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GOE 493 AIRFOIL (goe493-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 493 AIRFOIL (goe493-il)
Reynolds number: 500,000
Max Cl/Cd: 95.23 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe493-il-500000-n5.txt
Download as CSV file: xf-goe493-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.7567   0.08678   0.08308  -0.0733   1.0000   0.0104
 -16.250  -0.7732   0.08088   0.07710  -0.0760   1.0000   0.0104
 -16.000  -0.7909   0.07501   0.07114  -0.0786   1.0000   0.0104
 -15.750  -0.8085   0.06931   0.06534  -0.0812   1.0000   0.0105
 -15.500  -0.8314   0.06321   0.05914  -0.0838   1.0000   0.0104
 -15.250  -0.8472   0.05826   0.05409  -0.0857   1.0000   0.0105
 -15.000  -0.8668   0.05315   0.04888  -0.0875   1.0000   0.0105
 -14.750  -0.8843   0.04870   0.04433  -0.0887   1.0000   0.0105
 -14.250  -0.9005   0.03941   0.03481  -0.0955   0.9972   0.0108
 -14.000  -0.8945   0.03542   0.03070  -0.1003   0.9926   0.0110
 -13.750  -0.8858   0.03212   0.02727  -0.1043   0.9876   0.0112
 -13.500  -0.8710   0.02958   0.02462  -0.1080   0.9839   0.0115
 -13.250  -0.8591   0.02752   0.02245  -0.1100   0.9772   0.0118
 -13.000  -0.8411   0.02571   0.02051  -0.1125   0.9733   0.0122
 -12.750  -0.8275   0.02425   0.01894  -0.1133   0.9660   0.0125
 -12.500  -0.8051   0.02303   0.01759  -0.1149   0.9621   0.0129
 -12.250  -0.7838   0.02197   0.01642  -0.1158   0.9572   0.0133
 -12.000  -0.7644   0.02091   0.01526  -0.1161   0.9510   0.0137
 -11.750  -0.7393   0.01986   0.01413  -0.1173   0.9470   0.0143
 -11.500  -0.7193   0.01910   0.01330  -0.1171   0.9403   0.0149
 -11.250  -0.6952   0.01840   0.01250  -0.1174   0.9349   0.0158
 -11.000  -0.6692   0.01776   0.01176  -0.1180   0.9304   0.0166
 -10.750  -0.6511   0.01715   0.01108  -0.1170   0.9230   0.0175
 -10.500  -0.6281   0.01654   0.01041  -0.1168   0.9174   0.0187
 -10.250  -0.6065   0.01604   0.00983  -0.1162   0.9117   0.0200
 -10.000  -0.5855   0.01558   0.00930  -0.1154   0.9052   0.0214
  -9.750  -0.5624   0.01508   0.00875  -0.1150   0.9000   0.0234
  -9.500  -0.5414   0.01468   0.00830  -0.1141   0.8941   0.0260
  -9.250  -0.5198   0.01425   0.00783  -0.1133   0.8883   0.0292
  -9.000  -0.4962   0.01383   0.00736  -0.1129   0.8834   0.0332
  -8.750  -0.4748   0.01347   0.00698  -0.1119   0.8777   0.0375
  -8.500  -0.4522   0.01310   0.00659  -0.1112   0.8721   0.0431
  -8.250  -0.4281   0.01273   0.00621  -0.1108   0.8673   0.0503
  -8.000  -0.4059   0.01240   0.00589  -0.1099   0.8617   0.0582
  -7.750  -0.3822   0.01210   0.00559  -0.1093   0.8561   0.0664
  -7.500  -0.3569   0.01185   0.00531  -0.1090   0.8515   0.0742
  -7.250  -0.3331   0.01162   0.00508  -0.1084   0.8458   0.0821
  -7.000  -0.3085   0.01138   0.00483  -0.1079   0.8403   0.0890
  -6.750  -0.2824   0.01120   0.00461  -0.1077   0.8356   0.0960
  -6.500  -0.2584   0.01097   0.00440  -0.1071   0.8299   0.1041
  -6.250  -0.2328   0.01081   0.00419  -0.1067   0.8245   0.1109
  -6.000  -0.2072   0.01060   0.00397  -0.1064   0.8195   0.1180
  -5.750  -0.1821   0.01045   0.00380  -0.1059   0.8137   0.1244
  -5.500  -0.1569   0.01025   0.00360  -0.1055   0.8079   0.1327
  -5.250  -0.1309   0.01010   0.00342  -0.1052   0.8027   0.1419
  -5.000  -0.1058   0.00992   0.00326  -0.1047   0.7966   0.1527
  -4.750  -0.0802   0.00975   0.00310  -0.1043   0.7908   0.1645
  -4.500  -0.0546   0.00960   0.00295  -0.1040   0.7850   0.1771
  -4.250  -0.0291   0.00945   0.00281  -0.1036   0.7784   0.1901
  -4.000  -0.0034   0.00930   0.00267  -0.1032   0.7726   0.2071
  -3.750   0.0220   0.00914   0.00255  -0.1028   0.7663   0.2247
  -3.500   0.0475   0.00900   0.00244  -0.1024   0.7597   0.2432
  -3.250   0.0731   0.00887   0.00233  -0.1020   0.7532   0.2644
  -3.000   0.0982   0.00871   0.00225  -0.1015   0.7461   0.2902
  -2.750   0.1238   0.00860   0.00216  -0.1011   0.7398   0.3156
  -2.500   0.1492   0.00848   0.00211  -0.1007   0.7328   0.3389
  -2.250   0.1749   0.00841   0.00205  -0.1002   0.7258   0.3610
  -2.000   0.2003   0.00832   0.00201  -0.0998   0.7184   0.3843
  -1.750   0.2259   0.00826   0.00198  -0.0993   0.7110   0.4059
  -1.500   0.2517   0.00822   0.00196  -0.0989   0.7040   0.4244
  -1.250   0.2771   0.00820   0.00194  -0.0984   0.6953   0.4416
  -1.000   0.3025   0.00818   0.00194  -0.0979   0.6862   0.4587
  -0.750   0.3273   0.00819   0.00194  -0.0973   0.6767   0.4776
  -0.500   0.3524   0.00817   0.00195  -0.0967   0.6674   0.4965
  -0.250   0.3774   0.00818   0.00196  -0.0961   0.6587   0.5130
   0.000   0.4022   0.00820   0.00198  -0.0955   0.6487   0.5268
   0.250   0.4270   0.00822   0.00201  -0.0949   0.6393   0.5402
   0.750   0.4764   0.00829   0.00208  -0.0936   0.6211   0.5670
   1.000   0.5008   0.00833   0.00213  -0.0929   0.6135   0.5825
   1.250   0.5257   0.00834   0.00219  -0.0923   0.6055   0.5989
   1.500   0.5499   0.00838   0.00225  -0.0915   0.5985   0.6143
   1.750   0.5749   0.00840   0.00231  -0.0910   0.5918   0.6299
   2.250   0.6231   0.00846   0.00247  -0.0894   0.5784   0.6650
   2.500   0.6468   0.00849   0.00257  -0.0886   0.5711   0.6860
   2.750   0.6698   0.00853   0.00267  -0.0876   0.5642   0.7097
   3.000   0.6930   0.00856   0.00278  -0.0866   0.5565   0.7342
   3.250   0.7150   0.00862   0.00289  -0.0854   0.5493   0.7595
   3.500   0.7375   0.00865   0.00301  -0.0843   0.5410   0.7847
   3.750   0.7578   0.00872   0.00313  -0.0827   0.5302   0.8109
   4.000   0.7771   0.00879   0.00326  -0.0809   0.5184   0.8416
   4.250   0.7998   0.00883   0.00341  -0.0798   0.5063   0.8814
   4.500   0.8450   0.00907   0.00368  -0.0838   0.4863   0.9358
   4.750   0.8980   0.00943   0.00397  -0.0898   0.4591   0.9954
   5.000   0.9158   0.00971   0.00417  -0.0879   0.4402   1.0000
   5.250   0.9278   0.00996   0.00434  -0.0848   0.4210   1.0000
   5.500   0.9375   0.01031   0.00457  -0.0812   0.3950   1.0000
   5.750   0.9478   0.01071   0.00484  -0.0779   0.3693   1.0000
   6.000   0.9584   0.01116   0.00516  -0.0748   0.3454   1.0000
   6.250   0.9721   0.01156   0.00548  -0.0723   0.3264   1.0000
   6.500   0.9863   0.01197   0.00582  -0.0700   0.3088   1.0000
   6.750   1.0010   0.01239   0.00618  -0.0677   0.2915   1.0000
   7.000   1.0142   0.01289   0.00658  -0.0653   0.2693   1.0000
   7.250   1.0252   0.01350   0.00705  -0.0627   0.2388   1.0000
   7.500   1.0228   0.01475   0.00791  -0.0581   0.1706   1.0000
   7.750   1.0298   0.01565   0.00865  -0.0550   0.1407   1.0000
   8.000   1.0380   0.01654   0.00940  -0.0523   0.1117   1.0000
   8.250   1.0449   0.01752   0.01022  -0.0495   0.0836   1.0000
   8.500   1.0557   0.01833   0.01096  -0.0473   0.0680   1.0000
   8.750   1.0671   0.01915   0.01172  -0.0453   0.0543   1.0000
   9.000   1.0785   0.01999   0.01251  -0.0434   0.0451   1.0000
   9.250   1.0915   0.02076   0.01328  -0.0417   0.0409   1.0000
   9.500   1.1054   0.02150   0.01404  -0.0401   0.0386   1.0000
   9.750   1.1180   0.02234   0.01489  -0.0385   0.0364   1.0000
  10.000   1.1300   0.02323   0.01581  -0.0369   0.0348   1.0000
  10.250   1.1433   0.02407   0.01669  -0.0355   0.0338   1.0000
  10.500   1.1561   0.02496   0.01764  -0.0342   0.0329   1.0000
  10.750   1.1685   0.02590   0.01863  -0.0328   0.0319   1.0000
  11.000   1.1796   0.02695   0.01972  -0.0314   0.0309   1.0000
  11.250   1.1895   0.02811   0.02091  -0.0300   0.0299   1.0000
  11.500   1.1979   0.02941   0.02226  -0.0285   0.0289   1.0000
  11.750   1.2057   0.03081   0.02371  -0.0271   0.0282   1.0000
  12.000   1.2173   0.03194   0.02491  -0.0261   0.0275   1.0000
  12.250   1.2268   0.03326   0.02630  -0.0250   0.0269   1.0000
  12.500   1.2363   0.03463   0.02773  -0.0239   0.0262   1.0000
  12.750   1.2453   0.03608   0.02924  -0.0229   0.0256   1.0000
  13.000   1.2531   0.03765   0.03087  -0.0220   0.0249   1.0000
  13.250   1.2599   0.03935   0.03263  -0.0211   0.0242   1.0000
  13.500   1.2647   0.04129   0.03461  -0.0202   0.0235   1.0000
  13.750   1.2683   0.04339   0.03678  -0.0193   0.0229   1.0000
  14.000   1.2789   0.04488   0.03835  -0.0188   0.0222   1.0000
  14.250   1.2844   0.04687   0.04042  -0.0182   0.0218   1.0000
  14.500   1.2927   0.04864   0.04225  -0.0177   0.0210   1.0000
  14.750   1.2989   0.05065   0.04433  -0.0173   0.0204   1.0000
  15.000   1.3050   0.05269   0.04644  -0.0170   0.0198   1.0000
  15.250   1.3086   0.05505   0.04885  -0.0166   0.0193   1.0000
  15.500   1.3110   0.05756   0.05142  -0.0164   0.0188   1.0000
  15.750   1.3142   0.06003   0.05397  -0.0162   0.0184   1.0000
  16.000   1.3185   0.06242   0.05646  -0.0161   0.0179   1.0000
  16.250   1.3228   0.06485   0.05897  -0.0161   0.0173   1.0000
  16.500   1.3263   0.06740   0.06160  -0.0162   0.0167   1.0000
  16.750   1.3289   0.07009   0.06437  -0.0163   0.0162   1.0000
  17.000   1.3323   0.07270   0.06704  -0.0165   0.0157   1.0000
  17.250   1.3330   0.07570   0.07011  -0.0168   0.0153   1.0000
  17.500   1.3323   0.07892   0.07339  -0.0173   0.0149   1.0000
  17.750   1.3323   0.08209   0.07666  -0.0177   0.0146   1.0000
  18.000   1.3333   0.08515   0.07981  -0.0182   0.0140   1.0000
  18.250   1.3325   0.08847   0.08323  -0.0189   0.0136   1.0000
  18.500   1.3322   0.09180   0.08664  -0.0196   0.0132   1.0000
  18.750   1.3305   0.09536   0.09028  -0.0205   0.0128   1.0000
  19.000   1.3286   0.09900   0.09400  -0.0215   0.0125   1.0000
  19.250   1.3256   0.10285   0.09793  -0.0226   0.0122   1.0000
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