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GOE 384 AIRFOIL (goe384-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 384 AIRFOIL (goe384-il)
Reynolds number: 1,000,000
Max Cl/Cd: 100.47 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe384-il-1000000-n5.txt
Download as CSV file: xf-goe384-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.9191   0.03693   0.03308  -0.1238   0.8074   0.0275
 -16.250  -0.9253   0.03284   0.02881  -0.1276   0.7972   0.0276
 -16.000  -0.9246   0.03034   0.02615  -0.1290   0.7880   0.0278
 -15.750  -0.9197   0.02857   0.02424  -0.1291   0.7765   0.0279
 -15.500  -0.9122   0.02720   0.02273  -0.1286   0.7635   0.0281
 -15.250  -0.9029   0.02610   0.02148  -0.1275   0.7457   0.0282
 -15.000  -0.8943   0.02525   0.02045  -0.1259   0.7188   0.0284
 -14.500  -0.8630   0.02372   0.01853  -0.1242   0.6634   0.0287
 -14.000  -0.8255   0.02234   0.01689  -0.1228   0.6424   0.0290
 -13.750  -0.8050   0.02171   0.01615  -0.1222   0.6360   0.0291
 -13.250  -0.7633   0.02042   0.01467  -0.1210   0.6261   0.0294
 -13.000  -0.7413   0.01981   0.01400  -0.1205   0.6226   0.0297
 -12.750  -0.7182   0.01929   0.01342  -0.1201   0.6192   0.0299
 -12.500  -0.6943   0.01883   0.01291  -0.1197   0.6161   0.0301
 -12.250  -0.6698   0.01841   0.01243  -0.1194   0.6133   0.0303
 -11.750  -0.6196   0.01763   0.01154  -0.1188   0.6083   0.0308
 -11.500  -0.5940   0.01725   0.01111  -0.1186   0.6069   0.0310
 -11.250  -0.5681   0.01688   0.01069  -0.1184   0.6054   0.0313
 -11.000  -0.5419   0.01652   0.01028  -0.1182   0.6038   0.0315
 -10.750  -0.5156   0.01618   0.00989  -0.1181   0.6018   0.0318
 -10.500  -0.4890   0.01587   0.00952  -0.1179   0.5994   0.0321
 -10.250  -0.4623   0.01557   0.00917  -0.1178   0.5968   0.0325
 -10.000  -0.4355   0.01529   0.00882  -0.1177   0.5942   0.0327
  -9.750  -0.4086   0.01502   0.00848  -0.1175   0.5918   0.0329
  -9.500  -0.3819   0.01471   0.00811  -0.1174   0.5894   0.0332
  -9.250  -0.3549   0.01436   0.00775  -0.1173   0.5880   0.0336
  -9.000  -0.3273   0.01408   0.00745  -0.1173   0.5864   0.0339
  -8.750  -0.2995   0.01383   0.00719  -0.1173   0.5848   0.0343
  -8.500  -0.2715   0.01361   0.00694  -0.1173   0.5832   0.0346
  -8.250  -0.2435   0.01339   0.00671  -0.1174   0.5815   0.0350
  -8.000  -0.2154   0.01319   0.00647  -0.1174   0.5793   0.0354
  -7.750  -0.1873   0.01300   0.00624  -0.1174   0.5770   0.0358
  -7.500  -0.1592   0.01281   0.00601  -0.1175   0.5749   0.0362
  -7.250  -0.1310   0.01264   0.00580  -0.1175   0.5731   0.0367
  -7.000  -0.1029   0.01249   0.00560  -0.1176   0.5710   0.0370
  -6.750  -0.0744   0.01228   0.00538  -0.1177   0.5694   0.0375
  -6.500  -0.0458   0.01207   0.00518  -0.1178   0.5674   0.0381
  -6.250  -0.0171   0.01191   0.00502  -0.1180   0.5652   0.0387
  -6.000   0.0117   0.01177   0.00486  -0.1181   0.5629   0.0392
  -5.750   0.0404   0.01163   0.00471  -0.1183   0.5609   0.0398
  -5.500   0.0692   0.01150   0.00456  -0.1184   0.5589   0.0404
  -5.250   0.0978   0.01138   0.00441  -0.1186   0.5568   0.0410
  -5.000   0.1265   0.01129   0.00428  -0.1187   0.5544   0.0415
  -4.750   0.1550   0.01116   0.00413  -0.1188   0.5521   0.0421
  -4.500   0.1840   0.01101   0.00399  -0.1191   0.5500   0.0429
  -4.250   0.2130   0.01089   0.00388  -0.1193   0.5473   0.0437
  -4.000   0.2421   0.01080   0.00379  -0.1195   0.5445   0.0446
  -3.750   0.2709   0.01072   0.00369  -0.1197   0.5414   0.0455
  -3.500   0.2996   0.01065   0.00360  -0.1199   0.5381   0.0462
  -3.250   0.3282   0.01059   0.00350  -0.1201   0.5347   0.0469
  -3.000   0.3572   0.01046   0.00340  -0.1203   0.5310   0.0480
  -2.750   0.3859   0.01039   0.00332  -0.1205   0.5256   0.0490
  -2.500   0.4142   0.01035   0.00325  -0.1206   0.5194   0.0501
  -2.250   0.4429   0.01030   0.00319  -0.1208   0.5138   0.0512
  -2.000   0.4711   0.01029   0.00314  -0.1210   0.5048   0.0522
  -1.750   0.4987   0.01026   0.00308  -0.1210   0.4939   0.0537
  -1.500   0.5253   0.01032   0.00307  -0.1209   0.4778   0.0552
  -1.250   0.5511   0.01043   0.00309  -0.1206   0.4600   0.0567
  -1.000   0.5769   0.01056   0.00313  -0.1203   0.4452   0.0581
  -0.750   0.6027   0.01066   0.00319  -0.1201   0.4340   0.0607
  -0.500   0.6294   0.01073   0.00323  -0.1200   0.4260   0.0635
  -0.250   0.6555   0.01082   0.00329  -0.1198   0.4187   0.0671
   0.000   0.6826   0.01086   0.00334  -0.1198   0.4138   0.0731
   0.250   0.7091   0.01091   0.00341  -0.1197   0.4085   0.0830
   0.500   0.7350   0.01101   0.00350  -0.1195   0.4030   0.0917
   0.750   0.7616   0.01108   0.00357  -0.1194   0.3989   0.0981
   1.000   0.7883   0.01113   0.00363  -0.1193   0.3954   0.1041
   1.250   0.8146   0.01120   0.00371  -0.1192   0.3919   0.1096
   1.500   0.8404   0.01128   0.00380  -0.1190   0.3884   0.1181
   1.750   0.8655   0.01136   0.00390  -0.1187   0.3849   0.1314
   2.000   0.8907   0.01124   0.00401  -0.1186   0.3821   0.2267
   2.250   0.9165   0.01113   0.00413  -0.1185   0.3798   0.3173
   2.500   0.9417   0.01102   0.00427  -0.1184   0.3769   0.4149
   2.750   0.9662   0.01091   0.00444  -0.1182   0.3739   0.5226
   3.000   0.9892   0.01076   0.00464  -0.1177   0.3709   0.6624
   3.250   1.0078   0.01054   0.00488  -0.1161   0.3682   0.8270
   3.500   1.0245   0.01054   0.00516  -0.1137   0.3654   0.9521
   3.750   1.0632   0.01069   0.00531  -0.1163   0.3636   1.0000
   4.000   1.0855   0.01086   0.00546  -0.1155   0.3618   1.0000
   4.250   1.1080   0.01104   0.00563  -0.1148   0.3596   1.0000
   4.500   1.1303   0.01125   0.00583  -0.1142   0.3572   1.0000
   4.750   1.1524   0.01150   0.00605  -0.1135   0.3545   1.0000
   5.000   1.1739   0.01178   0.00630  -0.1127   0.3517   1.0000
   5.250   1.1952   0.01208   0.00658  -0.1120   0.3488   1.0000
   5.500   1.2179   0.01234   0.00684  -0.1115   0.3470   1.0000
   5.750   1.2411   0.01258   0.00708  -0.1111   0.3456   1.0000
   6.000   1.2641   0.01284   0.00735  -0.1108   0.3438   1.0000
   6.250   1.2868   0.01312   0.00763  -0.1104   0.3419   1.0000
   6.500   1.3087   0.01344   0.00795  -0.1099   0.3398   1.0000
   6.750   1.3301   0.01379   0.00829  -0.1093   0.3376   1.0000
   7.000   1.3507   0.01418   0.00868  -0.1087   0.3351   1.0000
   7.250   1.3702   0.01464   0.00912  -0.1079   0.3324   1.0000
   7.500   1.3909   0.01505   0.00953  -0.1074   0.3303   1.0000
   7.750   1.4129   0.01540   0.00991  -0.1070   0.3289   1.0000
   8.000   1.4340   0.01579   0.01032  -0.1066   0.3273   1.0000
   8.250   1.4548   0.01621   0.01075  -0.1061   0.3255   1.0000
   8.500   1.4750   0.01666   0.01121  -0.1056   0.3235   1.0000
   8.750   1.4941   0.01719   0.01175  -0.1050   0.3215   1.0000
   9.000   1.5121   0.01778   0.01234  -0.1042   0.3187   1.0000
   9.250   1.5269   0.01855   0.01310  -0.1032   0.3146   1.0000
   9.500   1.5470   0.01904   0.01362  -0.1027   0.3114   1.0000
   9.750   1.5650   0.01966   0.01424  -0.1021   0.3072   1.0000
  10.000   1.5804   0.02044   0.01502  -0.1012   0.3035   1.0000
  10.250   1.5942   0.02133   0.01590  -0.1002   0.2996   1.0000
  10.500   1.6105   0.02208   0.01668  -0.0995   0.2965   1.0000
  10.750   1.6267   0.02284   0.01746  -0.0988   0.2929   1.0000
  11.000   1.6411   0.02374   0.01837  -0.0980   0.2894   1.0000
  11.250   1.6536   0.02479   0.01943  -0.0970   0.2861   1.0000
  11.500   1.6656   0.02590   0.02055  -0.0960   0.2828   1.0000
  11.750   1.6804   0.02683   0.02151  -0.0954   0.2794   1.0000
  12.000   1.6925   0.02798   0.02268  -0.0945   0.2748   1.0000
  12.250   1.7002   0.02948   0.02418  -0.0934   0.2698   1.0000
  12.500   1.7106   0.03083   0.02555  -0.0925   0.2653   1.0000
  12.750   1.7192   0.03233   0.02706  -0.0916   0.2590   1.0000
  13.000   1.7230   0.03426   0.02898  -0.0904   0.2531   1.0000
  13.250   1.7316   0.03584   0.03059  -0.0896   0.2477   1.0000
  13.500   1.7343   0.03794   0.03269  -0.0884   0.2410   1.0000
  13.750   1.7393   0.03989   0.03465  -0.0875   0.2349   1.0000
  14.000   1.7404   0.04221   0.03697  -0.0865   0.2275   1.0000
  14.250   1.7416   0.04453   0.03930  -0.0855   0.2211   1.0000
  14.500   1.7379   0.04733   0.04209  -0.0843   0.2123   1.0000
  14.750   1.7343   0.05013   0.04489  -0.0831   0.2025   1.0000
  15.000   1.7246   0.05356   0.04829  -0.0817   0.1916   1.0000
  15.250   1.7111   0.05740   0.05211  -0.0803   0.1803   1.0000
  15.500   1.6980   0.06130   0.05599  -0.0790   0.1701   1.0000
  15.750   1.6886   0.06487   0.05955  -0.0780   0.1611   1.0000
  16.000   1.6798   0.06847   0.06317  -0.0771   0.1546   1.0000
  16.250   1.6714   0.07209   0.06681  -0.0764   0.1484   1.0000
  16.500   1.6655   0.07550   0.07025  -0.0758   0.1432   1.0000
  16.750   1.6571   0.07924   0.07402  -0.0753   0.1380   1.0000
  17.000   1.6482   0.08306   0.07788  -0.0748   0.1331   1.0000
  17.250   1.6416   0.08671   0.08156  -0.0746   0.1284   1.0000
  17.500   1.6296   0.09106   0.08595  -0.0743   0.1237   1.0000
  17.750   1.6221   0.09491   0.08985  -0.0742   0.1198   1.0000
  18.000   1.6131   0.09894   0.09391  -0.0742   0.1151   1.0000
  18.250   1.6003   0.10354   0.09855  -0.0743   0.1107   1.0000
  18.500   1.5893   0.10797   0.10303  -0.0746   0.1057   1.0000
  18.750   1.5746   0.11293   0.10801  -0.0750   0.1003   1.0000
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