469
   0.750   0.4844   0.00783   0.00244  -0.0959   0.6913   0.6655
   1.000   0.5091   0.00783   0.00249  -0.0952   0.6836   0.6866
   1.250   0.5335   0.00783   0.00254  -0.0944   0.6754   0.7096
   1.500   0.5576   0.00783   0.00261  -0.0936   0.6677   0.7337
   1.750   0.5817   0.00785   0.00267  -0.0927   0.6598   0.7589
   2.000   0.6056   0.00785   0.00275  -0.0918   0.6526   0.7847
   2.250   0.6291   0.00786   0.00283  -0.0908   0.6449   0.8116
   2.500   0.6528   0.00787   0.00291  -0.0898   0.6379   0.8403
   2.750   0.6769   0.00786   0.00300  -0.0889   0.6302   0.8731
   3.000   0.7086   0.00790   0.00312  -0.0896   0.6229   0.9112
   3.250   0.7569   0.00801   0.00329  -0.0941   0.6141   0.9447
   3.500   0.8054   0.00817   0.00344  -0.0988   0.6057   0.9680
   3.750   0.8484   0.00833   0.00356  -0.1022   0.5940   0.9847
   4.000   0.8886   0.00849   0.00371  -0.1051   0.5813   1.0000
   4.250   0.9050   0.00860   0.00379  -0.1028   0.5695   1.0000
   4.500   0.9215   0.00875   0.00388  -0.1005   0.5568   1.0000
   4.750   0.9391   0.00891   0.00399  -0.0985   0.5459   1.0000
   5.000   0.9572   0.00904   0.00412  -0.0965   0.5344   1.0000
   5.250   0.9743   0.00920   0.00426  -0.0943   0.5216   1.0000
   5.500   0.9895   0.00939   0.00440  -0.0918   0.5056   1.0000
   5.750   1.0039   0.00960   0.00456  -0.0891   0.4882   1.0000
   6.000   1.0172   0.00983   0.00474  -0.0862   0.4712   1.0000
   6.250   1.0271   0.01010   0.00494  -0.0826   0.4517   1.0000
   6.500   1.0379   0.01040   0.00516  -0.0793   0.4291   1.0000
   6.750   1.0468   0.01081   0.00545  -0.0757   0.4039   1.0000
   7.000   1.0569   0.01125   0.00579  -0.0725   0.3773   1.0000
   7.250   1.0660   0.01179   0.00620  -0.0692   0.3511   1.0000
   7.500   1.0748   0.01239   0.00667  -0.0660   0.3259   1.0000
   7.750   1.0861   0.01295   0.00714  -0.0632   0.3017   1.0000
   8.000   1.0954   0.01362   0.00768  -0.0603   0.2729   1.0000
   8.250   1.0972   0.01466   0.00844  -0.0564   0.2183   1.0000
   8.500   1.0875   0.01637   0.00970  -0.0510   0.1478   1.0000
   9.000   1.0853   0.01926   0.01208  -0.0435   0.0648   1.0000
   9.250   1.0933   0.02031   0.01306  -0.0411   0.0532   1.0000
   9.500   1.1035   0.02126   0.01401  -0.0391   0.0482   1.0000
   9.750   1.1154   0.02214   0.01492  -0.0373   0.0454   1.0000
  10.000   1.1248   0.02320   0.01599  -0.0354   0.0429   1.0000
  10.250   1.1328   0.02438   0.01720  -0.0334   0.0410   1.0000
  10.500   1.1446   0.02535   0.01823  -0.0319   0.0397   1.0000
  10.750   1.1546   0.02646   0.01941  -0.0304   0.0384   1.0000
  11.000   1.1632   0.02770   0.02070  -0.0288   0.0373   1.0000
  11.250   1.1699   0.02913   0.02216  -0.0271   0.0362   1.0000
  11.500   1.1705   0.03104   0.02412  -0.0251   0.0348   1.0000
  11.750   1.1765   0.03263   0.02577  -0.0236   0.0340   1.0000
  12.000   1.1854   0.03403   0.02725  -0.0224   0.0334   1.0000
  12.250   1.1933   0.03554   0.02884  -0.0213   0.0326   1.0000
  12.500   1.2001   0.03720   0.03055  -0.0201   0.0317   1.0000
  12.750   1.2066   0.03891   0.03231  -0.0191   0.0308   1.0000
  13.000   1.2116   0.04078   0.03422  -0.0181   0.0299   1.0000
  13.250   1.2124   0.04307   0.03655  -0.0169   0.0292   1.0000
  13.500   1.2117   0.04548   0.03901  -0.0155   0.0284   1.0000
  13.750   1.2206   0.04714   0.04076  -0.0149   0.0279   1.0000
  14.000   1.2283   0.04893   0.04263  -0.0143   0.0273   1.0000
  14.250   1.2350   0.05083   0.04461  -0.0137   0.0266   1.0000
  14.500   1.2413   0.05281   0.04665  -0.0132   0.0259   1.0000
  14.750   1.2474   0.05483   0.04871  -0.0127   0.0252   1.0000
  15.000   1.2526   0.05694   0.05085  -0.0123   0.0246   1.0000
  15.250   1.2563   0.05905   0.05297  -0.0115   0.0239   1.0000
  15.500   1.2612   0.06106   0.05504  -0.0105   0.0233   1.0000
  15.750   1.2666   0.06335   0.05746  -0.0105   0.0228   1.0000
  16.000   1.2718   0.06562   0.05983  -0.0103   0.0223   1.0000
  16.250   1.2767   0.06794   0.06223  -0.0102   0.0218   1.0000
  16.500   1.2808   0.07035   0.06473  -0.0102   0.0213   1.0000
  16.750   1.2842   0.07296   0.06739  -0.0104   0.0207   1.0000
  17.000   1.2878   0.07549   0.06997  -0.0106   0.0203   1.0000
  17.250   1.2913   0.07802   0.07253  -0.0107   0.0198   1.0000
  17.500   1.2967   0.07983   0.07437  -0.0096   0.0192   1.0000
  17.750   1.2953   0.08332   0.07801  -0.0106   0.0189   1.0000
  18.000   1.2955   0.08650   0.08132  -0.0111   0.0186   1.0000
  18.250   1.2948   0.08987   0.08482  -0.0118   0.0183   1.0000
  18.500   1.2939   0.09326   0.08833  -0.0125   0.0180   1.0000
  18.750   1.2927   0.09674   0.09193  -0.0135   0.0176   1.0000
  19.000   1.2906   0.10038   0.09568  -0.0145   0.0173   1.0000
  19.250   1.2881   0.10418   0.09958  -0.0158   0.0170   1.0000
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