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GOE 384 AIRFOIL (goe384-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 384 AIRFOIL (goe384-il)
Reynolds number: 500,000
Max Cl/Cd: 87.06 at α=2°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe384-il-500000.txt
Download as CSV file: xf-goe384-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 384 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
  ------ -------- --------- --------- -------- -------- --------
  -9.750  -0.0081   0.08877   0.08487  -0.0884   0.6650   0.0496
  -9.500  -0.1930   0.04712   0.04296  -0.1241   0.6701   0.0471
  -9.250  -0.1880   0.04459   0.04030  -0.1245   0.6656   0.0472
  -9.000  -0.1783   0.04249   0.03813  -0.1248   0.6621   0.0474
  -8.750  -0.2052   0.03361   0.02864  -0.1246   0.6599   0.0457
  -8.500  -0.2119   0.02772   0.02203  -0.1231   0.6572   0.0460
  -8.250  -0.1056   0.04524   0.04076  -0.1247   0.6512   0.0586
  -8.000  -0.0860   0.04393   0.03943  -0.1248   0.6479   0.0589
  -7.750  -0.0683   0.04242   0.03790  -0.1249   0.6453   0.0592
  -7.500  -0.1299   0.02207   0.01547  -0.1213   0.6450   0.0483
  -7.250  -0.1042   0.02143   0.01477  -0.1212   0.6421   0.0488
  -7.000  -0.0789   0.02068   0.01391  -0.1211   0.6389   0.0494
  -6.750  -0.0535   0.01990   0.01298  -0.1208   0.6357   0.0501
  -6.500  -0.0278   0.01918   0.01207  -0.1206   0.6326   0.0509
  -6.250  -0.0013   0.01861   0.01129  -0.1205   0.6298   0.0517
  -6.000   0.0258   0.01822   0.01073  -0.1204   0.6274   0.0523
  -5.750   0.0522   0.01727   0.00981  -0.1205   0.6254   0.0533
  -5.500   0.0798   0.01692   0.00946  -0.1205   0.6228   0.0542
  -5.250   0.1075   0.01657   0.00908  -0.1206   0.6200   0.0552
  -5.000   0.1353   0.01620   0.00865  -0.1206   0.6173   0.0562
  -4.750   0.1632   0.01587   0.00824  -0.1206   0.6148   0.0572
  -4.500   0.1914   0.01566   0.00792  -0.1207   0.6121   0.0581
  -4.250   0.2187   0.01515   0.00737  -0.1207   0.6090   0.0593
  -4.000   0.2463   0.01485   0.00713  -0.1208   0.6069   0.0606
  -3.750   0.2742   0.01463   0.00692  -0.1209   0.6041   0.0620
  -3.500   0.3022   0.01441   0.00667  -0.1209   0.6010   0.0635
  -3.250   0.3304   0.01423   0.00645  -0.1209   0.5979   0.0647
  -3.000   0.3574   0.01383   0.00606  -0.1209   0.5951   0.0664
  -2.750   0.3855   0.01372   0.00592  -0.1210   0.5919   0.0681
  -2.500   0.4138   0.01364   0.00583  -0.1212   0.5888   0.0702
  -2.250   0.4416   0.01348   0.00567  -0.1212   0.5858   0.0722
  -2.000   0.4688   0.01321   0.00545  -0.1211   0.5822   0.0747
  -1.750   0.4967   0.01307   0.00532  -0.1212   0.5783   0.0773
  -1.500   0.5248   0.01300   0.00520  -0.1212   0.5747   0.0800
  -1.250   0.5527   0.01291   0.00510  -0.1214   0.5707   0.0840
  -1.000   0.5802   0.01279   0.00503  -0.1213   0.5673   0.0883
  -0.750   0.6074   0.01261   0.00490  -0.1213   0.5629   0.0937
  -0.500   0.6348   0.01248   0.00477  -0.1213   0.5582   0.1011
  -0.250   0.6620   0.01239   0.00466  -0.1213   0.5535   0.1113
   0.000   0.6887   0.01220   0.00456  -0.1212   0.5483   0.1259
   0.250   0.7151   0.01199   0.00447  -0.1211   0.5422   0.1517
   0.500   0.7392   0.01146   0.00444  -0.1208   0.5365   0.3262
   0.750   0.7627   0.01092   0.00450  -0.1204   0.5298   0.5169
   1.000   0.7820   0.01031   0.00460  -0.1189   0.5220   0.7450
   1.250   0.7998   0.01007   0.00476  -0.1162   0.5139   0.9035
   1.500   0.8408   0.01021   0.00487  -0.1189   0.5021   0.9715
   1.750   0.8908   0.01042   0.00497  -0.1238   0.4886   0.9944
   2.000   0.9263   0.01064   0.00507  -0.1257   0.4768   1.0000
   2.500   0.9587   0.01105   0.00529  -0.1216   0.4590   1.0000
   2.750   0.9746   0.01131   0.00544  -0.1196   0.4515   1.0000
   3.000   0.9938   0.01153   0.00560  -0.1181   0.4453   1.0000
   3.250   1.0125   0.01178   0.00579  -0.1167   0.4392   1.0000
   3.500   1.0291   0.01211   0.00601  -0.1148   0.4336   1.0000
   3.750   1.0490   0.01231   0.00620  -0.1135   0.4292   1.0000
   4.000   1.0684   0.01257   0.00642  -0.1122   0.4248   1.0000
   4.250   1.0874   0.01289   0.00668  -0.1110   0.4206   1.0000
   4.500   1.1067   0.01327   0.00698  -0.1098   0.4164   1.0000
   4.750   1.1286   0.01352   0.00723  -0.1091   0.4134   1.0000
   5.000   1.1504   0.01379   0.00751  -0.1084   0.4101   1.0000
   5.250   1.1714   0.01411   0.00780  -0.1076   0.4067   1.0000
   5.500   1.1918   0.01448   0.00813  -0.1067   0.4033   1.0000
   5.750   1.2128   0.01491   0.00848  -0.1060   0.3995   1.0000
   6.000   1.2344   0.01523   0.00882  -0.1054   0.3969   1.0000
   6.250   1.2558   0.01555   0.00916  -0.1048   0.3943   1.0000
   6.500   1.2770   0.01590   0.00952  -0.1042   0.3916   1.0000
   6.750   1.2978   0.01628   0.00989  -0.1036   0.3889   1.0000
   7.000   1.3184   0.01669   0.01028  -0.1029   0.3862   1.0000
   7.250   1.3397   0.01713   0.01068  -0.1024   0.3833   1.0000
   7.500   1.3618   0.01754   0.01107  -0.1020   0.3807   1.0000
   7.750   1.3811   0.01796   0.01154  -0.1012   0.3786   1.0000
   8.000   1.4006   0.01840   0.01201  -0.1005   0.3761   1.0000
   8.250   1.4202   0.01885   0.01249  -0.0999   0.3735   1.0000
   8.500   1.4396   0.01933   0.01298  -0.0992   0.3712   1.0000
   8.750   1.4591   0.01982   0.01346  -0.0986   0.3689   1.0000
   9.000   1.4800   0.02030   0.01391  -0.0981   0.3663   1.0000
   9.250   1.5022   0.02074   0.01434  -0.0979   0.3638   1.0000
   9.500   1.5191   0.02132   0.01500  -0.0970   0.3621   1.0000
   9.750   1.5361   0.02191   0.01564  -0.0962   0.3599   1.0000
  10.000   1.5527   0.02253   0.01630  -0.0954   0.3573   1.0000
  10.250   1.5682   0.02321   0.01700  -0.0945   0.3544   1.0000
  10.500   1.5840   0.02389   0.01769  -0.0936   0.3513   1.0000
  10.750   1.6042   0.02443   0.01816  -0.0932   0.3475   1.0000
  11.000   1.6149   0.02538   0.01921  -0.0919   0.3452   1.0000
  11.250   1.6273   0.02628   0.02019  -0.0909   0.3423   1.0000
  11.500   1.6406   0.02716   0.02112  -0.0900   0.3394   1.0000
  11.750   1.6540   0.02806   0.02205  -0.0891   0.3367   1.0000
  12.000   1.6683   0.02892   0.02290  -0.0883   0.3339   1.0000
  12.250   1.6856   0.02960   0.02357  -0.0878   0.3308   1.0000
  12.500   1.6954   0.03081   0.02489  -0.0868   0.3286   1.0000
  12.750   1.7064   0.03199   0.02615  -0.0860   0.3258   1.0000
  13.000   1.7162   0.03328   0.02750  -0.0851   0.3226   1.0000
  13.250   1.7264   0.03455   0.02880  -0.0843   0.3192   1.0000
  13.500   1.7385   0.03564   0.02985  -0.0836   0.3154   1.0000
  13.750   1.7463   0.03723   0.03155  -0.0828   0.3126   1.0000
  14.000   1.7541   0.03885   0.03326  -0.0821   0.3093   1.0000
  14.250   1.7618   0.04051   0.03498  -0.0815   0.3058   1.0000
  14.500   1.7696   0.04212   0.03660  -0.0808   0.3022   1.0000
  14.750   1.7781   0.04366   0.03814  -0.0802   0.2987   1.0000
  15.000   1.7840   0.04561   0.04022  -0.0797   0.2955   1.0000
  15.250   1.7899   0.04755   0.04225  -0.0791   0.2917   1.0000
  15.500   1.7937   0.04966   0.04438  -0.0785   0.2876   1.0000
  15.750   1.7972   0.05176   0.04648  -0.0779   0.2832   1.0000
  16.000   1.7998   0.05414   0.04899  -0.0774   0.2787   1.0000
  16.250   1.8013   0.05657   0.05146  -0.0769   0.2740   1.0000
  16.500   1.8010   0.05909   0.05397  -0.0762   0.2693   1.0000
  16.750   1.8027   0.06157   0.05657  -0.0758   0.2648   1.0000
  17.000   1.8027   0.06419   0.05925  -0.0754   0.2597   1.0000
  17.250   1.7983   0.06724   0.06230  -0.0748   0.2547   1.0000
  17.500   1.7982   0.06995   0.06511  -0.0744   0.2494   1.0000
  17.750   1.7912   0.07342   0.06861  -0.0739   0.2432   1.0000
  18.000   1.7857   0.07672   0.07196  -0.0735   0.2373   1.0000
  18.250   1.7777   0.08039   0.07569  -0.0732   0.2305   1.0000
  18.500   1.7661   0.08449   0.07981  -0.0728   0.2239   1.0000
  18.750   1.7554   0.08856   0.08394  -0.0726   0.2162   1.0000
  19.000   1.7409   0.09310   0.08850  -0.0725   0.2089   1.0000
  19.250   1.7231   0.09813   0.09356  -0.0725   0.2007   1.0000
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