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GOE 384 AIRFOIL (goe384-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 384 AIRFOIL (goe384-il)
Reynolds number: 500,000
Max Cl/Cd: 78.37 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe384-il-500000-n5.txt
Download as CSV file: xf-goe384-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.5833   0.04359   0.03948  -0.1207   0.7659   0.0326
 -13.500  -0.6191   0.03564   0.03107  -0.1287   0.7505   0.0327
 -13.250  -0.6301   0.03256   0.02767  -0.1288   0.7308   0.0329
 -13.000  -0.6338   0.03065   0.02544  -0.1272   0.7090   0.0330
 -12.750  -0.6247   0.02930   0.02389  -0.1263   0.6897   0.0332
 -12.500  -0.6106   0.02830   0.02273  -0.1255   0.6755   0.0334
 -12.250  -0.5938   0.02747   0.02176  -0.1249   0.6647   0.0336
 -12.000  -0.5753   0.02671   0.02089  -0.1243   0.6569   0.0338
 -11.750  -0.5559   0.02600   0.02006  -0.1238   0.6504   0.0340
 -11.500  -0.5356   0.02530   0.01925  -0.1233   0.6457   0.0342
 -11.250  -0.5146   0.02458   0.01844  -0.1228   0.6418   0.0345
 -11.000  -0.4930   0.02390   0.01765  -0.1224   0.6382   0.0348
 -10.750  -0.4708   0.02325   0.01688  -0.1220   0.6348   0.0351
 -10.500  -0.4483   0.02260   0.01610  -0.1216   0.6318   0.0355
 -10.000  -0.4024   0.02123   0.01444  -0.1209   0.6269   0.0364
  -9.750  -0.3787   0.02054   0.01362  -0.1205   0.6245   0.0367
  -9.500  -0.3543   0.01993   0.01287  -0.1202   0.6217   0.0371
  -9.250  -0.3298   0.01935   0.01220  -0.1200   0.6186   0.0374
  -9.000  -0.3046   0.01890   0.01170  -0.1197   0.6156   0.0377
  -8.750  -0.2788   0.01854   0.01128  -0.1195   0.6126   0.0380
  -8.250  -0.2263   0.01787   0.01049  -0.1193   0.6072   0.0388
  -8.000  -0.1996   0.01751   0.01009  -0.1192   0.6052   0.0392
  -7.750  -0.1728   0.01716   0.00968  -0.1191   0.6031   0.0397
  -7.500  -0.1459   0.01681   0.00927  -0.1190   0.6011   0.0403
  -7.250  -0.1188   0.01650   0.00888  -0.1190   0.5987   0.0409
  -7.000  -0.0917   0.01621   0.00849  -0.1189   0.5962   0.0415
  -6.750  -0.0649   0.01589   0.00811  -0.1188   0.5936   0.0420
  -6.500  -0.0380   0.01562   0.00781  -0.1187   0.5908   0.0425
  -6.250  -0.0105   0.01538   0.00755  -0.1187   0.5885   0.0431
  -6.000   0.0173   0.01514   0.00729  -0.1187   0.5865   0.0437
  -5.750   0.0451   0.01490   0.00704  -0.1188   0.5844   0.0443
  -5.500   0.0729   0.01467   0.00678  -0.1188   0.5821   0.0451
  -5.250   0.1007   0.01445   0.00652  -0.1188   0.5796   0.0458
  -5.000   0.1286   0.01427   0.00628  -0.1189   0.5770   0.0465
  -4.750   0.1560   0.01404   0.00603  -0.1189   0.5746   0.0474
  -4.500   0.1837   0.01388   0.00585  -0.1189   0.5723   0.0482
  -4.250   0.2117   0.01374   0.00570  -0.1190   0.5702   0.0492
  -4.000   0.2399   0.01356   0.00552  -0.1191   0.5681   0.0501
  -3.750   0.2681   0.01339   0.00535  -0.1192   0.5654   0.0511
  -3.500   0.2962   0.01325   0.00518  -0.1193   0.5622   0.0520
  -3.250   0.3239   0.01307   0.00500  -0.1193   0.5589   0.0531
  -3.000   0.3516   0.01294   0.00486  -0.1193   0.5558   0.0543
  -2.750   0.3793   0.01286   0.00474  -0.1194   0.5528   0.0558
  -2.500   0.4077   0.01274   0.00464  -0.1195   0.5499   0.0572
  -2.250   0.4359   0.01262   0.00453  -0.1196   0.5462   0.0585
  -2.000   0.4636   0.01250   0.00441  -0.1197   0.5419   0.0602
  -1.750   0.4910   0.01243   0.00432  -0.1197   0.5372   0.0621
  -1.500   0.5188   0.01236   0.00425  -0.1197   0.5326   0.0644
  -1.250   0.5465   0.01227   0.00418  -0.1198   0.5267   0.0670
  -1.000   0.5736   0.01223   0.00413  -0.1197   0.5205   0.0701
  -0.750   0.6009   0.01219   0.00410  -0.1197   0.5140   0.0740
  -0.500   0.6276   0.01217   0.00408  -0.1196   0.5048   0.0799
  -0.250   0.6536   0.01218   0.00408  -0.1194   0.4939   0.0875
   0.000   0.6784   0.01223   0.00409  -0.1190   0.4809   0.0950
   0.250   0.7022   0.01234   0.00413  -0.1184   0.4674   0.1019
   0.500   0.7258   0.01247   0.00419  -0.1178   0.4554   0.1093
   0.750   0.7497   0.01257   0.00427  -0.1172   0.4461   0.1184
   1.000   0.7728   0.01270   0.00438  -0.1166   0.4376   0.1308
   1.250   0.7962   0.01261   0.00451  -0.1161   0.4310   0.2111
   1.500   0.8191   0.01254   0.00467  -0.1156   0.4245   0.3092
   1.750   0.8407   0.01254   0.00487  -0.1148   0.4186   0.4025
   2.000   0.8640   0.01236   0.00505  -0.1144   0.4139   0.5312
   2.250   0.8839   0.01204   0.00530  -0.1132   0.4095   0.7258
   2.500   0.8969   0.01189   0.00560  -0.1100   0.4056   0.8860
   2.750   0.9393   0.01216   0.00589  -0.1132   0.4012   0.9968
   3.000   0.9609   0.01234   0.00604  -0.1123   0.3983   1.0000
   3.250   0.9813   0.01254   0.00622  -0.1112   0.3952   1.0000
   3.500   1.0016   0.01278   0.00642  -0.1101   0.3919   1.0000
   3.750   1.0215   0.01307   0.00667  -0.1090   0.3885   1.0000
   4.000   1.0410   0.01340   0.00694  -0.1079   0.3851   1.0000
   4.250   1.0617   0.01371   0.00722  -0.1070   0.3823   1.0000
   4.500   1.0845   0.01396   0.00746  -0.1065   0.3800   1.0000
   4.750   1.1067   0.01423   0.00773  -0.1059   0.3776   1.0000
   5.000   1.1284   0.01454   0.00803  -0.1053   0.3750   1.0000
   5.250   1.1496   0.01488   0.00835  -0.1046   0.3724   1.0000
   5.500   1.1699   0.01527   0.00871  -0.1039   0.3698   1.0000
   5.750   1.1895   0.01570   0.00911  -0.1030   0.3671   1.0000
   6.000   1.2096   0.01612   0.00952  -0.1023   0.3646   1.0000
   6.250   1.2316   0.01646   0.00987  -0.1019   0.3625   1.0000
   6.500   1.2530   0.01683   0.01025  -0.1014   0.3602   1.0000
   6.750   1.2738   0.01724   0.01067  -0.1008   0.3579   1.0000
   7.000   1.2937   0.01769   0.01113  -0.1002   0.3556   1.0000
   7.250   1.3131   0.01818   0.01161  -0.0995   0.3534   1.0000
   7.500   1.3317   0.01873   0.01215  -0.0988   0.3511   1.0000
   7.750   1.3493   0.01933   0.01274  -0.0979   0.3489   1.0000
   8.000   1.3684   0.01986   0.01328  -0.0973   0.3469   1.0000
   8.250   1.3886   0.02034   0.01381  -0.0968   0.3450   1.0000
   8.500   1.4077   0.02088   0.01438  -0.0963   0.3427   1.0000
   8.750   1.4264   0.02146   0.01498  -0.0957   0.3405   1.0000
   9.000   1.4441   0.02209   0.01564  -0.0950   0.3383   1.0000
   9.250   1.4609   0.02279   0.01635  -0.0943   0.3362   1.0000
   9.500   1.4772   0.02352   0.01708  -0.0935   0.3341   1.0000
   9.750   1.4921   0.02435   0.01792  -0.0926   0.3320   1.0000
  10.000   1.5084   0.02510   0.01870  -0.0919   0.3302   1.0000
  10.250   1.5261   0.02578   0.01944  -0.0914   0.3280   1.0000
  10.500   1.5414   0.02663   0.02033  -0.0907   0.3247   1.0000
  10.750   1.5551   0.02760   0.02132  -0.0899   0.3208   1.0000
  11.000   1.5664   0.02876   0.02249  -0.0889   0.3173   1.0000
  11.250   1.5778   0.02993   0.02366  -0.0880   0.3141   1.0000
  11.500   1.5929   0.03090   0.02469  -0.0875   0.3111   1.0000
  11.750   1.6060   0.03202   0.02587  -0.0869   0.3071   1.0000
  12.000   1.6163   0.03338   0.02724  -0.0861   0.3033   1.0000
  12.250   1.6252   0.03485   0.02873  -0.0852   0.2999   1.0000
  12.500   1.6368   0.03615   0.03006  -0.0846   0.2972   1.0000
  12.750   1.6501   0.03733   0.03132  -0.0841   0.2945   1.0000
  13.000   1.6609   0.03874   0.03278  -0.0835   0.2912   1.0000
  13.250   1.6689   0.04040   0.03447  -0.0828   0.2874   1.0000
  13.500   1.6745   0.04229   0.03636  -0.0820   0.2836   1.0000
  13.750   1.6844   0.04384   0.03799  -0.0816   0.2798   1.0000
  14.000   1.6919   0.04563   0.03983  -0.0810   0.2750   1.0000
  14.250   1.6938   0.04796   0.04216  -0.0802   0.2697   1.0000
  14.500   1.6996   0.04992   0.04417  -0.0796   0.2652   1.0000
  14.750   1.7050   0.05193   0.04622  -0.0791   0.2600   1.0000
  15.000   1.7047   0.05450   0.04882  -0.0783   0.2549   1.0000
  15.250   1.7095   0.05658   0.05094  -0.0778   0.2503   1.0000
  15.500   1.7112   0.05901   0.05341  -0.0772   0.2447   1.0000
  15.750   1.7078   0.06195   0.05637  -0.0764   0.2389   1.0000
  16.000   1.7080   0.06457   0.05904  -0.0759   0.2321   1.0000
  16.250   1.7004   0.06804   0.06251  -0.0751   0.2248   1.0000
  16.500   1.6959   0.07124   0.06575  -0.0746   0.2167   1.0000
  16.750   1.6858   0.07511   0.06963  -0.0740   0.2089   1.0000
  17.000   1.6751   0.07907   0.07360  -0.0734   0.1998   1.0000
  17.250   1.6618   0.08343   0.07798  -0.0729   0.1913   1.0000
  17.500   1.6454   0.08824   0.08282  -0.0726   0.1834   1.0000
  17.750   1.6308   0.09291   0.08751  -0.0724   0.1755   1.0000
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