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GOE 723 AIRFOIL (goe723-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 723 AIRFOIL (goe723-il)
Reynolds number: 200,000
Max Cl/Cd: 79.19 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe723-il-200000-n5.txt
Download as CSV file: xf-goe723-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 723 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.3362   0.10565   0.10179  -0.0459   1.0000   0.0461
 -10.000  -0.3379   0.10177   0.09796  -0.0467   1.0000   0.0464
  -9.750  -0.3272   0.09986   0.09607  -0.0449   1.0000   0.0470
  -9.500  -0.3188   0.09814   0.09439  -0.0436   1.0000   0.0478
  -9.000  -0.3524   0.08590   0.08226  -0.0480   1.0000   0.0393
  -8.750  -0.3272   0.08402   0.08035  -0.0497   0.9957   0.0381
  -8.500  -0.3139   0.07970   0.07603  -0.0540   0.9860   0.0373
  -8.250  -0.3065   0.07469   0.07104  -0.0590   0.9705   0.0367
  -8.000  -0.3026   0.06842   0.06476  -0.0661   0.9503   0.0369
  -7.750  -0.3189   0.03970   0.03519  -0.1040   0.9201   0.0344
  -7.500  -0.2979   0.03402   0.02888  -0.1098   0.9069   0.0343
  -7.250  -0.2716   0.03067   0.02507  -0.1129   0.8952   0.0343
  -7.000  -0.2442   0.02816   0.02215  -0.1149   0.8835   0.0345
  -6.750  -0.2188   0.02629   0.01996  -0.1157   0.8703   0.0347
  -6.500  -0.1930   0.02490   0.01829  -0.1162   0.8579   0.0354
  -6.250  -0.1673   0.02361   0.01672  -0.1164   0.8463   0.0360
  -6.000  -0.1428   0.02238   0.01520  -0.1162   0.8342   0.0364
  -5.750  -0.1187   0.02126   0.01381  -0.1157   0.8226   0.0365
  -5.500  -0.0936   0.02028   0.01258  -0.1153   0.8122   0.0367
  -5.250  -0.0689   0.01942   0.01151  -0.1148   0.8017   0.0370
  -5.000  -0.0438   0.01865   0.01057  -0.1142   0.7918   0.0373
  -4.750  -0.0183   0.01796   0.00970  -0.1137   0.7825   0.0376
  -4.500   0.0068   0.01735   0.00897  -0.1131   0.7732   0.0379
  -4.250   0.0326   0.01682   0.00830  -0.1126   0.7651   0.0383
  -4.000   0.0578   0.01635   0.00774  -0.1120   0.7564   0.0387
  -3.750   0.0831   0.01580   0.00712  -0.1114   0.7487   0.0395
  -3.500   0.1076   0.01529   0.00661  -0.1108   0.7405   0.0405
  -3.250   0.1329   0.01489   0.00618  -0.1102   0.7333   0.0413
  -3.000   0.1582   0.01454   0.00580  -0.1096   0.7262   0.0419
  -2.750   0.1835   0.01424   0.00544  -0.1090   0.7188   0.0425
  -2.500   0.2093   0.01398   0.00511  -0.1085   0.7123   0.0433
  -2.250   0.2348   0.01374   0.00483  -0.1079   0.7051   0.0442
  -2.000   0.2611   0.01357   0.00456  -0.1074   0.6989   0.0452
  -1.750   0.2872   0.01340   0.00434  -0.1069   0.6923   0.0464
  -1.500   0.3131   0.01320   0.00410  -0.1064   0.6855   0.0485
  -1.250   0.3397   0.01308   0.00390  -0.1060   0.6800   0.0520
  -1.000   0.3656   0.01292   0.00376  -0.1055   0.6730   0.0573
  -0.750   0.3915   0.01268   0.00360  -0.1050   0.6667   0.0801
  -0.500   0.4153   0.01209   0.00356  -0.1044   0.6607   0.2400
  -0.250   0.4405   0.01191   0.00361  -0.1039   0.6535   0.3117
   0.250   0.4914   0.01178   0.00368  -0.1026   0.6380   0.4039
   0.500   0.5170   0.01175   0.00369  -0.1020   0.6310   0.4411
   0.750   0.5423   0.01170   0.00376  -0.1013   0.6238   0.4768
   1.000   0.5674   0.01165   0.00383  -0.1006   0.6172   0.5217
   1.250   0.5928   0.01159   0.00388  -0.1000   0.6113   0.5683
   1.500   0.6179   0.01152   0.00395  -0.0992   0.6044   0.6091
   1.750   0.6441   0.01141   0.00398  -0.0987   0.5984   0.6657
   2.250   0.7493   0.01107   0.00412  -0.1092   0.5835   1.0000
   2.500   0.7751   0.01121   0.00421  -0.1087   0.5771   1.0000
   2.750   0.8007   0.01134   0.00432  -0.1081   0.5698   1.0000
   3.000   0.8261   0.01149   0.00440  -0.1075   0.5625   1.0000
   3.250   0.8509   0.01163   0.00451  -0.1067   0.5529   1.0000
   3.500   0.8752   0.01177   0.00462  -0.1059   0.5421   1.0000
   3.750   0.8991   0.01193   0.00471  -0.1049   0.5299   1.0000
   4.000   0.9225   0.01209   0.00482  -0.1039   0.5164   1.0000
   4.250   0.9464   0.01226   0.00499  -0.1030   0.5045   1.0000
   4.500   0.9701   0.01245   0.00515  -0.1021   0.4932   1.0000
   4.750   0.9934   0.01266   0.00532  -0.1011   0.4812   1.0000
   5.000   1.0163   0.01287   0.00552  -0.1001   0.4677   1.0000
   5.250   1.0382   0.01311   0.00572  -0.0988   0.4510   1.0000
   5.500   1.0590   0.01339   0.00593  -0.0974   0.4296   1.0000
   5.750   1.0794   0.01370   0.00619  -0.0960   0.4088   1.0000
   6.000   1.0989   0.01406   0.00647  -0.0944   0.3884   1.0000
   6.250   1.1177   0.01446   0.00679  -0.0927   0.3667   1.0000
   6.500   1.1353   0.01492   0.00716  -0.0908   0.3441   1.0000
   6.750   1.1512   0.01546   0.00760  -0.0887   0.3191   1.0000
   7.000   1.1652   0.01609   0.00809  -0.0863   0.2905   1.0000
   7.250   1.1770   0.01683   0.00866  -0.0836   0.2521   1.0000
   7.500   1.1736   0.01831   0.00963  -0.0788   0.1658   1.0000
   7.750   1.1691   0.01978   0.01073  -0.0737   0.1173   1.0000
   8.000   1.1760   0.02071   0.01160  -0.0705   0.1010   1.0000
   8.250   1.1865   0.02148   0.01238  -0.0679   0.0900   1.0000
   8.500   1.1965   0.02231   0.01321  -0.0654   0.0823   1.0000
   8.750   1.2067   0.02316   0.01407  -0.0630   0.0769   1.0000
   9.000   1.2159   0.02409   0.01503  -0.0607   0.0733   1.0000
   9.250   1.2257   0.02504   0.01604  -0.0586   0.0703   1.0000
   9.500   1.2343   0.02611   0.01716  -0.0565   0.0678   1.0000
   9.750   1.2413   0.02734   0.01842  -0.0544   0.0658   1.0000
  10.000   1.2463   0.02878   0.01991  -0.0524   0.0641   1.0000
  10.250   1.2529   0.03019   0.02139  -0.0506   0.0627   1.0000
  10.500   1.2603   0.03161   0.02291  -0.0491   0.0614   1.0000
  10.750   1.2674   0.03311   0.02449  -0.0477   0.0599   1.0000
  11.000   1.2736   0.03473   0.02619  -0.0463   0.0584   1.0000
  11.250   1.2792   0.03646   0.02798  -0.0450   0.0570   1.0000
  11.500   1.2832   0.03837   0.02993  -0.0438   0.0555   1.0000
  11.750   1.2847   0.04055   0.03213  -0.0425   0.0540   1.0000
  12.000   1.2914   0.04230   0.03398  -0.0416   0.0527   1.0000
  12.250   1.2989   0.04401   0.03580  -0.0407   0.0513   1.0000
  12.500   1.3057   0.04580   0.03768  -0.0399   0.0498   1.0000
  12.750   1.3115   0.04771   0.03966  -0.0390   0.0484   1.0000
  13.000   1.3167   0.04970   0.04172  -0.0383   0.0471   1.0000
  13.250   1.3208   0.05181   0.04388  -0.0376   0.0460   1.0000
  13.500   1.3239   0.05402   0.04608  -0.0367   0.0447   1.0000
  13.750   1.3310   0.05596   0.04818  -0.0362   0.0435   1.0000
  14.000   1.3371   0.05802   0.05037  -0.0358   0.0421   1.0000
  14.250   1.3423   0.06019   0.05264  -0.0354   0.0408   1.0000
  14.500   1.3467   0.06249   0.05502  -0.0351   0.0395   1.0000
  14.750   1.3503   0.06492   0.05751  -0.0350   0.0384   1.0000
  15.000   1.3530   0.06742   0.06003  -0.0347   0.0374   1.0000
  15.250   1.3577   0.06985   0.06264  -0.0346   0.0362   1.0000
  15.500   1.3612   0.07243   0.06536  -0.0346   0.0349   1.0000
  15.750   1.3638   0.07517   0.06821  -0.0348   0.0336   1.0000
  16.000   1.3659   0.07801   0.07114  -0.0351   0.0327   1.0000
  16.250   1.3669   0.08105   0.07424  -0.0355   0.0319   1.0000
  16.500   1.3683   0.08402   0.07731  -0.0358   0.0311   1.0000
  16.750   1.3696   0.08708   0.08054  -0.0361   0.0299   1.0000
  17.000   1.3698   0.09036   0.08396  -0.0368   0.0288   1.0000
  17.250   1.3694   0.09381   0.08752  -0.0376   0.0279   1.0000
  17.500   1.3687   0.09732   0.09111  -0.0386   0.0273   1.0000
  17.750   1.3673   0.10100   0.09487  -0.0398   0.0267   1.0000
  18.000   1.3653   0.10474   0.09874  -0.0407   0.0259   1.0000
  18.250   1.3627   0.10865   0.10283  -0.0418   0.0251   1.0000
  18.500   1.3594   0.11275   0.10709  -0.0432   0.0244   1.0000
  18.750   1.3558   0.11698   0.11145  -0.0448   0.0238   1.0000
  19.000   1.3521   0.12129   0.11587  -0.0467   0.0233   1.0000
  19.250   1.3484   0.12568   0.12035  -0.0487   0.0228   1.0000
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