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GOE 493 AIRFOIL (goe493-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: GOE 493 AIRFOIL (goe493-il)
Reynolds number: 50,000
Max Cl/Cd: 24.39 at α=9.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe493-il-50000-n5.txt
Download as CSV file: xf-goe493-il-50000-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 =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.4301   0.10851   0.10116  -0.0594   1.0000   0.0703
 -11.750  -0.4511   0.10172   0.09449  -0.0614   1.0000   0.0709
 -11.500  -0.4806   0.09338   0.08627  -0.0642   1.0000   0.0712
 -11.250  -0.5178   0.08461   0.07761  -0.0674   1.0000   0.0710
 -11.000  -0.5564   0.07712   0.07018  -0.0697   1.0000   0.0702
 -10.750  -0.5964   0.07103   0.06409  -0.0709   1.0000   0.0691
 -10.500  -0.6388   0.06631   0.05936  -0.0703   1.0000   0.0680
 -10.250  -0.6824   0.06300   0.05601  -0.0672   1.0000   0.0667
 -10.000  -0.7159   0.06002   0.05292  -0.0635   1.0000   0.0664
  -9.750  -0.7386   0.05715   0.04988  -0.0604   1.0000   0.0669
  -9.500  -0.7555   0.05426   0.04676  -0.0575   1.0000   0.0684
  -9.250  -0.7679   0.05120   0.04335  -0.0548   1.0000   0.0702
  -9.000  -0.7727   0.04857   0.04043  -0.0524   1.0000   0.0728
  -8.750  -0.7597   0.04731   0.03917  -0.0518   0.9978   0.0767
  -8.500  -0.7422   0.04430   0.03556  -0.0531   0.9920   0.0831
  -8.250  -0.7182   0.04309   0.03437  -0.0542   0.9865   0.0897
  -8.000  -0.6968   0.04114   0.03203  -0.0551   0.9809   0.0985
  -7.750  -0.6725   0.03978   0.03043  -0.0561   0.9751   0.1084
  -7.500  -0.6486   0.03870   0.02929  -0.0568   0.9695   0.1182
  -7.250  -0.6238   0.03749   0.02789  -0.0575   0.9637   0.1296
  -7.000  -0.5975   0.03641   0.02656  -0.0583   0.9582   0.1420
  -6.750  -0.5738   0.03554   0.02544  -0.0585   0.9519   0.1545
  -6.500  -0.5436   0.03480   0.02463  -0.0599   0.9469   0.1680
  -6.250  -0.5217   0.03411   0.02389  -0.0595   0.9402   0.1797
  -6.000  -0.4937   0.03342   0.02307  -0.0603   0.9345   0.1932
  -5.750  -0.4644   0.03279   0.02233  -0.0612   0.9293   0.2077
  -5.500  -0.4418   0.03221   0.02165  -0.0608   0.9222   0.2211
  -5.250  -0.4111   0.03167   0.02106  -0.0618   0.9171   0.2376
  -5.000  -0.3867   0.03119   0.02053  -0.0617   0.9106   0.2539
  -4.750  -0.3609   0.03076   0.02010  -0.0618   0.9041   0.2730
  -4.500  -0.3277   0.03034   0.01964  -0.0632   0.8995   0.2983
  -4.250  -0.3083   0.03005   0.01943  -0.0621   0.8916   0.3203
  -4.000  -0.2786   0.02978   0.01921  -0.0628   0.8860   0.3518
  -3.750  -0.2525   0.02963   0.01909  -0.0627   0.8799   0.3839
  -3.500  -0.2300   0.02955   0.01903  -0.0619   0.8726   0.4162
  -3.250  -0.1982   0.02948   0.01898  -0.0626   0.8678   0.4528
  -3.000  -0.1812   0.02955   0.01905  -0.0609   0.8595   0.4824
  -2.750  -0.1527   0.02955   0.01903  -0.0609   0.8539   0.5159
  -2.500  -0.1301   0.02962   0.01908  -0.0600   0.8471   0.5463
  -2.250  -0.1074   0.02970   0.01916  -0.0590   0.8402   0.5749
  -2.000  -0.0752   0.02966   0.01911  -0.0595   0.8359   0.6055
  -1.750  -0.0612   0.02984   0.01930  -0.0571   0.8269   0.6303
  -1.500  -0.0324   0.02984   0.01931  -0.0570   0.8218   0.6582
  -1.250  -0.0133   0.02999   0.01948  -0.0554   0.8145   0.6836
  -1.000   0.0103   0.03005   0.01955  -0.0544   0.8080   0.7115
  -0.750   0.0422   0.02998   0.01951  -0.0546   0.8041   0.7413
  -0.500   0.0537   0.03026   0.01983  -0.0519   0.7947   0.7687
  -0.250   0.0847   0.03019   0.01979  -0.0521   0.7900   0.8016
   0.000   0.1071   0.03038   0.02004  -0.0512   0.7827   0.8360
   0.250   0.1451   0.03051   0.02021  -0.0532   0.7770   0.8768
   0.500   0.2076   0.03057   0.02025  -0.0598   0.7738   0.9207
   0.750   0.2600   0.03094   0.02059  -0.0658   0.7670   0.9811
   1.000   0.2873   0.03114   0.02063  -0.0669   0.7604   1.0000
   1.250   0.3216   0.03105   0.02039  -0.0683   0.7564   1.0000
   1.500   0.3256   0.03173   0.02095  -0.0654   0.7452   1.0000
   1.750   0.3612   0.03167   0.02078  -0.0668   0.7411   1.0000
   2.000   0.3691   0.03237   0.02140  -0.0644   0.7300   1.0000
   2.250   0.4054   0.03224   0.02120  -0.0656   0.7256   1.0000
   2.500   0.4158   0.03291   0.02181  -0.0634   0.7143   1.0000
   2.750   0.4536   0.03264   0.02149  -0.0647   0.7098   1.0000
   3.000   0.4645   0.03333   0.02214  -0.0625   0.6981   1.0000
   3.250   0.5028   0.03298   0.02177  -0.0637   0.6938   1.0000
   3.500   0.5122   0.03381   0.02258  -0.0614   0.6821   1.0000
   3.750   0.5504   0.03344   0.02221  -0.0625   0.6780   1.0000
   4.000   0.5586   0.03439   0.02318  -0.0602   0.6661   1.0000
   4.250   0.5964   0.03405   0.02286  -0.0612   0.6621   1.0000
   4.500   0.6040   0.03508   0.02390  -0.0588   0.6501   1.0000
   4.750   0.6426   0.03466   0.02354  -0.0598   0.6461   1.0000
   5.000   0.6489   0.03581   0.02473  -0.0574   0.6339   1.0000
   5.250   0.6881   0.03536   0.02435  -0.0584   0.6301   1.0000
   5.500   0.6939   0.03656   0.02560  -0.0560   0.6175   1.0000
   5.750   0.7337   0.03604   0.02516  -0.0569   0.6137   1.0000
   6.000   0.7386   0.03734   0.02653  -0.0545   0.6010   1.0000
   6.500   0.7829   0.03818   0.02756  -0.0529   0.5843   1.0000
   6.750   0.7908   0.03948   0.02894  -0.0510   0.5726   1.0000
   7.000   0.8271   0.03904   0.02866  -0.0514   0.5675   1.0000
   7.250   0.8309   0.04063   0.03034  -0.0492   0.5551   1.0000
   7.500   0.8701   0.04003   0.02989  -0.0497   0.5508   1.0000
   7.750   0.8702   0.04191   0.03187  -0.0473   0.5378   1.0000
   8.000   0.9131   0.04100   0.03116  -0.0480   0.5338   1.0000
   8.250   0.9132   0.04280   0.03306  -0.0455   0.5204   1.0000
   8.500   0.9192   0.04417   0.03455  -0.0435   0.5075   1.0000
   8.750   0.9413   0.04413   0.03466  -0.0422   0.4962   1.0000
   9.000   0.9910   0.04172   0.03246  -0.0422   0.4864   1.0000
   9.250   1.0097   0.04140   0.03224  -0.0402   0.4701   1.0000
   9.500   1.0084   0.04255   0.03349  -0.0371   0.4508   1.0000
   9.750   1.0207   0.04213   0.03309  -0.0342   0.4260   1.0000
  10.000   1.0227   0.04293   0.03394  -0.0314   0.4003   1.0000
  10.250   1.0300   0.04341   0.03438  -0.0289   0.3717   1.0000
  10.500   1.0385   0.04410   0.03502  -0.0267   0.3441   1.0000
  10.750   1.0410   0.04558   0.03649  -0.0247   0.3167   1.0000
  11.000   1.0404   0.04747   0.03836  -0.0228   0.2861   1.0000
  11.250   1.0367   0.04981   0.04066  -0.0211   0.2489   1.0000
  11.500   1.0311   0.05243   0.04304  -0.0195   0.2043   1.0000
  11.750   1.0217   0.05559   0.04582  -0.0180   0.1726   1.0000
  12.000   1.0119   0.05912   0.04908  -0.0170   0.1516   1.0000
  12.250   1.0053   0.06256   0.05234  -0.0162   0.1354   1.0000
  12.500   1.0016   0.06581   0.05555  -0.0156   0.1225   1.0000
  12.750   1.0016   0.06875   0.05848  -0.0151   0.1122   1.0000
  13.000   1.0029   0.07154   0.06124  -0.0146   0.1048   1.0000
  13.250   1.0076   0.07399   0.06372  -0.0140   0.0986   1.0000
  13.500   1.0140   0.07623   0.06594  -0.0134   0.0938   1.0000
  13.750   1.0224   0.07837   0.06821  -0.0129   0.0884   1.0000
  14.000   1.0312   0.08035   0.07018  -0.0123   0.0841   1.0000
  14.250   1.0443   0.08205   0.07201  -0.0115   0.0803   1.0000
  14.500   1.0575   0.08388   0.07405  -0.0108   0.0769   1.0000
  14.750   1.0699   0.08574   0.07600  -0.0103   0.0736   1.0000
  15.000   1.0878   0.08702   0.07726  -0.0094   0.0701   1.0000
  15.250   1.0913   0.09035   0.08093  -0.0096   0.0680   1.0000
  15.500   1.0934   0.09387   0.08474  -0.0099   0.0661   1.0000
  15.750   1.0926   0.09771   0.08884  -0.0105   0.0643   1.0000
  16.000   1.0917   0.10152   0.09282  -0.0113   0.0626   1.0000
  16.250   1.0962   0.10453   0.09590  -0.0117   0.0607   1.0000
  16.500   1.0940   0.10873   0.10022  -0.0128   0.0595   1.0000
  16.750   1.0751   0.11553   0.10732  -0.0157   0.0591   1.0000
  17.000   1.0546   0.12301   0.11507  -0.0194   0.0589   1.0000
  17.250   1.0296   0.13188   0.12417  -0.0242   0.0589   1.0000
  17.500   1.0006   0.14244   0.13493  -0.0305   0.0591   1.0000
  17.750   0.9702   0.15462   0.14721  -0.0378   0.0594   1.0000
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