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GOE 404 AIRFOIL (goe404-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 404 AIRFOIL (goe404-il)
Reynolds number: 500,000
Max Cl/Cd: 94.19 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe404-il-500000-n5.txt
Download as CSV file: xf-goe404-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 404 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
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.7035   0.03331   0.02950  -0.0939   0.9745   0.0270
 -11.250  -0.6874   0.02979   0.02564  -0.0963   0.9666   0.0271
 -11.000  -0.6688   0.02760   0.02319  -0.0970   0.9578   0.0272
 -10.750  -0.6478   0.02590   0.02127  -0.0974   0.9499   0.0273
 -10.500  -0.6282   0.02432   0.01950  -0.0972   0.9407   0.0275
 -10.250  -0.6072   0.02305   0.01810  -0.0968   0.9322   0.0277
 -10.000  -0.5852   0.02202   0.01695  -0.0963   0.9232   0.0279
  -9.750  -0.5624   0.02112   0.01594  -0.0958   0.9149   0.0280
  -9.500  -0.5393   0.02031   0.01503  -0.0952   0.9046   0.0282
  -9.250  -0.5159   0.01957   0.01417  -0.0945   0.8927   0.0284
  -9.000  -0.4923   0.01888   0.01335  -0.0938   0.8784   0.0286
  -8.750  -0.4683   0.01823   0.01257  -0.0931   0.8620   0.0288
  -8.500  -0.4440   0.01762   0.01182  -0.0924   0.8429   0.0291
  -8.250  -0.4195   0.01707   0.01110  -0.0917   0.8177   0.0293
  -8.000  -0.3950   0.01659   0.01043  -0.0910   0.7894   0.0296
  -7.750  -0.3699   0.01615   0.00981  -0.0903   0.7647   0.0299
  -7.500  -0.3443   0.01574   0.00923  -0.0897   0.7448   0.0303
  -7.250  -0.3183   0.01537   0.00869  -0.0893   0.7285   0.0306
  -7.000  -0.2920   0.01500   0.00819  -0.0888   0.7141   0.0309
  -6.750  -0.2653   0.01464   0.00771  -0.0884   0.7020   0.0311
  -6.500  -0.2392   0.01421   0.00720  -0.0880   0.6908   0.0315
  -6.250  -0.2122   0.01385   0.00678  -0.0877   0.6803   0.0318
  -6.000  -0.1853   0.01355   0.00640  -0.0873   0.6711   0.0322
  -5.750  -0.1578   0.01325   0.00605  -0.0871   0.6618   0.0327
  -5.250  -0.1029   0.01275   0.00541  -0.0865   0.6433   0.0336
  -5.000  -0.0754   0.01253   0.00512  -0.0862   0.6343   0.0342
  -4.750  -0.0476   0.01231   0.00484  -0.0859   0.6264   0.0348
  -4.500  -0.0199   0.01209   0.00457  -0.0856   0.6174   0.0354
  -4.250   0.0077   0.01188   0.00433  -0.0854   0.6085   0.0363
  -4.000   0.0355   0.01170   0.00410  -0.0851   0.5981   0.0374
  -3.750   0.0633   0.01155   0.00389  -0.0848   0.5883   0.0387
  -3.500   0.0910   0.01139   0.00369  -0.0845   0.5778   0.0404
  -3.250   0.1187   0.01123   0.00351  -0.0843   0.5676   0.0429
  -3.000   0.1463   0.01111   0.00336  -0.0840   0.5560   0.0465
  -2.750   0.1741   0.01101   0.00326  -0.0837   0.5431   0.0525
  -2.500   0.2018   0.01097   0.00320  -0.0835   0.5288   0.0595
  -2.250   0.2295   0.01099   0.00316  -0.0832   0.5127   0.0649
  -2.000   0.2571   0.01103   0.00313  -0.0829   0.4963   0.0690
  -1.750   0.2846   0.01108   0.00309  -0.0826   0.4811   0.0727
  -1.500   0.3123   0.01112   0.00309  -0.0823   0.4672   0.0757
  -1.250   0.3400   0.01117   0.00309  -0.0821   0.4554   0.0787
  -1.000   0.3675   0.01124   0.00306  -0.0818   0.4448   0.0811
  -0.750   0.3952   0.01123   0.00305  -0.0816   0.4355   0.0836
  -0.500   0.4227   0.01130   0.00308  -0.0813   0.4269   0.0863
  -0.250   0.4506   0.01133   0.00308  -0.0811   0.4192   0.0891
   0.000   0.4780   0.01139   0.00309  -0.0809   0.4109   0.0916
   0.250   0.5055   0.01139   0.00309  -0.0807   0.4034   0.0945
   0.500   0.5331   0.01143   0.00311  -0.0804   0.3960   0.0970
   0.750   0.5604   0.01149   0.00313  -0.0802   0.3896   0.0992
   1.000   0.5883   0.01151   0.00313  -0.0800   0.3837   0.1010
   1.250   0.6157   0.01152   0.00314  -0.0797   0.3772   0.1036
   1.500   0.6428   0.01158   0.00318  -0.0795   0.3717   0.1062
   1.750   0.6707   0.01160   0.00321  -0.0793   0.3674   0.1090
   2.000   0.6983   0.01165   0.00325  -0.0791   0.3622   0.1120
   2.250   0.7256   0.01171   0.00330  -0.0789   0.3570   0.1162
   2.500   0.7528   0.01178   0.00338  -0.0786   0.3526   0.1224
   2.750   0.7804   0.01181   0.00345  -0.0785   0.3486   0.1310
   3.000   0.8078   0.01184   0.00354  -0.0783   0.3443   0.1487
   3.250   0.8347   0.01187   0.00366  -0.0780   0.3397   0.1917
   3.500   0.8591   0.01130   0.00384  -0.0778   0.3348   0.5156
   4.000   0.9237   0.01055   0.00418  -0.0793   0.3258   1.0000
   4.250   0.9497   0.01072   0.00430  -0.0789   0.3218   1.0000
   4.500   0.9753   0.01091   0.00445  -0.0784   0.3178   1.0000
   4.750   1.0019   0.01104   0.00457  -0.0780   0.3141   1.0000
   5.000   1.0279   0.01121   0.00471  -0.0776   0.3076   1.0000
   5.250   1.0529   0.01145   0.00487  -0.0771   0.3001   1.0000
   5.500   1.0790   0.01160   0.00502  -0.0767   0.2939   1.0000
   5.750   1.1043   0.01182   0.00519  -0.0762   0.2868   1.0000
   6.000   1.1296   0.01203   0.00538  -0.0757   0.2800   1.0000
   6.250   1.1546   0.01226   0.00557  -0.0752   0.2716   1.0000
   6.500   1.1793   0.01252   0.00578  -0.0747   0.2624   1.0000
   6.750   1.2031   0.01282   0.00602  -0.0740   0.2504   1.0000
   7.000   1.2260   0.01319   0.00630  -0.0733   0.2335   1.0000
   7.250   1.2458   0.01377   0.00671  -0.0721   0.2055   1.0000
   7.500   1.2642   0.01445   0.00722  -0.0708   0.1819   1.0000
   7.750   1.2850   0.01494   0.00764  -0.0698   0.1719   1.0000
   8.000   1.3057   0.01541   0.00807  -0.0687   0.1652   1.0000
   8.250   1.3272   0.01580   0.00846  -0.0678   0.1608   1.0000
   8.500   1.3477   0.01623   0.00888  -0.0667   0.1568   1.0000
   8.750   1.3673   0.01670   0.00933  -0.0656   0.1531   1.0000
   9.000   1.3870   0.01708   0.00974  -0.0644   0.1506   1.0000
   9.250   1.4059   0.01747   0.01015  -0.0631   0.1482   1.0000
   9.500   1.4239   0.01792   0.01062  -0.0617   0.1455   1.0000
   9.750   1.4409   0.01843   0.01114  -0.0602   0.1428   1.0000
  10.000   1.4565   0.01903   0.01175  -0.0586   0.1398   1.0000
  10.250   1.4730   0.01959   0.01233  -0.0572   0.1372   1.0000
  10.500   1.4905   0.02011   0.01289  -0.0560   0.1350   1.0000
  10.750   1.5069   0.02070   0.01352  -0.0548   0.1326   1.0000
  11.000   1.5223   0.02138   0.01423  -0.0535   0.1302   1.0000
  11.250   1.5364   0.02215   0.01503  -0.0521   0.1279   1.0000
  11.500   1.5493   0.02303   0.01594  -0.0507   0.1256   1.0000
  11.750   1.5642   0.02381   0.01677  -0.0496   0.1238   1.0000
  12.000   1.5786   0.02464   0.01765  -0.0485   0.1216   1.0000
  12.250   1.5915   0.02561   0.01867  -0.0474   0.1185   1.0000
  12.500   1.6025   0.02676   0.01984  -0.0463   0.1154   1.0000
  12.750   1.6123   0.02805   0.02117  -0.0453   0.1127   1.0000
  13.000   1.6239   0.02925   0.02242  -0.0444   0.1096   1.0000
  13.250   1.6331   0.03069   0.02391  -0.0435   0.1057   1.0000
  13.500   1.6396   0.03244   0.02568  -0.0427   0.1019   1.0000
  13.750   1.6472   0.03414   0.02744  -0.0421   0.0973   1.0000
  14.000   1.6503   0.03635   0.02967  -0.0414   0.0917   1.0000
  14.250   1.6516   0.03878   0.03212  -0.0409   0.0846   1.0000
  14.500   1.6485   0.04173   0.03508  -0.0404   0.0770   1.0000
  14.750   1.6433   0.04498   0.03835  -0.0400   0.0718   1.0000
  15.000   1.6370   0.04843   0.04185  -0.0398   0.0681   1.0000
  15.250   1.6316   0.05188   0.04536  -0.0398   0.0659   1.0000
  15.500   1.6260   0.05545   0.04900  -0.0399   0.0642   1.0000
  15.750   1.6186   0.05930   0.05292  -0.0401   0.0626   1.0000
  16.000   1.6099   0.06342   0.05712  -0.0405   0.0613   1.0000
  16.250   1.6011   0.06765   0.06144  -0.0410   0.0601   1.0000
  16.500   1.5947   0.07163   0.06552  -0.0416   0.0593   1.0000
  16.750   1.5873   0.07580   0.06979  -0.0423   0.0585   1.0000
  17.000   1.5795   0.08010   0.07417  -0.0430   0.0578   1.0000
  17.250   1.5711   0.08448   0.07865  -0.0439   0.0572   1.0000
  17.500   1.5622   0.08897   0.08322  -0.0449   0.0565   1.0000
  17.750   1.5529   0.09358   0.08791  -0.0459   0.0558   1.0000
  18.000   1.5435   0.09823   0.09265  -0.0471   0.0552   1.0000
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