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GOE 478 AIRFOIL (goe478-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 478 AIRFOIL (goe478-il)
Reynolds number: 200,000
Max Cl/Cd: 71.05 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe478-il-200000-n5.txt
Download as CSV file: xf-goe478-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 478 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.500  -0.2476   0.08709   0.08309  -0.0681   0.9628   0.0388
  -9.250  -0.2411   0.08184   0.07783  -0.0730   0.9546   0.0387
  -9.000  -0.2359   0.07602   0.07199  -0.0788   0.9451   0.0385
  -8.750  -0.2327   0.06896   0.06491  -0.0868   0.9348   0.0383
  -8.500  -0.3470   0.03411   0.02859  -0.1158   0.8966   0.0383
  -8.250  -0.3383   0.03051   0.02444  -0.1158   0.8866   0.0387
  -8.000  -0.3235   0.02810   0.02158  -0.1153   0.8776   0.0390
  -7.750  -0.3049   0.02620   0.01928  -0.1148   0.8702   0.0393
  -7.500  -0.2865   0.02474   0.01746  -0.1138   0.8614   0.0397
  -7.250  -0.2621   0.02351   0.01602  -0.1137   0.8547   0.0400
  -7.000  -0.2411   0.02267   0.01509  -0.1127   0.8462   0.0404
  -6.750  -0.2169   0.02185   0.01415  -0.1123   0.8393   0.0408
  -6.500  -0.1926   0.02112   0.01329  -0.1118   0.8333   0.0413
  -6.250  -0.1699   0.02045   0.01251  -0.1109   0.8271   0.0420
  -6.000  -0.1450   0.01981   0.01173  -0.1104   0.8212   0.0429
  -5.750  -0.1197   0.01918   0.01093  -0.1099   0.8158   0.0438
  -5.500  -0.0963   0.01861   0.01023  -0.1090   0.8095   0.0446
  -5.250  -0.0714   0.01801   0.00955  -0.1085   0.8045   0.0452
  -5.000  -0.0453   0.01747   0.00898  -0.1081   0.8001   0.0459
  -4.750  -0.0214   0.01702   0.00852  -0.1073   0.7945   0.0468
  -4.500   0.0030   0.01659   0.00805  -0.1066   0.7886   0.0477
  -4.250   0.0291   0.01619   0.00757  -0.1061   0.7835   0.0488
  -4.000   0.0546   0.01584   0.00714  -0.1054   0.7783   0.0502
  -3.750   0.0783   0.01547   0.00679  -0.1046   0.7726   0.0517
  -3.500   0.1037   0.01516   0.00647  -0.1040   0.7675   0.0537
  -3.250   0.1305   0.01487   0.00611  -0.1036   0.7632   0.0559
  -3.000   0.1546   0.01458   0.00584  -0.1028   0.7581   0.0580
  -2.750   0.1792   0.01433   0.00559  -0.1020   0.7526   0.0609
  -2.500   0.2052   0.01409   0.00533  -0.1014   0.7473   0.0647
  -2.250   0.2315   0.01388   0.00513  -0.1010   0.7422   0.0710
  -2.000   0.2555   0.01368   0.00504  -0.1001   0.7361   0.0809
  -1.750   0.2811   0.01353   0.00491  -0.0994   0.7303   0.0965
  -1.500   0.3084   0.01338   0.00474  -0.0991   0.7250   0.1124
  -1.250   0.3317   0.01322   0.00468  -0.0981   0.7179   0.1277
  -1.000   0.3567   0.01308   0.00462  -0.0974   0.7108   0.1463
  -0.750   0.3832   0.01298   0.00456  -0.0969   0.7045   0.1694
  -0.500   0.4068   0.01290   0.00457  -0.0959   0.6964   0.1917
  -0.250   0.4324   0.01280   0.00449  -0.0953   0.6889   0.2148
   0.000   0.4560   0.01268   0.00446  -0.0943   0.6799   0.2390
   0.250   0.4798   0.01250   0.00438  -0.0933   0.6703   0.2701
   0.500   0.5015   0.01225   0.00436  -0.0920   0.6595   0.3246
   0.750   0.5207   0.01177   0.00435  -0.0903   0.6490   0.4733
   1.000   0.5362   0.01121   0.00442  -0.0874   0.6362   0.6672
   1.250   0.6011   0.01086   0.00461  -0.0942   0.6190   0.9133
   1.500   0.6630   0.01097   0.00459  -0.1010   0.5987   0.9771
   1.750   0.7140   0.01111   0.00456  -0.1058   0.5796   1.0000
   2.000   0.7327   0.01125   0.00455  -0.1038   0.5648   1.0000
   2.250   0.7516   0.01143   0.00458  -0.1018   0.5517   1.0000
   2.500   0.7711   0.01162   0.00466  -0.1001   0.5404   1.0000
   2.750   0.7910   0.01184   0.00475  -0.0983   0.5310   1.0000
   3.000   0.8114   0.01204   0.00487  -0.0968   0.5218   1.0000
   3.250   0.8315   0.01229   0.00501  -0.0951   0.5122   1.0000
   3.500   0.8512   0.01252   0.00516  -0.0934   0.5013   1.0000
   3.750   0.8711   0.01278   0.00532  -0.0918   0.4913   1.0000
   4.000   0.8911   0.01300   0.00550  -0.0902   0.4819   1.0000
   4.250   0.9118   0.01325   0.00568  -0.0887   0.4744   1.0000
   4.500   0.9321   0.01345   0.00587  -0.0871   0.4662   1.0000
   4.750   0.9522   0.01371   0.00606  -0.0855   0.4587   1.0000
   5.000   0.9724   0.01390   0.00627  -0.0840   0.4507   1.0000
   5.250   0.9921   0.01413   0.00647  -0.0823   0.4428   1.0000
   5.500   1.0119   0.01437   0.00669  -0.0807   0.4352   1.0000
   5.750   1.0313   0.01458   0.00691  -0.0790   0.4271   1.0000
   6.000   1.0502   0.01485   0.00713  -0.0773   0.4196   1.0000
   6.250   1.0693   0.01505   0.00738  -0.0756   0.4112   1.0000
   6.500   1.0865   0.01533   0.00761  -0.0735   0.4026   1.0000
   6.750   1.1037   0.01556   0.00788  -0.0715   0.3918   1.0000
   7.000   1.1179   0.01584   0.00813  -0.0689   0.3806   1.0000
   7.250   1.1296   0.01615   0.00840  -0.0659   0.3677   1.0000
   7.500   1.1417   0.01647   0.00870  -0.0630   0.3527   1.0000
   7.750   1.1526   0.01687   0.00905  -0.0601   0.3359   1.0000
   8.000   1.1629   0.01733   0.00945  -0.0571   0.3172   1.0000
   8.250   1.1730   0.01786   0.00991  -0.0542   0.2978   1.0000
   8.500   1.1820   0.01848   0.01045  -0.0513   0.2783   1.0000
   8.750   1.1903   0.01919   0.01107  -0.0484   0.2600   1.0000
   9.000   1.1984   0.01997   0.01177  -0.0457   0.2433   1.0000
   9.250   1.2065   0.02081   0.01255  -0.0431   0.2279   1.0000
   9.500   1.2149   0.02169   0.01337  -0.0407   0.2144   1.0000
   9.750   1.2231   0.02263   0.01426  -0.0383   0.2022   1.0000
  10.000   1.2318   0.02358   0.01519  -0.0362   0.1913   1.0000
  10.250   1.2415   0.02453   0.01613  -0.0342   0.1812   1.0000
  10.500   1.2497   0.02560   0.01719  -0.0323   0.1724   1.0000
  10.750   1.2591   0.02664   0.01823  -0.0305   0.1636   1.0000
  11.000   1.2675   0.02778   0.01937  -0.0288   0.1559   1.0000
  11.250   1.2754   0.02899   0.02059  -0.0271   0.1479   1.0000
  11.500   1.2836   0.03023   0.02184  -0.0255   0.1409   1.0000
  11.750   1.2901   0.03161   0.02323  -0.0240   0.1336   1.0000
  12.000   1.2976   0.03298   0.02462  -0.0226   0.1272   1.0000
  12.250   1.3034   0.03450   0.02616  -0.0212   0.1209   1.0000
  12.500   1.3096   0.03604   0.02773  -0.0199   0.1156   1.0000
  12.750   1.3152   0.03767   0.02939  -0.0187   0.1102   1.0000
  13.000   1.3185   0.03953   0.03128  -0.0174   0.1059   1.0000
  13.250   1.3248   0.04119   0.03301  -0.0164   0.1014   1.0000
  13.500   1.3278   0.04319   0.03503  -0.0154   0.0973   1.0000
  13.750   1.3306   0.04526   0.03714  -0.0145   0.0940   1.0000
  14.000   1.3353   0.04722   0.03918  -0.0138   0.0905   1.0000
  14.250   1.3382   0.04941   0.04142  -0.0131   0.0879   1.0000
  14.500   1.3382   0.05195   0.04399  -0.0126   0.0853   1.0000
  14.750   1.3421   0.05415   0.04627  -0.0121   0.0832   1.0000
  15.000   1.3454   0.05647   0.04867  -0.0117   0.0811   1.0000
  15.250   1.3478   0.05896   0.05123  -0.0115   0.0793   1.0000
  15.500   1.3491   0.06161   0.05394  -0.0114   0.0777   1.0000
  15.750   1.3490   0.06447   0.05683  -0.0114   0.0762   1.0000
  16.000   1.3515   0.06708   0.05952  -0.0114   0.0747   1.0000
  16.250   1.3548   0.06962   0.06215  -0.0114   0.0733   1.0000
  16.500   1.3573   0.07231   0.06493  -0.0116   0.0718   1.0000
  16.750   1.3593   0.07506   0.06776  -0.0119   0.0706   1.0000
  17.000   1.3609   0.07789   0.07065  -0.0122   0.0695   1.0000
  17.250   1.3618   0.08081   0.07362  -0.0126   0.0684   1.0000
  17.500   1.3632   0.08363   0.07643  -0.0129   0.0673   1.0000
  17.750   1.3660   0.08638   0.07932  -0.0133   0.0663   1.0000
  18.000   1.3684   0.08920   0.08225  -0.0138   0.0653   1.0000
  18.250   1.3697   0.09220   0.08535  -0.0145   0.0641   1.0000
  18.500   1.3707   0.09527   0.08851  -0.0152   0.0629   1.0000
  18.750   1.3705   0.09853   0.09184  -0.0161   0.0617   1.0000
  19.000   1.3711   0.10164   0.09498  -0.0170   0.0605   1.0000
  19.250   1.3729   0.10452   0.09787  -0.0178   0.0595   1.0000
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