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GOE 384 AIRFOIL (goe384-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 384 AIRFOIL (goe384-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.13 at α=4°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe384-il-1000000.txt
Download as CSV file: xf-goe384-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.6754   0.03738   0.03407  -0.1263   0.8215   0.0322
 -14.000  -0.6906   0.03329   0.02971  -0.1289   0.8113   0.0324
 -13.750  -0.6955   0.03088   0.02710  -0.1286   0.8003   0.0325
 -13.500  -0.6962   0.02928   0.02530  -0.1268   0.7879   0.0327
 -13.250  -0.6866   0.02797   0.02378  -0.1259   0.7720   0.0328
 -13.000  -0.6731   0.02688   0.02249  -0.1250   0.7507   0.0329
 -12.750  -0.6644   0.02520   0.02050  -0.1239   0.7222   0.0332
 -12.500  -0.6523   0.02369   0.01875  -0.1229   0.6944   0.0335
 -12.250  -0.6320   0.02305   0.01799  -0.1224   0.6762   0.0338
 -12.000  -0.6094   0.02262   0.01747  -0.1220   0.6645   0.0341
 -11.750  -0.5860   0.02220   0.01698  -0.1216   0.6573   0.0344
 -11.500  -0.5628   0.02173   0.01643  -0.1213   0.6510   0.0346
 -11.250  -0.5396   0.02119   0.01580  -0.1209   0.6461   0.0349
 -11.000  -0.5160   0.02062   0.01514  -0.1206   0.6428   0.0352
 -10.750  -0.4922   0.02004   0.01447  -0.1202   0.6394   0.0356
 -10.500  -0.4681   0.01950   0.01382  -0.1199   0.6356   0.0359
 -10.250  -0.4437   0.01898   0.01319  -0.1196   0.6315   0.0363
 -10.000  -0.4188   0.01850   0.01259  -0.1193   0.6278   0.0366
  -9.750  -0.3930   0.01803   0.01204  -0.1191   0.6258   0.0369
  -9.500  -0.3668   0.01764   0.01157  -0.1190   0.6234   0.0371
  -9.250  -0.3428   0.01679   0.01062  -0.1187   0.6207   0.0376
  -9.000  -0.3175   0.01618   0.00997  -0.1184   0.6182   0.0380
  -8.750  -0.2908   0.01586   0.00962  -0.1184   0.6159   0.0384
  -8.500  -0.2635   0.01564   0.00936  -0.1183   0.6135   0.0389
  -8.250  -0.2362   0.01544   0.00911  -0.1183   0.6104   0.0394
  -8.000  -0.2087   0.01518   0.00881  -0.1183   0.6082   0.0399
  -7.750  -0.1810   0.01486   0.00845  -0.1183   0.6068   0.0404
  -7.500  -0.1532   0.01456   0.00811  -0.1183   0.6052   0.0409
  -7.250  -0.1253   0.01429   0.00779  -0.1183   0.6033   0.0413
  -7.000  -0.0970   0.01407   0.00752  -0.1184   0.6011   0.0417
  -6.750  -0.0706   0.01353   0.00693  -0.1182   0.5988   0.0424
  -6.500  -0.0432   0.01320   0.00659  -0.1182   0.5965   0.0430
  -6.250  -0.0153   0.01301   0.00638  -0.1183   0.5940   0.0436
  -6.000   0.0129   0.01287   0.00620  -0.1183   0.5914   0.0442
  -5.750   0.0413   0.01272   0.00603  -0.1185   0.5894   0.0449
  -5.500   0.0701   0.01255   0.00584  -0.1186   0.5883   0.0458
  -5.250   0.0991   0.01240   0.00567  -0.1188   0.5868   0.0464
  -5.000   0.1274   0.01215   0.00540  -0.1189   0.5849   0.0471
  -4.750   0.1550   0.01179   0.00505  -0.1189   0.5828   0.0481
  -4.500   0.1836   0.01161   0.00488  -0.1191   0.5806   0.0489
  -4.250   0.2122   0.01147   0.00473  -0.1193   0.5783   0.0498
  -4.000   0.2408   0.01135   0.00458  -0.1194   0.5760   0.0508
  -3.750   0.2694   0.01128   0.00447  -0.1195   0.5732   0.0517
  -3.500   0.2977   0.01115   0.00431  -0.1197   0.5705   0.0528
  -3.250   0.3262   0.01091   0.00410  -0.1198   0.5687   0.0542
  -3.000   0.3552   0.01077   0.00398  -0.1201   0.5663   0.0555
  -2.750   0.3841   0.01065   0.00386  -0.1203   0.5636   0.0568
  -2.500   0.4131   0.01056   0.00375  -0.1205   0.5607   0.0580
  -2.250   0.4413   0.01040   0.00358  -0.1207   0.5576   0.0597
  -2.000   0.4695   0.01033   0.00350  -0.1208   0.5540   0.0616
  -1.750   0.4984   0.01026   0.00343  -0.1210   0.5510   0.0637
  -1.500   0.5275   0.01014   0.00333  -0.1213   0.5476   0.0658
  -1.250   0.5562   0.01003   0.00324  -0.1215   0.5432   0.0688
  -1.000   0.5845   0.00999   0.00318  -0.1217   0.5384   0.0717
  -0.750   0.6126   0.00994   0.00314  -0.1218   0.5336   0.0770
  -0.500   0.6415   0.00986   0.00311  -0.1221   0.5283   0.0840
  -0.250   0.6695   0.00982   0.00308  -0.1222   0.5212   0.0935
   0.000   0.6973   0.00980   0.00307  -0.1223   0.5135   0.1036
   0.250   0.7243   0.00982   0.00305  -0.1223   0.5018   0.1126
   0.500   0.7507   0.00985   0.00306  -0.1221   0.4873   0.1234
   0.750   0.7755   0.00991   0.00311  -0.1218   0.4710   0.1476
   1.000   0.7989   0.00973   0.00322  -0.1214   0.4571   0.2802
   1.250   0.8223   0.00960   0.00338  -0.1209   0.4459   0.4088
   1.500   0.8453   0.00941   0.00355  -0.1204   0.4365   0.5606
   1.750   0.8674   0.00915   0.00374  -0.1196   0.4295   0.7363
   2.000   0.8861   0.00898   0.00397  -0.1177   0.4235   0.8815
   2.250   0.9081   0.00914   0.00420  -0.1164   0.4170   0.9559
   2.500   0.9506   0.00934   0.00437  -0.1197   0.4122   0.9901
   2.750   0.9960   0.00957   0.00454  -0.1238   0.4073   0.9999
   3.000   1.0139   0.00976   0.00468  -0.1220   0.4032   1.0000
   3.250   1.0314   0.00999   0.00485  -0.1202   0.3987   1.0000
   3.500   1.0543   0.01010   0.00495  -0.1195   0.3966   1.0000
   3.750   1.0757   0.01024   0.00508  -0.1184   0.3939   1.0000
   4.000   1.0955   0.01042   0.00524  -0.1171   0.3909   1.0000
   4.250   1.1152   0.01065   0.00544  -0.1158   0.3877   1.0000
   4.500   1.1342   0.01094   0.00569  -0.1145   0.3840   1.0000
   4.750   1.1549   0.01122   0.00594  -0.1136   0.3809   1.0000
   5.000   1.1788   0.01139   0.00612  -0.1132   0.3790   1.0000
   5.250   1.2023   0.01159   0.00633  -0.1128   0.3768   1.0000
   5.500   1.2249   0.01184   0.00657  -0.1123   0.3744   1.0000
   5.750   1.2468   0.01213   0.00684  -0.1116   0.3718   1.0000
   6.000   1.2675   0.01247   0.00716  -0.1109   0.3691   1.0000
   6.250   1.2868   0.01289   0.00755  -0.1099   0.3659   1.0000
   6.500   1.3085   0.01322   0.00788  -0.1093   0.3637   1.0000
   6.750   1.3319   0.01347   0.00815  -0.1091   0.3620   1.0000
   7.000   1.3547   0.01375   0.00845  -0.1087   0.3600   1.0000
   7.250   1.3769   0.01406   0.00877  -0.1083   0.3577   1.0000
   7.500   1.3978   0.01445   0.00915  -0.1078   0.3554   1.0000
   7.750   1.4176   0.01489   0.00959  -0.1071   0.3531   1.0000
   8.000   1.4359   0.01541   0.01010  -0.1062   0.3503   1.0000
   8.250   1.4531   0.01599   0.01067  -0.1052   0.3474   1.0000
   8.500   1.4753   0.01634   0.01105  -0.1049   0.3462   1.0000
   8.750   1.4970   0.01671   0.01146  -0.1046   0.3446   1.0000
   9.000   1.5178   0.01714   0.01191  -0.1042   0.3424   1.0000
   9.250   1.5373   0.01763   0.01241  -0.1037   0.3392   1.0000
   9.500   1.5539   0.01829   0.01305  -0.1028   0.3355   1.0000
   9.750   1.5670   0.01915   0.01389  -0.1015   0.3314   1.0000
  10.000   1.5878   0.01960   0.01438  -0.1012   0.3297   1.0000
  10.250   1.6076   0.02011   0.01494  -0.1008   0.3275   1.0000
  10.500   1.6261   0.02071   0.01556  -0.1003   0.3246   1.0000
  10.750   1.6426   0.02142   0.01628  -0.0996   0.3216   1.0000
  11.000   1.6559   0.02234   0.01720  -0.0986   0.3186   1.0000
  11.250   1.6673   0.02338   0.01824  -0.0973   0.3151   1.0000
  11.500   1.6860   0.02401   0.01892  -0.0970   0.3131   1.0000
  11.750   1.7037   0.02471   0.01967  -0.0966   0.3100   1.0000
  12.000   1.7182   0.02563   0.02061  -0.0959   0.3063   1.0000
  12.250   1.7288   0.02685   0.02183  -0.0948   0.3027   1.0000
  12.500   1.7379   0.02818   0.02317  -0.0937   0.2992   1.0000
  12.750   1.7548   0.02899   0.02403  -0.0934   0.2970   1.0000
  13.000   1.7697   0.02995   0.02504  -0.0929   0.2936   1.0000
  13.250   1.7804   0.03127   0.02638  -0.0921   0.2901   1.0000
  13.500   1.7886   0.03279   0.02791  -0.0911   0.2867   1.0000
  13.750   1.7969   0.03432   0.02947  -0.0903   0.2833   1.0000
  14.000   1.8106   0.03544   0.03065  -0.0898   0.2803   1.0000
  14.250   1.8203   0.03692   0.03216  -0.0892   0.2762   1.0000
  14.500   1.8235   0.03899   0.03424  -0.0882   0.2713   1.0000
  14.750   1.8307   0.04072   0.03600  -0.0874   0.2668   1.0000
  15.000   1.8387   0.04237   0.03770  -0.0868   0.2622   1.0000
  15.250   1.8406   0.04462   0.03996  -0.0859   0.2572   1.0000
  15.500   1.8442   0.04669   0.04205  -0.0851   0.2525   1.0000
  15.750   1.8487   0.04873   0.04413  -0.0844   0.2470   1.0000
  16.000   1.8446   0.05157   0.04697  -0.0833   0.2407   1.0000
  16.250   1.8474   0.05374   0.04918  -0.0826   0.2346   1.0000
  16.500   1.8401   0.05694   0.05237  -0.0815   0.2270   1.0000
  16.750   1.8384   0.05960   0.05504  -0.0807   0.2192   1.0000
  17.000   1.8262   0.06338   0.05882  -0.0796   0.2106   1.0000
  17.250   1.8151   0.06706   0.06250  -0.0785   0.2006   1.0000
  17.500   1.8028   0.07096   0.06639  -0.0776   0.1910   1.0000
  17.750   1.7857   0.07548   0.07091  -0.0767   0.1822   1.0000
  18.000   1.7688   0.08004   0.07548  -0.0759   0.1738   1.0000
  18.250   1.7560   0.08421   0.07967  -0.0754   0.1664   1.0000
  18.500   1.7379   0.08910   0.08458  -0.0749   0.1599   1.0000
  18.750   1.7267   0.09328   0.08880  -0.0747   0.1546   1.0000
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