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GOE 423 AIRFOIL (goe423-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 423 AIRFOIL (goe423-il)
Reynolds number: 1,000,000
Max Cl/Cd: 124.53 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe423-il-1000000-n5.txt
Download as CSV file: xf-goe423-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 423 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
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -1.0959   0.04449   0.04125  -0.1159   1.0000   0.0319
 -17.750  -1.1063   0.03930   0.03593  -0.1205   0.9971   0.0321
 -17.500  -1.1020   0.03563   0.03213  -0.1247   0.9901   0.0324
 -17.250  -1.0941   0.03286   0.02925  -0.1277   0.9833   0.0326
 -17.000  -1.0865   0.03068   0.02695  -0.1293   0.9762   0.0329
 -16.500  -1.0708   0.02755   0.02360  -0.1296   0.9604   0.0334
 -16.250  -1.0624   0.02636   0.02231  -0.1288   0.9528   0.0337
 -16.000  -1.0527   0.02534   0.02119  -0.1278   0.9449   0.0339
 -15.750  -1.0415   0.02448   0.02022  -0.1265   0.9374   0.0341
 -15.500  -1.0294   0.02366   0.01930  -0.1252   0.9291   0.0343
 -15.250  -1.0190   0.02279   0.01835  -0.1236   0.9217   0.0346
 -15.000  -1.0045   0.02215   0.01766  -0.1223   0.9135   0.0350
 -14.750  -0.9891   0.02168   0.01712  -0.1208   0.9048   0.0353
 -14.500  -0.9702   0.02123   0.01662  -0.1198   0.8951   0.0356
 -14.250  -0.9507   0.02078   0.01609  -0.1190   0.8855   0.0359
 -14.000  -0.9311   0.02032   0.01553  -0.1180   0.8738   0.0361
 -13.750  -0.9110   0.01984   0.01496  -0.1172   0.8616   0.0364
 -13.500  -0.8900   0.01943   0.01445  -0.1164   0.8496   0.0367
 -13.000  -0.8468   0.01858   0.01340  -0.1151   0.8279   0.0373
 -12.750  -0.8251   0.01815   0.01286  -0.1144   0.8163   0.0376
 -12.500  -0.8027   0.01773   0.01234  -0.1137   0.8047   0.0378
 -12.250  -0.7799   0.01733   0.01184  -0.1132   0.7946   0.0380
 -12.000  -0.7570   0.01697   0.01137  -0.1126   0.7823   0.0382
 -11.750  -0.7334   0.01663   0.01093  -0.1120   0.7674   0.0384
 -11.500  -0.7099   0.01637   0.01053  -0.1115   0.7472   0.0386
 -11.250  -0.6889   0.01596   0.00997  -0.1105   0.7140   0.0390
 -11.000  -0.6675   0.01573   0.00954  -0.1096   0.6716   0.0393
 -10.750  -0.6446   0.01550   0.00918  -0.1089   0.6464   0.0396
 -10.500  -0.6206   0.01525   0.00884  -0.1084   0.6321   0.0399
 -10.000  -0.5710   0.01477   0.00822  -0.1076   0.6136   0.0405
  -9.750  -0.5459   0.01454   0.00792  -0.1072   0.6065   0.0408
  -9.500  -0.5206   0.01431   0.00763  -0.1068   0.6006   0.0411
  -9.250  -0.4949   0.01406   0.00734  -0.1065   0.5960   0.0414
  -9.000  -0.4691   0.01384   0.00707  -0.1062   0.5911   0.0418
  -8.750  -0.4433   0.01364   0.00681  -0.1059   0.5863   0.0422
  -8.500  -0.4175   0.01344   0.00656  -0.1056   0.5819   0.0426
  -8.250  -0.3913   0.01322   0.00629  -0.1054   0.5784   0.0429
  -8.000  -0.3650   0.01301   0.00604  -0.1052   0.5746   0.0431
  -7.750  -0.3388   0.01283   0.00581  -0.1049   0.5706   0.0434
  -7.500  -0.3126   0.01264   0.00557  -0.1046   0.5668   0.0436
  -7.000  -0.2609   0.01215   0.00503  -0.1040   0.5611   0.0446
  -6.750  -0.2343   0.01196   0.00483  -0.1038   0.5586   0.0450
  -6.500  -0.2075   0.01180   0.00464  -0.1036   0.5559   0.0455
  -6.250  -0.1808   0.01165   0.00447  -0.1035   0.5531   0.0460
  -6.000  -0.1539   0.01152   0.00431  -0.1033   0.5503   0.0465
  -5.750  -0.1271   0.01140   0.00417  -0.1031   0.5475   0.0471
  -5.250  -0.0732   0.01116   0.00387  -0.1028   0.5430   0.0481
  -5.000  -0.0459   0.01103   0.00373  -0.1027   0.5412   0.0485
  -4.750  -0.0186   0.01092   0.00360  -0.1026   0.5392   0.0489
  -4.500   0.0083   0.01078   0.00345  -0.1024   0.5370   0.0495
  -4.250   0.0351   0.01064   0.00330  -0.1022   0.5347   0.0503
  -4.000   0.0621   0.01053   0.00318  -0.1021   0.5323   0.0511
  -3.750   0.0891   0.01045   0.00308  -0.1019   0.5299   0.0519
  -3.500   0.1160   0.01037   0.00299  -0.1017   0.5275   0.0527
  -3.250   0.1432   0.01030   0.00291  -0.1016   0.5256   0.0536
  -3.000   0.1708   0.01023   0.00284  -0.1016   0.5244   0.0545
  -2.750   0.1985   0.01016   0.00276  -0.1015   0.5230   0.0552
  -2.500   0.2258   0.01006   0.00268  -0.1014   0.5214   0.0565
  -2.250   0.2532   0.00998   0.00261  -0.1014   0.5198   0.0579
  -2.000   0.2806   0.00992   0.00255  -0.1013   0.5182   0.0594
  -1.750   0.3080   0.00987   0.00251  -0.1012   0.5165   0.0609
  -1.500   0.3354   0.00983   0.00246  -0.1012   0.5149   0.0625
  -1.250   0.3625   0.00977   0.00242  -0.1010   0.5132   0.0655
  -1.000   0.3896   0.00973   0.00240  -0.1009   0.5116   0.0692
  -0.750   0.4165   0.00969   0.00238  -0.1008   0.5098   0.0754
  -0.500   0.4432   0.00965   0.00237  -0.1006   0.5080   0.0860
  -0.250   0.4703   0.00954   0.00236  -0.1006   0.5070   0.1104
   0.000   0.4976   0.00946   0.00237  -0.1005   0.5058   0.1297
   0.250   0.5252   0.00943   0.00238  -0.1005   0.5045   0.1414
   0.500   0.5527   0.00940   0.00239  -0.1005   0.5033   0.1528
   0.750   0.5800   0.00936   0.00240  -0.1005   0.5020   0.1661
   1.000   0.6070   0.00929   0.00242  -0.1004   0.5006   0.1900
   1.250   0.6332   0.00915   0.00246  -0.1002   0.4993   0.2533
   1.500   0.6597   0.00907   0.00250  -0.1001   0.4980   0.2983
   1.750   0.6848   0.00883   0.00254  -0.0998   0.4967   0.3943
   2.000   0.7082   0.00848   0.00263  -0.0992   0.4953   0.5517
   2.250   0.7329   0.00833   0.00270  -0.0987   0.4937   0.6303
   2.500   0.7551   0.00808   0.00280  -0.0976   0.4917   0.7458
   2.750   0.7766   0.00785   0.00293  -0.0962   0.4897   0.8628
   3.000   0.8043   0.00780   0.00306  -0.0960   0.4875   0.9257
   3.250   0.8402   0.00789   0.00318  -0.0978   0.4843   0.9542
   3.500   0.8753   0.00800   0.00328  -0.0995   0.4804   0.9690
   3.750   0.9083   0.00816   0.00339  -0.1008   0.4747   0.9791
   4.000   0.9450   0.00825   0.00348  -0.1028   0.4683   0.9849
   4.250   0.9806   0.00839   0.00358  -0.1047   0.4616   0.9902
   4.500   1.0138   0.00853   0.00369  -0.1061   0.4558   0.9935
   4.750   1.0531   0.00866   0.00380  -0.1089   0.4478   0.9963
   5.000   1.0946   0.00885   0.00395  -0.1122   0.4397   0.9995
   5.250   1.1183   0.00898   0.00405  -0.1115   0.4307   1.0000
   5.500   1.1338   0.00915   0.00417  -0.1091   0.4179   1.0000
   5.750   1.1425   0.00950   0.00438  -0.1055   0.3905   1.0000
   6.000   1.1389   0.01004   0.00472  -0.0993   0.3533   1.0000
   6.250   1.1353   0.01076   0.00522  -0.0934   0.3151   1.0000
   6.500   1.1394   0.01148   0.00576  -0.0892   0.2826   1.0000
   6.750   1.1461   0.01221   0.00633  -0.0857   0.2523   1.0000
   7.000   1.1536   0.01299   0.00695  -0.0825   0.2230   1.0000
   7.250   1.1557   0.01405   0.00781  -0.0786   0.1865   1.0000
   7.500   1.1374   0.01616   0.00954  -0.0721   0.1144   1.0000
   7.750   1.1384   0.01750   0.01075  -0.0686   0.0839   1.0000
   8.000   1.1347   0.01923   0.01231  -0.0649   0.0459   1.0000
   8.250   1.1469   0.02013   0.01320  -0.0633   0.0400   1.0000
   8.500   1.1604   0.02101   0.01407  -0.0619   0.0372   1.0000
   8.750   1.1739   0.02191   0.01498  -0.0607   0.0354   1.0000
   9.000   1.1880   0.02280   0.01589  -0.0595   0.0342   1.0000
   9.250   1.2009   0.02379   0.01690  -0.0583   0.0332   1.0000
   9.500   1.2131   0.02487   0.01799  -0.0571   0.0323   1.0000
   9.750   1.2245   0.02604   0.01918  -0.0559   0.0314   1.0000
  10.000   1.2364   0.02721   0.02038  -0.0549   0.0308   1.0000
  10.250   1.2480   0.02842   0.02162  -0.0539   0.0304   1.0000
  10.500   1.2593   0.02971   0.02294  -0.0529   0.0300   1.0000
  10.750   1.2697   0.03110   0.02437  -0.0520   0.0296   1.0000
  11.000   1.2795   0.03260   0.02590  -0.0511   0.0292   1.0000
  11.250   1.2887   0.03418   0.02751  -0.0502   0.0288   1.0000
  11.500   1.2973   0.03584   0.02921  -0.0494   0.0284   1.0000
  11.750   1.3054   0.03759   0.03100  -0.0486   0.0281   1.0000
  12.000   1.3129   0.03944   0.03288  -0.0479   0.0277   1.0000
  12.250   1.3194   0.04142   0.03490  -0.0472   0.0274   1.0000
  12.500   1.3247   0.04351   0.03704  -0.0464   0.0271   1.0000
  12.750   1.3312   0.04550   0.03907  -0.0458   0.0268   1.0000
  13.000   1.3386   0.04741   0.04103  -0.0452   0.0267   1.0000
  13.250   1.3456   0.04938   0.04305  -0.0447   0.0264   1.0000
  13.500   1.3524   0.05136   0.04507  -0.0441   0.0262   1.0000
  13.750   1.3582   0.05346   0.04722  -0.0436   0.0260   1.0000
  14.000   1.3640   0.05555   0.04935  -0.0431   0.0258   1.0000
  14.250   1.3692   0.05771   0.05156  -0.0426   0.0256   1.0000
  14.500   1.3743   0.05993   0.05382  -0.0421   0.0253   1.0000
  14.750   1.3797   0.06209   0.05603  -0.0417   0.0251   1.0000
  15.000   1.3838   0.06445   0.05843  -0.0413   0.0249   1.0000
  15.250   1.3888   0.06666   0.06069  -0.0409   0.0247   1.0000
  15.500   1.3925   0.06908   0.06316  -0.0406   0.0245   1.0000
  15.750   1.3966   0.07147   0.06559  -0.0403   0.0243   1.0000
  16.000   1.4008   0.07384   0.06800  -0.0401   0.0240   1.0000
  16.250   1.4027   0.07653   0.07074  -0.0399   0.0238   1.0000
  16.500   1.4052   0.07911   0.07337  -0.0396   0.0236   1.0000
  16.750   1.4052   0.08204   0.07635  -0.0395   0.0233   1.0000
  17.000   1.4051   0.08500   0.07937  -0.0394   0.0231   1.0000
  17.250   1.4094   0.08744   0.08186  -0.0393   0.0230   1.0000
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