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GOE 506 AIRFOIL (goe506-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 506 AIRFOIL (goe506-il)
Reynolds number: 500,000
Max Cl/Cd: 61.92 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe506-il-500000-n5.txt
Download as CSV file: xf-goe506-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 506 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.4759   0.09442   0.09165  -0.0939   0.9782   0.0106
 -15.750  -0.5312   0.07991   0.07687  -0.1031   0.9753   0.0104
 -15.500  -0.5535   0.07213   0.06894  -0.1086   0.9712   0.0104
 -15.250  -0.5740   0.06474   0.06138  -0.1141   0.9668   0.0105
 -15.000  -0.5806   0.05894   0.05544  -0.1195   0.9636   0.0107
 -14.750  -0.5893   0.05295   0.04929  -0.1251   0.9597   0.0108
 -14.500  -0.5959   0.04707   0.04324  -0.1309   0.9547   0.0108
 -14.250  -0.5926   0.04189   0.03789  -0.1374   0.9509   0.0109
 -14.000  -0.5798   0.03750   0.03330  -0.1441   0.9480   0.0112
 -13.750  -0.5692   0.03327   0.02885  -0.1505   0.9428   0.0114
 -13.500  -0.5527   0.03012   0.02554  -0.1560   0.9379   0.0117
 -13.250  -0.5318   0.02780   0.02309  -0.1606   0.9334   0.0120
 -13.000  -0.5175   0.02625   0.02143  -0.1621   0.9267   0.0123
 -12.750  -0.4986   0.02510   0.02017  -0.1636   0.9211   0.0126
 -12.500  -0.4853   0.02392   0.01887  -0.1637   0.9153   0.0129
 -12.250  -0.4773   0.02297   0.01782  -0.1622   0.9088   0.0131
 -12.000  -0.4652   0.02212   0.01684  -0.1611   0.9037   0.0135
 -11.750  -0.4575   0.02136   0.01597  -0.1588   0.8984   0.0139
 -11.500  -0.4517   0.02066   0.01516  -0.1558   0.8928   0.0142
 -11.250  -0.4421   0.01999   0.01435  -0.1533   0.8880   0.0146
 -11.000  -0.4344   0.01944   0.01375  -0.1503   0.8835   0.0149
 -10.750  -0.4252   0.01907   0.01334  -0.1473   0.8785   0.0153
 -10.500  -0.4093   0.01868   0.01290  -0.1455   0.8744   0.0156
 -10.250  -0.3898   0.01833   0.01248  -0.1444   0.8709   0.0162
 -10.000  -0.3740   0.01800   0.01209  -0.1424   0.8666   0.0168
  -9.750  -0.3586   0.01759   0.01160  -0.1404   0.8615   0.0174
  -9.500  -0.3402   0.01715   0.01104  -0.1389   0.8564   0.0181
  -9.250  -0.3238   0.01669   0.01052  -0.1371   0.8519   0.0186
  -9.000  -0.3068   0.01632   0.01013  -0.1352   0.8463   0.0191
  -8.750  -0.2862   0.01600   0.00975  -0.1341   0.8420   0.0197
  -8.500  -0.2644   0.01571   0.00939  -0.1331   0.8385   0.0206
  -8.250  -0.2455   0.01541   0.00905  -0.1315   0.8335   0.0215
  -8.000  -0.2245   0.01512   0.00868  -0.1303   0.8283   0.0223
  -7.750  -0.2039   0.01471   0.00818  -0.1291   0.8238   0.0230
  -7.500  -0.1861   0.01432   0.00777  -0.1273   0.8181   0.0237
  -7.250  -0.1653   0.01399   0.00740  -0.1260   0.8127   0.0245
  -7.000  -0.1430   0.01371   0.00707  -0.1250   0.8078   0.0256
  -6.750  -0.1224   0.01345   0.00676  -0.1236   0.8012   0.0265
  -6.500  -0.1000   0.01319   0.00641  -0.1225   0.7944   0.0274
  -6.250  -0.0784   0.01297   0.00614  -0.1213   0.7877   0.0280
  -6.000  -0.0588   0.01254   0.00564  -0.1198   0.7814   0.0293
  -5.750  -0.0368   0.01226   0.00532  -0.1187   0.7760   0.0304
  -5.500  -0.0147   0.01202   0.00503  -0.1175   0.7697   0.0314
  -5.250   0.0084   0.01181   0.00474  -0.1166   0.7637   0.0326
  -5.000   0.0311   0.01163   0.00451  -0.1155   0.7574   0.0336
  -4.750   0.0540   0.01147   0.00427  -0.1145   0.7496   0.0344
  -4.500   0.0764   0.01127   0.00402  -0.1134   0.7430   0.0357
  -4.250   0.0993   0.01108   0.00379  -0.1124   0.7369   0.0376
  -4.000   0.1224   0.01094   0.00359  -0.1114   0.7304   0.0397
  -3.750   0.1454   0.01082   0.00343  -0.1104   0.7236   0.0419
  -3.500   0.1679   0.01070   0.00327  -0.1092   0.7158   0.0472
  -3.250   0.1840   0.01019   0.00299  -0.1070   0.7048   0.1131
  -3.000   0.2025   0.00989   0.00291  -0.1052   0.6950   0.1856
  -2.750   0.2227   0.00986   0.00285  -0.1036   0.6815   0.2009
  -2.500   0.2418   0.00983   0.00280  -0.1017   0.6647   0.2124
  -2.250   0.2567   0.00986   0.00274  -0.0989   0.6371   0.2218
  -2.000   0.2412   0.01028   0.00276  -0.0897   0.5488   0.2250
  -1.750   0.2405   0.01062   0.00287  -0.0838   0.5076   0.2282
  -1.250   0.2652   0.01098   0.00302  -0.0776   0.4636   0.2392
  -1.000   0.2804   0.01115   0.00310  -0.0751   0.4445   0.2459
  -0.750   0.2957   0.01133   0.00320  -0.0726   0.4235   0.2537
  -0.500   0.3114   0.01149   0.00330  -0.0703   0.4046   0.2647
  -0.250   0.3267   0.01166   0.00342  -0.0679   0.3859   0.2756
   0.000   0.3430   0.01183   0.00353  -0.0657   0.3705   0.2886
   0.250   0.3605   0.01197   0.00364  -0.0638   0.3600   0.3024
   0.750   0.3958   0.01218   0.00390  -0.0601   0.3418   0.3500
   1.000   0.4133   0.01232   0.00404  -0.0582   0.3340   0.3708
   1.250   0.4324   0.01240   0.00417  -0.0567   0.3293   0.3946
   1.500   0.4518   0.01248   0.00429  -0.0552   0.3249   0.4194
   1.750   0.4702   0.01256   0.00444  -0.0535   0.3206   0.4510
   2.000   0.4880   0.01261   0.00460  -0.0517   0.3172   0.4914
   2.250   0.5047   0.01261   0.00478  -0.0497   0.3144   0.5547
   2.500   0.5208   0.01254   0.00495  -0.0476   0.3117   0.6314
   3.000   0.7028   0.01249   0.00572  -0.0756   0.3011   0.9705
   3.250   0.7356   0.01280   0.00599  -0.0771   0.2979   0.9915
   3.750   0.7816   0.01329   0.00643  -0.0758   0.2933   1.0000
   4.000   0.7996   0.01348   0.00661  -0.0742   0.2909   1.0000
   4.250   0.8178   0.01370   0.00681  -0.0726   0.2888   1.0000
   4.500   0.8358   0.01394   0.00703  -0.0709   0.2864   1.0000
   4.750   0.8537   0.01420   0.00726  -0.0694   0.2839   1.0000
   5.000   0.8721   0.01446   0.00751  -0.0679   0.2816   1.0000
   5.250   0.8921   0.01467   0.00774  -0.0667   0.2797   1.0000
   5.500   0.9120   0.01490   0.00797  -0.0656   0.2775   1.0000
   5.750   0.9317   0.01515   0.00822  -0.0644   0.2745   1.0000
   6.000   0.9509   0.01544   0.00850  -0.0632   0.2714   1.0000
   6.250   0.9699   0.01574   0.00880  -0.0620   0.2689   1.0000
   6.500   0.9890   0.01605   0.00910  -0.0608   0.2662   1.0000
   6.750   1.0095   0.01631   0.00939  -0.0598   0.2630   1.0000
   7.000   1.0291   0.01662   0.00970  -0.0588   0.2587   1.0000
   7.250   1.0476   0.01698   0.01005  -0.0576   0.2536   1.0000
   7.500   1.0671   0.01732   0.01039  -0.0566   0.2474   1.0000
   7.750   1.0848   0.01775   0.01078  -0.0554   0.2372   1.0000
   8.000   1.1001   0.01830   0.01125  -0.0539   0.2165   1.0000
   8.250   1.1074   0.01933   0.01203  -0.0514   0.1807   1.0000
   8.500   1.1206   0.02006   0.01270  -0.0497   0.1713   1.0000
   8.750   1.1340   0.02080   0.01340  -0.0480   0.1641   1.0000
   9.000   1.1500   0.02139   0.01399  -0.0468   0.1604   1.0000
   9.250   1.1661   0.02198   0.01460  -0.0456   0.1573   1.0000
   9.500   1.1820   0.02260   0.01524  -0.0444   0.1547   1.0000
   9.750   1.1968   0.02330   0.01595  -0.0431   0.1516   1.0000
  10.000   1.2104   0.02408   0.01674  -0.0417   0.1481   1.0000
  10.250   1.2259   0.02475   0.01744  -0.0406   0.1454   1.0000
  10.500   1.2431   0.02532   0.01806  -0.0397   0.1434   1.0000
  10.750   1.2588   0.02600   0.01878  -0.0387   0.1401   1.0000
  11.000   1.2733   0.02677   0.01958  -0.0376   0.1367   1.0000
  11.250   1.2850   0.02774   0.02055  -0.0363   0.1319   1.0000
  11.500   1.3005   0.02847   0.02130  -0.0354   0.1242   1.0000
  11.750   1.2987   0.03042   0.02298  -0.0329   0.0833   1.0000
  12.000   1.2960   0.03253   0.02503  -0.0305   0.0659   1.0000
  12.250   1.2775   0.03597   0.02831  -0.0271   0.0246   1.0000
  12.500   1.2807   0.03783   0.03021  -0.0256   0.0191   1.0000
  12.750   1.2847   0.03968   0.03211  -0.0243   0.0163   1.0000
  13.000   1.2910   0.04139   0.03390  -0.0233   0.0150   1.0000
  13.250   1.2972   0.04315   0.03573  -0.0223   0.0143   1.0000
  13.500   1.3001   0.04524   0.03789  -0.0213   0.0132   1.0000
  13.750   1.3024   0.04748   0.04021  -0.0204   0.0126   1.0000
  14.000   1.3041   0.04985   0.04268  -0.0196   0.0121   1.0000
  14.250   1.3068   0.05219   0.04510  -0.0190   0.0114   1.0000
  14.500   1.3076   0.05480   0.04781  -0.0185   0.0111   1.0000
  14.750   1.3067   0.05767   0.05078  -0.0182   0.0107   1.0000
  15.000   1.3046   0.06079   0.05400  -0.0180   0.0104   1.0000
  15.250   1.3006   0.06428   0.05759  -0.0180   0.0100   1.0000
  15.500   1.2938   0.06823   0.06165  -0.0182   0.0098   1.0000
  15.750   1.2853   0.07252   0.06605  -0.0186   0.0096   1.0000
  16.000   1.2755   0.07706   0.07072  -0.0192   0.0095   1.0000
  16.250   1.2650   0.08178   0.07556  -0.0200   0.0093   1.0000
  16.500   1.2559   0.08637   0.08027  -0.0208   0.0092   1.0000
  16.750   1.2471   0.09093   0.08494  -0.0217   0.0090   1.0000
  17.000   1.2360   0.09587   0.09000  -0.0228   0.0090   1.0000
  17.250   1.2277   0.10046   0.09469  -0.0239   0.0086   1.0000
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