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GOE 629 AIRFOIL (goe629-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 629 AIRFOIL (goe629-il)
Reynolds number: 500,000
Max Cl/Cd: 81.93 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe629-il-500000-n5.txt
Download as CSV file: xf-goe629-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 629 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.9175   0.08084   0.07718  -0.0657   1.0000   0.0238
 -16.500  -0.9820   0.06817   0.06431  -0.0729   1.0000   0.0229
 -16.250  -1.0519   0.05463   0.05051  -0.0809   1.0000   0.0216
 -16.000  -1.1010   0.04327   0.03888  -0.0890   1.0000   0.0211
 -15.750  -1.1260   0.03661   0.03200  -0.0938   1.0000   0.0210
 -15.500  -1.1434   0.03273   0.02798  -0.0948   1.0000   0.0215
 -15.250  -1.1558   0.03032   0.02545  -0.0934   1.0000   0.0221
 -15.000  -1.1668   0.02861   0.02364  -0.0904   1.0000   0.0229
 -14.500  -1.1934   0.02652   0.02141  -0.0803   1.0000   0.0243
 -14.250  -1.2010   0.02564   0.02047  -0.0754   0.9997   0.0254
 -14.000  -1.1791   0.02439   0.01914  -0.0762   0.9971   0.0280
 -13.750  -1.1561   0.02329   0.01797  -0.0769   0.9943   0.0308
 -13.500  -1.1340   0.02232   0.01694  -0.0772   0.9914   0.0338
 -13.250  -1.1104   0.02152   0.01607  -0.0774   0.9884   0.0367
 -13.000  -1.0851   0.02075   0.01526  -0.0779   0.9858   0.0400
 -12.750  -1.0575   0.02009   0.01455  -0.0787   0.9838   0.0427
 -12.500  -1.0295   0.01949   0.01391  -0.0795   0.9820   0.0455
 -12.250  -1.0063   0.01900   0.01333  -0.0791   0.9781   0.0476
 -12.000  -0.9795   0.01847   0.01278  -0.0795   0.9753   0.0498
 -11.750  -0.9503   0.01802   0.01228  -0.0802   0.9733   0.0525
 -11.500  -0.9198   0.01760   0.01178  -0.0811   0.9717   0.0545
 -11.250  -0.8892   0.01712   0.01129  -0.0821   0.9704   0.0567
 -11.000  -0.8661   0.01677   0.01090  -0.0815   0.9657   0.0586
 -10.750  -0.8376   0.01642   0.01048  -0.0818   0.9628   0.0606
 -10.500  -0.8069   0.01608   0.01006  -0.0827   0.9607   0.0623
 -10.250  -0.7757   0.01565   0.00963  -0.0837   0.9589   0.0647
 -10.000  -0.7434   0.01532   0.00928  -0.0849   0.9573   0.0672
  -9.750  -0.7167   0.01507   0.00896  -0.0848   0.9533   0.0692
  -9.500  -0.6891   0.01482   0.00864  -0.0848   0.9490   0.0707
  -9.250  -0.6599   0.01436   0.00817  -0.0853   0.9453   0.0729
  -9.000  -0.6274   0.01396   0.00774  -0.0864   0.9423   0.0747
  -8.750  -0.6024   0.01366   0.00740  -0.0859   0.9357   0.0761
  -8.500  -0.5738   0.01335   0.00704  -0.0861   0.9300   0.0776
  -8.250  -0.5416   0.01305   0.00667  -0.0870   0.9255   0.0793
  -8.000  -0.5173   0.01283   0.00638  -0.0863   0.9172   0.0804
  -7.750  -0.4890   0.01248   0.00600  -0.0864   0.9108   0.0821
  -7.500  -0.4633   0.01218   0.00568  -0.0860   0.9046   0.0840
  -7.250  -0.4374   0.01193   0.00541  -0.0856   0.8982   0.0860
  -7.000  -0.4091   0.01169   0.00512  -0.0856   0.8926   0.0881
  -6.750  -0.3840   0.01149   0.00488  -0.0850   0.8855   0.0898
  -6.500  -0.3570   0.01130   0.00464  -0.0848   0.8791   0.0913
  -6.250  -0.3305   0.01107   0.00439  -0.0844   0.8731   0.0941
  -6.000  -0.3050   0.01087   0.00418  -0.0839   0.8659   0.0972
  -5.750  -0.2777   0.01069   0.00397  -0.0837   0.8593   0.1003
  -5.500  -0.2520   0.01054   0.00380  -0.0831   0.8516   0.1031
  -5.250  -0.2255   0.01036   0.00362  -0.0827   0.8440   0.1079
  -5.000  -0.1993   0.01023   0.00347  -0.0823   0.8366   0.1133
  -4.750  -0.1730   0.01009   0.00333  -0.0818   0.8289   0.1186
  -4.500  -0.1465   0.00997   0.00320  -0.0814   0.8216   0.1245
  -4.250  -0.1200   0.00989   0.00308  -0.0810   0.8133   0.1293
  -4.000  -0.0938   0.00977   0.00296  -0.0805   0.8051   0.1349
  -3.750  -0.0676   0.00969   0.00286  -0.0800   0.7957   0.1404
  -3.500  -0.0411   0.00963   0.00275  -0.0796   0.7868   0.1446
  -3.250  -0.0152   0.00952   0.00265  -0.0791   0.7774   0.1498
  -3.000   0.0110   0.00945   0.00256  -0.0786   0.7682   0.1544
  -2.750   0.0371   0.00941   0.00247  -0.0780   0.7575   0.1581
  -2.500   0.0626   0.00936   0.00237  -0.0773   0.7443   0.1620
  -2.250   0.0876   0.00930   0.00229  -0.0766   0.7294   0.1669
  -2.000   0.1128   0.00927   0.00222  -0.0759   0.7146   0.1718
  -1.750   0.1380   0.00926   0.00216  -0.0751   0.7000   0.1766
  -1.500   0.1626   0.00922   0.00210  -0.0743   0.6847   0.1831
  -1.250   0.1871   0.00922   0.00205  -0.0735   0.6681   0.1894
  -1.000   0.2113   0.00923   0.00201  -0.0726   0.6499   0.1968
  -0.750   0.2353   0.00922   0.00199  -0.0717   0.6331   0.2087
  -0.500   0.2595   0.00920   0.00198  -0.0708   0.6192   0.2253
  -0.250   0.2840   0.00917   0.00197  -0.0700   0.6064   0.2444
   0.000   0.3082   0.00913   0.00198  -0.0692   0.5938   0.2697
   0.500   0.3565   0.00907   0.00202  -0.0675   0.5719   0.3237
   0.750   0.3812   0.00903   0.00205  -0.0667   0.5629   0.3525
   1.000   0.4050   0.00898   0.00209  -0.0658   0.5540   0.3886
   1.250   0.4291   0.00891   0.00214  -0.0650   0.5454   0.4296
   1.500   0.4524   0.00886   0.00220  -0.0640   0.5368   0.4743
   1.750   0.4757   0.00877   0.00226  -0.0630   0.5283   0.5255
   2.000   0.4978   0.00867   0.00233  -0.0617   0.5207   0.5848
   2.250   0.5187   0.00850   0.00241  -0.0602   0.5138   0.6607
   2.500   0.5380   0.00831   0.00251  -0.0582   0.5062   0.7516
   2.750   0.5594   0.00821   0.00264  -0.0565   0.4973   0.8279
   3.000   0.5971   0.00828   0.00285  -0.0584   0.4834   0.9055
   3.250   0.6529   0.00853   0.00308  -0.0643   0.4635   0.9449
   3.500   0.6948   0.00878   0.00324  -0.0674   0.4379   0.9616
   3.750   0.7290   0.00906   0.00340  -0.0688   0.4115   0.9732
   4.000   0.7590   0.00938   0.00358  -0.0693   0.3830   0.9830
   4.250   0.7911   0.00980   0.00381  -0.0705   0.3489   0.9902
   4.750   0.8578   0.01047   0.00427  -0.0732   0.3082   1.0000
   5.000   0.8752   0.01069   0.00444  -0.0711   0.2973   1.0000
   5.250   0.8925   0.01092   0.00462  -0.0690   0.2856   1.0000
   5.500   0.9102   0.01115   0.00480  -0.0669   0.2728   1.0000
   5.750   0.9272   0.01140   0.00500  -0.0648   0.2585   1.0000
   6.000   0.9441   0.01166   0.00521  -0.0626   0.2441   1.0000
   6.250   0.9599   0.01197   0.00544  -0.0603   0.2259   1.0000
   6.500   0.9746   0.01234   0.00570  -0.0577   0.2058   1.0000
   6.750   0.9875   0.01277   0.00600  -0.0549   0.1825   1.0000
   7.000   0.9979   0.01320   0.00633  -0.0516   0.1632   1.0000
   7.250   1.0101   0.01357   0.00664  -0.0486   0.1502   1.0000
   7.500   1.0228   0.01396   0.00697  -0.0458   0.1376   1.0000
   7.750   1.0365   0.01435   0.00731  -0.0432   0.1270   1.0000
   8.000   1.0501   0.01478   0.00769  -0.0407   0.1160   1.0000
   8.250   1.0636   0.01524   0.00810  -0.0382   0.1046   1.0000
   8.500   1.0784   0.01567   0.00850  -0.0361   0.0961   1.0000
   8.750   1.0923   0.01617   0.00895  -0.0338   0.0870   1.0000
   9.000   1.1066   0.01667   0.00943  -0.0317   0.0803   1.0000
   9.250   1.1211   0.01717   0.00992  -0.0296   0.0734   1.0000
   9.500   1.1354   0.01771   0.01044  -0.0276   0.0662   1.0000
   9.750   1.1475   0.01838   0.01105  -0.0254   0.0553   1.0000
  10.000   1.1581   0.01915   0.01176  -0.0231   0.0452   1.0000
  10.250   1.1697   0.01990   0.01249  -0.0209   0.0405   1.0000
  10.500   1.1825   0.02061   0.01321  -0.0191   0.0381   1.0000
  10.750   1.1948   0.02136   0.01398  -0.0172   0.0364   1.0000
  11.000   1.2064   0.02219   0.01483  -0.0153   0.0348   1.0000
  11.250   1.2192   0.02296   0.01566  -0.0137   0.0340   1.0000
  11.500   1.2314   0.02381   0.01655  -0.0121   0.0332   1.0000
  11.750   1.2427   0.02473   0.01753  -0.0105   0.0324   1.0000
  12.000   1.2534   0.02573   0.01858  -0.0089   0.0319   1.0000
  12.250   1.2626   0.02687   0.01976  -0.0074   0.0312   1.0000
  12.500   1.2705   0.02814   0.02107  -0.0058   0.0306   1.0000
  12.750   1.2770   0.02958   0.02256  -0.0043   0.0300   1.0000
  13.000   1.2861   0.03085   0.02390  -0.0031   0.0296   1.0000
  13.250   1.2950   0.03218   0.02531  -0.0020   0.0292   1.0000
  13.500   1.3024   0.03368   0.02688  -0.0009   0.0287   1.0000
  13.750   1.3093   0.03527   0.02855   0.0000   0.0283   1.0000
  14.000   1.3150   0.03702   0.03037   0.0009   0.0278   1.0000
  14.250   1.3203   0.03888   0.03229   0.0017   0.0274   1.0000
  14.500   1.3244   0.04091   0.03440   0.0023   0.0270   1.0000
  14.750   1.3276   0.04309   0.03664   0.0028   0.0266   1.0000
  15.000   1.3292   0.04553   0.03915   0.0032   0.0263   1.0000
  15.250   1.3282   0.04831   0.04201   0.0034   0.0259   1.0000
  15.500   1.3253   0.05140   0.04517   0.0035   0.0255   1.0000
  15.750   1.3260   0.05415   0.04800   0.0035   0.0253   1.0000
  16.000   1.3290   0.05670   0.05065   0.0033   0.0250   1.0000
  16.250   1.3294   0.05961   0.05365   0.0031   0.0248   1.0000
  16.500   1.3295   0.06262   0.05676   0.0027   0.0245   1.0000
  16.750   1.3293   0.06570   0.05993   0.0022   0.0241   1.0000
  17.000   1.3278   0.06898   0.06329   0.0017   0.0238   1.0000
  17.250   1.3259   0.07237   0.06678   0.0010   0.0235   1.0000
  17.500   1.3232   0.07593   0.07043   0.0002   0.0232   1.0000
  17.750   1.3194   0.07965   0.07424  -0.0007   0.0230   1.0000
  18.000   1.3153   0.08349   0.07816  -0.0017   0.0227   1.0000
  18.250   1.3110   0.08742   0.08217  -0.0029   0.0224   1.0000
  18.500   1.3056   0.09154   0.08638  -0.0041   0.0222   1.0000
  18.750   1.2993   0.09584   0.09074  -0.0055   0.0219   1.0000
  19.000   1.2933   0.10011   0.09509  -0.0070   0.0218   1.0000
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