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GOE 480 AIRFOIL (goe480-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 480 AIRFOIL (goe480-il)
Reynolds number: 500,000
Max Cl/Cd: 112.5 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe480-il-500000.txt
Download as CSV file: xf-goe480-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.2756   0.12345   0.12096  -0.0405   1.0000   0.0358
 -11.500  -0.2724   0.12077   0.11830  -0.0409   1.0000   0.0369
 -11.250  -0.2983   0.11569   0.11325  -0.0460   1.0000   0.0384
 -11.000  -0.2925   0.11261   0.11019  -0.0448   1.0000   0.0386
 -10.750  -0.2835   0.11057   0.10818  -0.0432   1.0000   0.0388
 -10.500  -0.2801   0.10877   0.10642  -0.0417   1.0000   0.0391
 -10.250  -0.2665   0.10622   0.10387  -0.0431   0.9991   0.0395
 -10.000  -0.2469   0.10277   0.10041  -0.0470   0.9967   0.0403
  -9.750  -0.2294   0.09900   0.09664  -0.0514   0.9923   0.0419
  -9.500  -0.2355   0.08999   0.08761  -0.0647   0.9838   0.0439
  -9.250  -0.2147   0.08733   0.08494  -0.0657   0.9780   0.0443
  -9.000  -0.1924   0.08478   0.08239  -0.0676   0.9716   0.0447
  -8.750  -0.1706   0.08189   0.07949  -0.0708   0.9633   0.0452
  -8.500  -0.1447   0.07862   0.07620  -0.0760   0.9562   0.0465
  -8.250  -0.1333   0.06598   0.06345  -0.1019   0.9301   0.0501
  -8.000  -0.1070   0.06374   0.06116  -0.1033   0.9170   0.0505
  -7.750  -0.0835   0.06186   0.05919  -0.1051   0.8989   0.0510
  -7.500  -0.0673   0.05996   0.05720  -0.1064   0.8790   0.0516
  -7.250  -0.0571   0.05777   0.05490  -0.1077   0.8604   0.0524
  -7.000  -0.0840   0.04383   0.04044  -0.1222   0.8365   0.0574
  -6.750  -0.0678   0.04242   0.03904  -0.1214   0.8263   0.0578
  -6.500  -0.0503   0.04148   0.03805  -0.1207   0.8174   0.0582
  -6.250  -0.0327   0.04033   0.03685  -0.1202   0.8084   0.0587
  -6.000  -0.0148   0.03896   0.03540  -0.1201   0.8007   0.0594
  -5.750   0.0030   0.03713   0.03346  -0.1203   0.7926   0.0605
  -5.500   0.0085   0.02962   0.02522  -0.1222   0.7855   0.0665
  -5.250   0.0305   0.02858   0.02421  -0.1218   0.7786   0.0672
  -5.000   0.0531   0.02774   0.02331  -0.1215   0.7721   0.0680
  -4.750   0.0757   0.02680   0.02231  -0.1211   0.7660   0.0692
  -4.500   0.0978   0.02540   0.02075  -0.1207   0.7594   0.0716
  -4.250   0.1166   0.02279   0.01765  -0.1201   0.7536   0.0771
  -4.000   0.1407   0.02190   0.01675  -0.1198   0.7477   0.0782
  -3.750   0.1600   0.01729   0.01130  -0.1180   0.7419   0.0635
  -3.500   0.1845   0.01596   0.00972  -0.1173   0.7362   0.0623
  -3.250   0.2099   0.01500   0.00858  -0.1168   0.7305   0.0617
  -3.000   0.2357   0.01427   0.00772  -0.1162   0.7242   0.0617
  -2.750   0.2622   0.01371   0.00700  -0.1158   0.7185   0.0619
  -2.500   0.2886   0.01328   0.00651  -0.1153   0.7125   0.0626
  -2.250   0.3151   0.01287   0.00603  -0.1149   0.7060   0.0632
  -2.000   0.3420   0.01251   0.00555  -0.1145   0.7001   0.0636
  -1.750   0.3684   0.01214   0.00515  -0.1140   0.6937   0.0640
  -1.500   0.3950   0.01184   0.00480  -0.1135   0.6869   0.0644
  -1.250   0.4218   0.01160   0.00451  -0.1131   0.6807   0.0649
  -1.000   0.4483   0.01138   0.00428  -0.1126   0.6734   0.0653
  -0.750   0.4741   0.01096   0.00381  -0.1121   0.6667   0.0662
  -0.500   0.4998   0.01062   0.00350  -0.1115   0.6594   0.0677
  -0.250   0.5259   0.01043   0.00330  -0.1110   0.6518   0.0690
   0.000   0.5520   0.01028   0.00315  -0.1105   0.6444   0.0701
   0.250   0.5781   0.01015   0.00301  -0.1099   0.6361   0.0713
   0.500   0.6042   0.01005   0.00290  -0.1094   0.6281   0.0728
   0.750   0.6302   0.00997   0.00280  -0.1089   0.6192   0.0742
   1.000   0.6561   0.00991   0.00272  -0.1083   0.6106   0.0758
   1.250   0.6817   0.00981   0.00261  -0.1077   0.6012   0.0796
   1.500   0.7075   0.00978   0.00258  -0.1071   0.5917   0.0838
   1.750   0.7329   0.00977   0.00254  -0.1065   0.5822   0.0912
   2.000   0.7577   0.00958   0.00262  -0.1058   0.5724   0.1765
   2.250   0.7797   0.00916   0.00274  -0.1048   0.5634   0.3999
   2.500   0.8472   0.00806   0.00296  -0.1136   0.5517   1.0000
   2.750   0.8714   0.00819   0.00303  -0.1128   0.5426   1.0000
   3.000   0.8950   0.00835   0.00311  -0.1118   0.5333   1.0000
   3.250   0.9192   0.00847   0.00320  -0.1109   0.5244   1.0000
   3.500   0.9426   0.00866   0.00330  -0.1099   0.5157   1.0000
   3.750   0.9668   0.00878   0.00341  -0.1091   0.5067   1.0000
   4.000   0.9899   0.00898   0.00353  -0.1080   0.4979   1.0000
   4.250   1.0140   0.00911   0.00366  -0.1072   0.4889   1.0000
   4.500   1.0371   0.00931   0.00380  -0.1062   0.4806   1.0000
   4.750   1.0609   0.00946   0.00394  -0.1053   0.4716   1.0000
   5.000   1.0838   0.00967   0.00410  -0.1043   0.4629   1.0000
   5.250   1.1069   0.00984   0.00426  -0.1033   0.4532   1.0000
   5.500   1.1295   0.01004   0.00443  -0.1022   0.4435   1.0000
   5.750   1.1510   0.01028   0.00461  -0.1010   0.4327   1.0000
   6.000   1.1739   0.01046   0.00480  -0.1000   0.4227   1.0000
   6.250   1.1953   0.01070   0.00500  -0.0987   0.4121   1.0000
   6.500   1.2161   0.01095   0.00521  -0.0974   0.4009   1.0000
   6.750   1.2378   0.01117   0.00544  -0.0962   0.3903   1.0000
   7.000   1.2581   0.01145   0.00568  -0.0948   0.3805   1.0000
   7.250   1.2775   0.01174   0.00594  -0.0933   0.3683   1.0000
   7.500   1.2965   0.01203   0.00620  -0.0916   0.3545   1.0000
   7.750   1.3147   0.01235   0.00649  -0.0899   0.3412   1.0000
   8.000   1.3315   0.01269   0.00679  -0.0879   0.3291   1.0000
   8.250   1.3458   0.01306   0.00712  -0.0855   0.3170   1.0000
   8.500   1.3602   0.01345   0.00748  -0.0831   0.3042   1.0000
   8.750   1.3753   0.01383   0.00784  -0.0809   0.2918   1.0000
   9.000   1.3891   0.01428   0.00825  -0.0785   0.2790   1.0000
   9.250   1.4022   0.01477   0.00871  -0.0762   0.2660   1.0000
   9.500   1.4146   0.01532   0.00922  -0.0738   0.2535   1.0000
   9.750   1.4267   0.01592   0.00978  -0.0714   0.2407   1.0000
  10.000   1.4391   0.01652   0.01036  -0.0692   0.2276   1.0000
  10.250   1.4498   0.01724   0.01103  -0.0669   0.2132   1.0000
  10.500   1.4581   0.01811   0.01184  -0.0643   0.1964   1.0000
  10.750   1.4648   0.01912   0.01277  -0.0617   0.1757   1.0000
  11.000   1.4651   0.02058   0.01406  -0.0586   0.1459   1.0000
  11.250   1.4570   0.02268   0.01591  -0.0550   0.1082   1.0000
  11.500   1.4517   0.02478   0.01785  -0.0520   0.0852   1.0000
  11.750   1.4520   0.02660   0.01964  -0.0498   0.0742   1.0000
  12.000   1.4545   0.02836   0.02139  -0.0479   0.0675   1.0000
  12.250   1.4575   0.03015   0.02320  -0.0462   0.0624   1.0000
  12.500   1.4607   0.03198   0.02507  -0.0447   0.0584   1.0000
  12.750   1.4645   0.03383   0.02696  -0.0434   0.0548   1.0000
  13.000   1.4625   0.03624   0.02940  -0.0420   0.0516   1.0000
  13.250   1.4691   0.03794   0.03118  -0.0410   0.0491   1.0000
  13.500   1.4707   0.04016   0.03344  -0.0400   0.0467   1.0000
  13.750   1.4660   0.04308   0.03640  -0.0389   0.0446   1.0000
  14.000   1.4716   0.04504   0.03846  -0.0383   0.0427   1.0000
  14.250   1.4739   0.04740   0.04089  -0.0377   0.0410   1.0000
  14.500   1.4719   0.05029   0.04381  -0.0371   0.0393   1.0000
  14.750   1.4661   0.05368   0.04727  -0.0367   0.0380   1.0000
  15.000   1.4685   0.05625   0.04993  -0.0364   0.0368   1.0000
  15.250   1.4686   0.05913   0.05290  -0.0363   0.0357   1.0000
  15.500   1.4680   0.06217   0.05601  -0.0363   0.0346   1.0000
  15.750   1.4625   0.06587   0.05976  -0.0364   0.0336   1.0000
  16.000   1.4529   0.07016   0.06413  -0.0367   0.0328   1.0000
  16.250   1.4538   0.07320   0.06726  -0.0369   0.0320   1.0000
  16.500   1.4522   0.07660   0.07075  -0.0373   0.0311   1.0000
  16.750   1.4501   0.08011   0.07434  -0.0378   0.0303   1.0000
  17.000   1.4468   0.08382   0.07813  -0.0384   0.0297   1.0000
  17.250   1.4419   0.08781   0.08218  -0.0392   0.0291   1.0000
  17.500   1.4348   0.09213   0.08655  -0.0401   0.0285   1.0000
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