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GOE 413 AIRFOIL (goe413-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 413 AIRFOIL (goe413-il)
Reynolds number: 1,000,000
Max Cl/Cd: 130.84 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe413-il-1000000.txt
Download as CSV file: xf-goe413-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 413 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.8430   0.05927   0.05649  -0.0745   1.0000   0.0366
 -14.250  -0.8642   0.05163   0.04864  -0.0825   0.9496   0.0367
 -14.000  -0.8802   0.04619   0.04293  -0.0873   0.9096   0.0368
 -13.750  -0.8872   0.04156   0.03807  -0.0923   0.8914   0.0369
 -13.500  -0.8882   0.03764   0.03397  -0.0971   0.8786   0.0371
 -13.250  -0.8854   0.03459   0.03074  -0.1012   0.8688   0.0372
 -13.000  -0.8761   0.03254   0.02853  -0.1032   0.8612   0.0374
 -12.750  -0.8619   0.03093   0.02676  -0.1043   0.8547   0.0377
 -12.500  -0.8449   0.02943   0.02515  -0.1051   0.8500   0.0379
 -12.250  -0.8263   0.02809   0.02367  -0.1057   0.8447   0.0382
 -12.000  -0.8063   0.02689   0.02233  -0.1061   0.8393   0.0385
 -11.750  -0.7850   0.02583   0.02113  -0.1065   0.8339   0.0387
 -11.500  -0.7621   0.02486   0.02005  -0.1068   0.8299   0.0389
 -11.250  -0.7382   0.02405   0.01913  -0.1071   0.8254   0.0392
 -11.000  -0.7134   0.02344   0.01840  -0.1073   0.8206   0.0393
 -10.750  -0.6917   0.02189   0.01670  -0.1075   0.8153   0.0398
 -10.500  -0.6670   0.02085   0.01565  -0.1077   0.8110   0.0401
 -10.250  -0.6411   0.02014   0.01492  -0.1079   0.8061   0.0404
 -10.000  -0.6149   0.01954   0.01426  -0.1080   0.8009   0.0406
  -9.750  -0.5884   0.01901   0.01366  -0.1081   0.7954   0.0409
  -9.500  -0.5613   0.01846   0.01308  -0.1083   0.7908   0.0412
  -9.250  -0.5340   0.01793   0.01251  -0.1084   0.7851   0.0415
  -9.000  -0.5068   0.01742   0.01194  -0.1085   0.7786   0.0418
  -8.750  -0.4794   0.01693   0.01139  -0.1086   0.7722   0.0422
  -8.500  -0.4516   0.01643   0.01084  -0.1088   0.7650   0.0425
  -8.250  -0.4239   0.01597   0.01031  -0.1089   0.7571   0.0429
  -8.000  -0.3958   0.01553   0.00982  -0.1090   0.7491   0.0432
  -7.750  -0.3676   0.01514   0.00936  -0.1091   0.7389   0.0435
  -7.500  -0.3390   0.01486   0.00900  -0.1092   0.7278   0.0438
  -7.250  -0.3104   0.01468   0.00872  -0.1093   0.7139   0.0441
  -7.000  -0.2836   0.01381   0.00780  -0.1094   0.6982   0.0446
  -6.750  -0.2559   0.01330   0.00724  -0.1095   0.6830   0.0450
  -6.500  -0.2276   0.01295   0.00684  -0.1096   0.6697   0.0454
  -6.000  -0.1704   0.01241   0.00620  -0.1099   0.6477   0.0463
  -5.750  -0.1417   0.01219   0.00590  -0.1100   0.6380   0.0467
  -5.500  -0.1125   0.01194   0.00562  -0.1102   0.6309   0.0472
  -5.250  -0.0834   0.01172   0.00536  -0.1103   0.6239   0.0477
  -5.000  -0.0544   0.01154   0.00512  -0.1105   0.6171   0.0482
  -4.750  -0.0248   0.01133   0.00490  -0.1107   0.6120   0.0486
  -4.500   0.0047   0.01120   0.00473  -0.1109   0.6063   0.0490
  -4.250   0.0337   0.01090   0.00437  -0.1111   0.6006   0.0497
  -4.000   0.0631   0.01059   0.00404  -0.1114   0.5957   0.0504
  -3.750   0.0928   0.01036   0.00381  -0.1116   0.5913   0.0511
  -3.500   0.1225   0.01020   0.00363  -0.1119   0.5861   0.0517
  -3.250   0.1519   0.01009   0.00347  -0.1120   0.5804   0.0525
  -3.000   0.1817   0.00996   0.00332  -0.1122   0.5757   0.0532
  -2.750   0.2116   0.00982   0.00318  -0.1125   0.5714   0.0539
  -2.500   0.2414   0.00973   0.00306  -0.1127   0.5668   0.0545
  -2.250   0.2710   0.00958   0.00287  -0.1129   0.5621   0.0556
  -2.000   0.3007   0.00946   0.00273  -0.1131   0.5574   0.0571
  -1.750   0.3308   0.00933   0.00262  -0.1134   0.5541   0.0584
  -1.500   0.3607   0.00925   0.00253  -0.1136   0.5501   0.0597
  -1.250   0.3905   0.00918   0.00244  -0.1138   0.5459   0.0612
  -1.000   0.4201   0.00911   0.00235  -0.1139   0.5411   0.0640
  -0.750   0.4499   0.00904   0.00229  -0.1142   0.5371   0.0687
  -0.500   0.4801   0.00863   0.00217  -0.1147   0.5338   0.1465
  -0.250   0.5100   0.00851   0.00216  -0.1150   0.5297   0.1751
   0.000   0.5396   0.00845   0.00216  -0.1153   0.5251   0.1984
   0.250   0.5689   0.00845   0.00218  -0.1154   0.5200   0.2180
   0.500   0.5989   0.00838   0.00219  -0.1157   0.5168   0.2395
   0.750   0.6288   0.00830   0.00221  -0.1160   0.5128   0.2647
   1.000   0.6585   0.00826   0.00224  -0.1162   0.5081   0.2933
   1.250   0.6877   0.00826   0.00229  -0.1164   0.5028   0.3223
   1.500   0.7174   0.00822   0.00234  -0.1166   0.4977   0.3515
   1.750   0.7470   0.00820   0.00237  -0.1169   0.4915   0.3772
   2.000   0.7762   0.00822   0.00242  -0.1170   0.4853   0.4001
   2.250   0.8055   0.00824   0.00249  -0.1172   0.4797   0.4247
   2.500   0.8351   0.00819   0.00255  -0.1174   0.4735   0.4613
   2.750   0.8640   0.00821   0.00264  -0.1176   0.4658   0.5080
   3.000   0.8932   0.00822   0.00274  -0.1178   0.4595   0.5479
   3.250   0.9223   0.00824   0.00283  -0.1179   0.4525   0.5815
   3.500   0.9508   0.00832   0.00293  -0.1180   0.4447   0.6130
   3.750   0.9798   0.00832   0.00302  -0.1181   0.4370   0.6427
   4.000   1.0078   0.00838   0.00316  -0.1181   0.4270   0.6930
   4.250   1.0355   0.00833   0.00332  -0.1180   0.4162   0.7848
   4.500   1.0599   0.00832   0.00348  -0.1171   0.4054   0.8689
   4.750   1.0815   0.00829   0.00356  -0.1155   0.3946   1.0000
   5.000   1.1095   0.00848   0.00370  -0.1155   0.3837   1.0000
   5.250   1.1369   0.00873   0.00387  -0.1154   0.3715   1.0000
   5.500   1.1641   0.00899   0.00405  -0.1154   0.3592   1.0000
   5.750   1.1913   0.00923   0.00424  -0.1153   0.3476   1.0000
   6.000   1.2178   0.00952   0.00445  -0.1151   0.3357   1.0000
   6.250   1.2440   0.00983   0.00468  -0.1149   0.3236   1.0000
   6.500   1.2705   0.01009   0.00490  -0.1147   0.3125   1.0000
   6.750   1.2962   0.01042   0.00515  -0.1144   0.3009   1.0000
   7.000   1.3211   0.01079   0.00544  -0.1140   0.2878   1.0000
   7.250   1.3456   0.01118   0.00575  -0.1136   0.2724   1.0000
   7.500   1.3689   0.01164   0.00610  -0.1130   0.2550   1.0000
   7.750   1.3911   0.01216   0.00650  -0.1122   0.2346   1.0000
   8.000   1.4092   0.01294   0.00708  -0.1109   0.2051   1.0000
   8.250   1.4198   0.01417   0.00801  -0.1087   0.1603   1.0000
   8.500   1.4078   0.01645   0.00980  -0.1033   0.0871   1.0000
   8.750   1.4174   0.01743   0.01071  -0.1010   0.0752   1.0000
   9.000   1.4311   0.01823   0.01150  -0.0993   0.0707   1.0000
   9.250   1.4471   0.01895   0.01222  -0.0981   0.0687   1.0000
   9.500   1.4619   0.01977   0.01306  -0.0968   0.0669   1.0000
   9.750   1.4757   0.02071   0.01400  -0.0955   0.0653   1.0000
  10.000   1.4886   0.02175   0.01506  -0.0943   0.0638   1.0000
  10.250   1.5038   0.02264   0.01599  -0.0933   0.0633   1.0000
  10.500   1.5184   0.02362   0.01699  -0.0923   0.0627   1.0000
  10.750   1.5321   0.02467   0.01809  -0.0913   0.0621   1.0000
  11.000   1.5446   0.02584   0.01929  -0.0903   0.0615   1.0000
  11.250   1.5562   0.02711   0.02060  -0.0892   0.0609   1.0000
  11.500   1.5667   0.02847   0.02200  -0.0882   0.0603   1.0000
  11.750   1.5759   0.02998   0.02355  -0.0871   0.0598   1.0000
  12.000   1.5838   0.03164   0.02525  -0.0861   0.0593   1.0000
  12.250   1.5901   0.03347   0.02712  -0.0851   0.0587   1.0000
  12.500   1.5944   0.03552   0.02923  -0.0840   0.0582   1.0000
  12.750   1.5964   0.03786   0.03164  -0.0831   0.0576   1.0000
  13.000   1.5966   0.04045   0.03430  -0.0821   0.0571   1.0000
  13.250   1.6023   0.04252   0.03643  -0.0815   0.0570   1.0000
  13.500   1.6074   0.04474   0.03871  -0.0809   0.0568   1.0000
  13.750   1.6116   0.04711   0.04115  -0.0804   0.0566   1.0000
  14.000   1.6147   0.04962   0.04372  -0.0799   0.0564   1.0000
  14.250   1.6175   0.05219   0.04636  -0.0795   0.0562   1.0000
  14.500   1.6194   0.05489   0.04913  -0.0791   0.0560   1.0000
  14.750   1.6201   0.05778   0.05208  -0.0788   0.0558   1.0000
  15.000   1.6206   0.06067   0.05504  -0.0785   0.0556   1.0000
  15.250   1.6207   0.06365   0.05809  -0.0783   0.0554   1.0000
  15.500   1.6202   0.06675   0.06126  -0.0781   0.0551   1.0000
  15.750   1.6208   0.06971   0.06428  -0.0780   0.0547   1.0000
  16.000   1.6198   0.07292   0.06755  -0.0779   0.0544   1.0000
  16.250   1.6193   0.07607   0.07076  -0.0779   0.0540   1.0000
  16.500   1.6178   0.07939   0.07414  -0.0780   0.0537   1.0000
  16.750   1.6159   0.08279   0.07760  -0.0781   0.0534   1.0000
  17.000   1.6142   0.08615   0.08101  -0.0782   0.0531   1.0000
  17.250   1.6112   0.08973   0.08466  -0.0785   0.0528   1.0000
  17.500   1.6089   0.09321   0.08819  -0.0788   0.0525   1.0000
  17.750   1.6045   0.09703   0.09207  -0.0792   0.0522   1.0000
  18.000   1.6017   0.10058   0.09566  -0.0796   0.0519   1.0000
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