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GOE 480 AIRFOIL (goe480-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 480 AIRFOIL (goe480-il)
Reynolds number: 500,000
Max Cl/Cd: 107.19 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe480-il-500000-n5.txt
Download as CSV file: xf-goe480-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 480 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.2841   0.10382   0.10131  -0.0530   0.9884   0.0259
 -11.000  -0.2708   0.10072   0.09820  -0.0559   0.9817   0.0265
 -10.750  -0.2772   0.09258   0.09004  -0.0621   0.9732   0.0289
 -10.500  -0.2582   0.08994   0.08738  -0.0656   0.9641   0.0292
 -10.250  -0.2325   0.08766   0.08508  -0.0698   0.9552   0.0297
 -10.000  -0.2056   0.08394   0.08132  -0.0763   0.9466   0.0304
  -9.750  -0.1991   0.07343   0.07073  -0.0901   0.9316   0.0334
  -9.500  -0.1627   0.07096   0.06818  -0.0969   0.9140   0.0339
  -9.250  -0.1370   0.06802   0.06512  -0.1025   0.8886   0.0343
  -9.000  -0.1259   0.06556   0.06252  -0.1048   0.8609   0.0348
  -8.750  -0.1265   0.06275   0.05961  -0.1059   0.8373   0.0353
  -8.500  -0.2211   0.04272   0.03932  -0.1207   0.8072   0.0387
  -8.250  -0.2129   0.03895   0.03538  -0.1228   0.7961   0.0392
  -8.000  -0.2083   0.03358   0.02975  -0.1248   0.7860   0.0400
  -7.750  -0.2089   0.02741   0.02304  -0.1257   0.7775   0.0412
  -7.500  -0.1988   0.02383   0.01897  -0.1253   0.7695   0.0422
  -7.250  -0.1820   0.02167   0.01639  -0.1246   0.7627   0.0432
  -7.000  -0.1617   0.02016   0.01458  -0.1240   0.7562   0.0438
  -6.750  -0.1392   0.01918   0.01335  -0.1234   0.7497   0.0441
  -6.500  -0.1159   0.01835   0.01230  -0.1228   0.7441   0.0444
  -6.250  -0.0929   0.01725   0.01106  -0.1223   0.7381   0.0448
  -6.000  -0.0681   0.01667   0.01039  -0.1219   0.7324   0.0452
  -5.750  -0.0427   0.01627   0.00992  -0.1215   0.7272   0.0456
  -5.500  -0.0170   0.01582   0.00939  -0.1211   0.7216   0.0460
  -5.250   0.0086   0.01535   0.00883  -0.1207   0.7161   0.0463
  -4.750   0.0605   0.01447   0.00775  -0.1199   0.7058   0.0470
  -4.500   0.0866   0.01405   0.00724  -0.1196   0.7002   0.0474
  -4.250   0.1127   0.01368   0.00677  -0.1191   0.6948   0.0478
  -4.000   0.1392   0.01331   0.00633  -0.1188   0.6898   0.0482
  -3.750   0.1657   0.01296   0.00592  -0.1184   0.6841   0.0486
  -3.500   0.1921   0.01266   0.00554  -0.1180   0.6784   0.0491
  -3.250   0.2187   0.01238   0.00520  -0.1177   0.6731   0.0496
  -3.000   0.2455   0.01213   0.00490  -0.1174   0.6670   0.0501
  -2.750   0.2721   0.01195   0.00466  -0.1170   0.6608   0.0506
  -2.500   0.2989   0.01174   0.00440  -0.1166   0.6551   0.0510
  -2.250   0.3256   0.01154   0.00416  -0.1162   0.6482   0.0513
  -2.000   0.3520   0.01139   0.00396  -0.1158   0.6416   0.0515
  -1.750   0.3781   0.01102   0.00358  -0.1154   0.6348   0.0521
  -1.500   0.4041   0.01078   0.00332  -0.1149   0.6272   0.0528
  -1.250   0.4304   0.01062   0.00314  -0.1145   0.6199   0.0534
  -1.000   0.4567   0.01049   0.00299  -0.1140   0.6118   0.0540
  -0.750   0.4829   0.01039   0.00287  -0.1136   0.6040   0.0546
  -0.500   0.5092   0.01030   0.00277  -0.1131   0.5953   0.0554
  -0.250   0.5353   0.01024   0.00268  -0.1127   0.5870   0.0563
   0.000   0.5613   0.01020   0.00261  -0.1122   0.5776   0.0574
   0.250   0.5874   0.01017   0.00256  -0.1117   0.5690   0.0583
   0.500   0.6131   0.01016   0.00251  -0.1112   0.5595   0.0591
   0.750   0.6391   0.01015   0.00247  -0.1107   0.5506   0.0598
   1.000   0.6646   0.01018   0.00246  -0.1101   0.5412   0.0603
   1.250   0.6905   0.01015   0.00242  -0.1096   0.5322   0.0619
   1.500   0.7155   0.01019   0.00242  -0.1089   0.5225   0.0636
   1.750   0.7413   0.01022   0.00244  -0.1084   0.5128   0.0656
   2.000   0.7664   0.01028   0.00248  -0.1078   0.5039   0.0678
   2.250   0.7919   0.01034   0.00252  -0.1073   0.4945   0.0709
   2.500   0.8170   0.01039   0.00259  -0.1066   0.4864   0.0800
   2.750   0.8416   0.01029   0.00271  -0.1060   0.4783   0.1632
   3.000   0.8660   0.01033   0.00282  -0.1054   0.4704   0.2067
   3.250   0.8897   0.01018   0.00297  -0.1046   0.4618   0.3294
   3.500   0.9081   0.00970   0.00318  -0.1030   0.4544   0.6284
   4.000   0.9921   0.00943   0.00356  -0.1092   0.4362   1.0000
   4.250   1.0158   0.00959   0.00369  -0.1083   0.4273   1.0000
   4.500   1.0388   0.00978   0.00384  -0.1074   0.4193   1.0000
   4.750   1.0624   0.00995   0.00399  -0.1065   0.4113   1.0000
   5.000   1.0850   0.01016   0.00416  -0.1055   0.4037   1.0000
   5.250   1.1083   0.01034   0.00432  -0.1045   0.3953   1.0000
   5.500   1.1301   0.01057   0.00451  -0.1034   0.3862   1.0000
   5.750   1.1516   0.01082   0.00471  -0.1022   0.3745   1.0000
   6.000   1.1729   0.01106   0.00493  -0.1010   0.3627   1.0000
   6.250   1.1934   0.01134   0.00516  -0.0996   0.3523   1.0000
   6.500   1.2145   0.01158   0.00539  -0.0984   0.3432   1.0000
   6.750   1.2349   0.01185   0.00564  -0.0970   0.3342   1.0000
   7.000   1.2535   0.01218   0.00592  -0.0953   0.3232   1.0000
   7.250   1.2727   0.01246   0.00618  -0.0938   0.3126   1.0000
   7.500   1.2895   0.01277   0.00648  -0.0918   0.3043   1.0000
   7.750   1.3063   0.01309   0.00678  -0.0898   0.2944   1.0000
   8.000   1.3220   0.01346   0.00712  -0.0877   0.2839   1.0000
   8.250   1.3365   0.01388   0.00750  -0.0854   0.2728   1.0000
   8.500   1.3504   0.01435   0.00793  -0.0831   0.2597   1.0000
   8.750   1.3638   0.01486   0.00838  -0.0808   0.2455   1.0000
   9.000   1.3760   0.01545   0.00891  -0.0784   0.2306   1.0000
   9.250   1.3892   0.01601   0.00944  -0.0763   0.2188   1.0000
   9.500   1.4011   0.01666   0.01005  -0.0740   0.2060   1.0000
   9.750   1.4120   0.01738   0.01072  -0.0717   0.1922   1.0000
  10.000   1.4225   0.01816   0.01145  -0.0695   0.1784   1.0000
  10.250   1.4316   0.01905   0.01228  -0.0672   0.1629   1.0000
  10.500   1.4365   0.02023   0.01336  -0.0645   0.1408   1.0000
  10.750   1.4384   0.02168   0.01468  -0.0618   0.1171   1.0000
  11.000   1.4357   0.02351   0.01636  -0.0588   0.0916   1.0000
  11.250   1.4390   0.02506   0.01785  -0.0566   0.0789   1.0000
  11.500   1.4445   0.02650   0.01929  -0.0548   0.0710   1.0000
  11.750   1.4498   0.02803   0.02082  -0.0531   0.0647   1.0000
  12.000   1.4578   0.02941   0.02224  -0.0518   0.0603   1.0000
  12.250   1.4630   0.03103   0.02388  -0.0503   0.0561   1.0000
  12.500   1.4709   0.03250   0.02539  -0.0491   0.0527   1.0000
  12.750   1.4760   0.03423   0.02715  -0.0479   0.0488   1.0000
  13.000   1.4819   0.03594   0.02890  -0.0468   0.0458   1.0000
  13.250   1.4871   0.03774   0.03075  -0.0458   0.0420   1.0000
  13.500   1.4908   0.03974   0.03279  -0.0448   0.0388   1.0000
  13.750   1.4943   0.04181   0.03490  -0.0439   0.0356   1.0000
  14.000   1.4962   0.04409   0.03721  -0.0431   0.0329   1.0000
  14.250   1.4988   0.04637   0.03955  -0.0424   0.0307   1.0000
  14.500   1.4998   0.04889   0.04211  -0.0418   0.0288   1.0000
  14.750   1.5004   0.05150   0.04478  -0.0413   0.0272   1.0000
  15.000   1.5016   0.05412   0.04748  -0.0409   0.0259   1.0000
  15.250   1.5014   0.05697   0.05040  -0.0406   0.0248   1.0000
  15.500   1.4993   0.06012   0.05362  -0.0405   0.0236   1.0000
  15.750   1.4979   0.06325   0.05683  -0.0405   0.0228   1.0000
  16.000   1.4971   0.06636   0.06002  -0.0405   0.0220   1.0000
  16.250   1.4949   0.06971   0.06346  -0.0407   0.0210   1.0000
  16.500   1.4916   0.07329   0.06712  -0.0411   0.0203   1.0000
  16.750   1.4878   0.07698   0.07090  -0.0415   0.0198   1.0000
  17.000   1.4820   0.08100   0.07499  -0.0421   0.0192   1.0000
  17.250   1.4788   0.08473   0.07882  -0.0427   0.0187   1.0000
  17.500   1.4749   0.08862   0.08280  -0.0435   0.0183   1.0000
  17.750   1.4704   0.09264   0.08693  -0.0443   0.0178   1.0000
  18.000   1.4652   0.09682   0.09119  -0.0453   0.0173   1.0000
  18.250   1.4598   0.10107   0.09554  -0.0465   0.0169   1.0000
  18.500   1.4537   0.10551   0.10005  -0.0478   0.0165   1.0000
  18.750   1.4470   0.11011   0.10474  -0.0492   0.0161   1.0000
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