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GOE 624 AIRFOIL (goe624-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 624 AIRFOIL (goe624-il)
Reynolds number: 200,000
Max Cl/Cd: 69.85 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe624-il-200000-n5.txt
Download as CSV file: xf-goe624-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 624 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.4982   0.04859   0.04420  -0.1040   0.9248   0.0358
 -11.000  -0.5397   0.04148   0.03655  -0.1071   0.9050   0.0358
 -10.750  -0.5531   0.03710   0.03160  -0.1069   0.8920   0.0361
 -10.500  -0.5457   0.03483   0.02905  -0.1062   0.8827   0.0364
 -10.250  -0.5312   0.03333   0.02741  -0.1055   0.8740   0.0367
 -10.000  -0.5157   0.03184   0.02575  -0.1048   0.8661   0.0371
  -9.750  -0.4988   0.03042   0.02414  -0.1041   0.8579   0.0374
  -9.250  -0.4613   0.02777   0.02108  -0.1029   0.8434   0.0382
  -9.000  -0.4410   0.02655   0.01964  -0.1022   0.8362   0.0387
  -8.750  -0.4196   0.02541   0.01827  -0.1016   0.8293   0.0392
  -8.500  -0.3973   0.02435   0.01700  -0.1011   0.8218   0.0398
  -8.250  -0.3743   0.02339   0.01580  -0.1005   0.8156   0.0405
  -8.000  -0.3503   0.02252   0.01475  -0.1001   0.8085   0.0412
  -7.750  -0.3260   0.02182   0.01402  -0.0997   0.8011   0.0418
  -7.500  -0.3012   0.02119   0.01330  -0.0993   0.7940   0.0425
  -7.250  -0.2762   0.02056   0.01258  -0.0989   0.7845   0.0432
  -7.000  -0.2511   0.01994   0.01182  -0.0984   0.7758   0.0440
  -6.750  -0.2256   0.01934   0.01111  -0.0980   0.7659   0.0449
  -6.500  -0.1997   0.01878   0.01040  -0.0976   0.7586   0.0458
  -6.250  -0.1736   0.01826   0.00983  -0.0974   0.7504   0.0468
  -6.000  -0.1472   0.01783   0.00935  -0.0971   0.7434   0.0480
  -5.750  -0.1204   0.01745   0.00891  -0.0969   0.7362   0.0497
  -5.500  -0.0935   0.01706   0.00843  -0.0967   0.7287   0.0518
  -5.250  -0.0667   0.01671   0.00804  -0.0965   0.7220   0.0539
  -5.000  -0.0395   0.01638   0.00769  -0.0963   0.7141   0.0566
  -4.750  -0.0123   0.01607   0.00731  -0.0961   0.7073   0.0599
  -4.500   0.0152   0.01580   0.00701  -0.0960   0.7003   0.0645
  -4.250   0.0427   0.01557   0.00675  -0.0959   0.6930   0.0700
  -4.000   0.0704   0.01537   0.00650  -0.0958   0.6863   0.0769
  -3.750   0.0981   0.01520   0.00629  -0.0957   0.6785   0.0842
  -3.500   0.1258   0.01505   0.00608  -0.0956   0.6717   0.0912
  -3.250   0.1536   0.01487   0.00589  -0.0956   0.6647   0.0973
  -3.000   0.1814   0.01474   0.00571  -0.0955   0.6577   0.1038
  -2.750   0.2090   0.01460   0.00552  -0.0954   0.6513   0.1103
  -2.500   0.2368   0.01448   0.00539  -0.0954   0.6435   0.1185
  -2.250   0.2643   0.01434   0.00525  -0.0953   0.6365   0.1292
  -2.000   0.2919   0.01421   0.00514  -0.0952   0.6291   0.1408
  -1.750   0.3195   0.01409   0.00502  -0.0952   0.6218   0.1528
  -1.500   0.3471   0.01398   0.00491  -0.0951   0.6153   0.1676
  -1.250   0.3746   0.01384   0.00485  -0.0951   0.6077   0.1896
  -1.000   0.4019   0.01372   0.00477  -0.0950   0.6005   0.2198
  -0.750   0.4291   0.01358   0.00474  -0.0949   0.5928   0.2571
  -0.500   0.4559   0.01342   0.00471  -0.0948   0.5848   0.3060
  -0.250   0.4823   0.01323   0.00470  -0.0947   0.5774   0.3732
   0.000   0.5079   0.01295   0.00473  -0.0943   0.5696   0.4670
   0.250   0.5318   0.01261   0.00478  -0.0935   0.5627   0.5952
   0.500   0.5531   0.01225   0.00492  -0.0918   0.5546   0.7451
   0.750   0.5797   0.01213   0.00502  -0.0907   0.5469   0.8780
   1.000   0.6222   0.01219   0.00508  -0.0934   0.5377   0.9555
   1.250   0.6725   0.01233   0.00509  -0.0982   0.5293   1.0000
   1.500   0.6966   0.01245   0.00514  -0.0975   0.5215   1.0000
   1.750   0.7207   0.01260   0.00518  -0.0968   0.5141   1.0000
   2.000   0.7452   0.01276   0.00526  -0.0962   0.5067   1.0000
   2.250   0.7698   0.01292   0.00534  -0.0957   0.4995   1.0000
   2.500   0.7945   0.01311   0.00542  -0.0951   0.4935   1.0000
   2.750   0.8196   0.01328   0.00555  -0.0947   0.4868   1.0000
   3.000   0.8444   0.01349   0.00567  -0.0942   0.4807   1.0000
   3.250   0.8695   0.01369   0.00581  -0.0938   0.4750   1.0000
   3.500   0.8947   0.01389   0.00598  -0.0934   0.4693   1.0000
   3.750   0.9197   0.01412   0.00613  -0.0929   0.4639   1.0000
   4.000   0.9448   0.01436   0.00631  -0.0925   0.4590   1.0000
   4.250   0.9700   0.01458   0.00652  -0.0922   0.4537   1.0000
   4.500   0.9949   0.01482   0.00672  -0.0918   0.4487   1.0000
   4.750   1.0197   0.01510   0.00692  -0.0914   0.4440   1.0000
   5.000   1.0443   0.01533   0.00717  -0.0910   0.4382   1.0000
   5.250   1.0680   0.01559   0.00740  -0.0904   0.4314   1.0000
   5.500   1.0914   0.01589   0.00763  -0.0898   0.4250   1.0000
   5.750   1.1149   0.01614   0.00791  -0.0892   0.4184   1.0000
   6.000   1.1384   0.01643   0.00817  -0.0886   0.4133   1.0000
   6.250   1.1621   0.01675   0.00844  -0.0881   0.4092   1.0000
   6.500   1.1858   0.01702   0.00877  -0.0876   0.4048   1.0000
   6.750   1.2089   0.01731   0.00910  -0.0870   0.4002   1.0000
   7.000   1.2315   0.01763   0.00942  -0.0863   0.3955   1.0000
   7.250   1.2539   0.01798   0.00973  -0.0856   0.3912   1.0000
   7.500   1.2755   0.01828   0.01012  -0.0848   0.3861   1.0000
   7.750   1.2965   0.01862   0.01050  -0.0839   0.3810   1.0000
   8.000   1.3170   0.01899   0.01085  -0.0830   0.3765   1.0000
   8.250   1.3373   0.01935   0.01126  -0.0820   0.3720   1.0000
   8.500   1.3555   0.01971   0.01170  -0.0806   0.3669   1.0000
   8.750   1.3724   0.02011   0.01214  -0.0791   0.3620   1.0000
   9.000   1.3894   0.02057   0.01257  -0.0777   0.3575   1.0000
   9.250   1.4057   0.02102   0.01314  -0.0762   0.3516   1.0000
   9.500   1.4204   0.02154   0.01370  -0.0745   0.3452   1.0000
   9.750   1.4347   0.02212   0.01431  -0.0729   0.3390   1.0000
  10.000   1.4483   0.02275   0.01501  -0.0713   0.3315   1.0000
  10.250   1.4605   0.02347   0.01573  -0.0696   0.3249   1.0000
  10.500   1.4738   0.02421   0.01656  -0.0682   0.3172   1.0000
  10.750   1.4843   0.02509   0.01745  -0.0665   0.3099   1.0000
  11.000   1.4964   0.02598   0.01842  -0.0652   0.3021   1.0000
  11.250   1.5055   0.02705   0.01950  -0.0636   0.2947   1.0000
  11.500   1.5159   0.02812   0.02064  -0.0622   0.2866   1.0000
  11.750   1.5222   0.02946   0.02197  -0.0606   0.2787   1.0000
  12.000   1.5304   0.03077   0.02335  -0.0593   0.2700   1.0000
  12.250   1.5353   0.03234   0.02491  -0.0578   0.2624   1.0000
  12.500   1.5422   0.03384   0.02649  -0.0566   0.2547   1.0000
  12.750   1.5453   0.03564   0.02829  -0.0552   0.2477   1.0000
  13.000   1.5507   0.03736   0.03007  -0.0541   0.2402   1.0000
  13.250   1.5523   0.03939   0.03211  -0.0529   0.2339   1.0000
  13.500   1.5575   0.04121   0.03402  -0.0519   0.2278   1.0000
  13.750   1.5600   0.04331   0.03616  -0.0509   0.2220   1.0000
  14.000   1.5624   0.04548   0.03837  -0.0501   0.2171   1.0000
  14.250   1.5661   0.04761   0.04058  -0.0494   0.2117   1.0000
  14.500   1.5665   0.05007   0.04308  -0.0486   0.2064   1.0000
  14.750   1.5680   0.05251   0.04559  -0.0481   0.2013   1.0000
  15.000   1.5688   0.05510   0.04826  -0.0476   0.1956   1.0000
  15.250   1.5662   0.05804   0.05121  -0.0471   0.1904   1.0000
  15.500   1.5668   0.06076   0.05403  -0.0468   0.1851   1.0000
  15.750   1.5649   0.06379   0.05712  -0.0466   0.1796   1.0000
  16.000   1.5609   0.06707   0.06041  -0.0464   0.1745   1.0000
  16.250   1.5596   0.07019   0.06366  -0.0465   0.1690   1.0000
  16.500   1.5548   0.07372   0.06724  -0.0466   0.1636   1.0000
  16.750   1.5511   0.07716   0.07075  -0.0467   0.1588   1.0000
  17.000   1.5478   0.08067   0.07436  -0.0470   0.1533   1.0000
  17.250   1.5412   0.08458   0.07830  -0.0474   0.1482   1.0000
  17.500   1.5373   0.08825   0.08209  -0.0479   0.1428   1.0000
  17.750   1.5303   0.09237   0.08627  -0.0486   0.1371   1.0000
  18.000   1.5241   0.09642   0.09039  -0.0493   0.1316   1.0000
  18.250   1.5169   0.10067   0.09472  -0.0502   0.1254   1.0000
  18.500   1.5090   0.10505   0.09915  -0.0512   0.1196   1.0000
  18.750   1.5003   0.10959   0.10375  -0.0524   0.1133   1.0000
  19.000   1.4919   0.11411   0.10831  -0.0536   0.1079   1.0000
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