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GOE 511 AIRFOIL (goe511-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 511 AIRFOIL (goe511-il)
Reynolds number: 1,000,000
Max Cl/Cd: 87.34 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe511-il-1000000.txt
Download as CSV file: xf-goe511-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 511 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
  ------ -------- --------- --------- -------- -------- --------
 -13.000   0.1989   0.09482   0.09291  -0.1402   0.9517   0.0247
 -12.750   0.2111   0.09285   0.09093  -0.1404   0.9472   0.0249
 -12.500   0.1323   0.09936   0.09738  -0.1380   0.9572   0.0247
 -12.250   0.1535   0.09708   0.09509  -0.1403   0.9558   0.0249
 -12.000   0.1651   0.09512   0.09313  -0.1409   0.9515   0.0251
 -11.750   0.1759   0.09308   0.09109  -0.1417   0.9468   0.0254
 -11.500   0.1909   0.09024   0.08823  -0.1445   0.9432   0.0257
 -11.250   0.2075   0.08731   0.08528  -0.1478   0.9407   0.0264
 -11.000   0.1886   0.07907   0.07703  -0.1537   0.9369   0.0284
 -10.750   0.1962   0.07710   0.07505  -0.1538   0.9308   0.0286
 -10.500   0.2119   0.07479   0.07273  -0.1560   0.9271   0.0287
 -10.250   0.2355   0.07311   0.07101  -0.1586   0.9226   0.0290
 -10.000   0.2406   0.07136   0.06927  -0.1582   0.9151   0.0292
  -9.750   0.2557   0.06871   0.06659  -0.1612   0.9094   0.0296
  -9.500   0.2667   0.06626   0.06412  -0.1633   0.9027   0.0303
  -9.250   0.2401   0.05461   0.05244  -0.1763   0.8934   0.0327
  -9.000   0.2381   0.05124   0.04903  -0.1793   0.8838   0.0328
  -8.750   0.2456   0.04973   0.04746  -0.1795   0.8724   0.0330
  -8.500   0.2404   0.04821   0.04589  -0.1771   0.8569   0.0332
  -8.250   0.2284   0.04634   0.04393  -0.1737   0.8323   0.0334
  -8.000   0.2096   0.04480   0.04208  -0.1682   0.7692   0.0335
  -7.750   0.1970   0.04413   0.04116  -0.1625   0.7256   0.0338
  -7.500  -0.0116   0.01794   0.01310  -0.1364   0.7340   0.0299
  -7.250  -0.0095   0.01759   0.01257  -0.1310   0.7116   0.0301
  -7.000  -0.0069   0.01718   0.01200  -0.1257   0.6940   0.0303
  -6.750  -0.0015   0.01678   0.01144  -0.1210   0.6771   0.0305
  -6.500   0.0060   0.01635   0.01085  -0.1167   0.6595   0.0308
  -6.250   0.0126   0.01597   0.01030  -0.1122   0.6389   0.0312
  -6.000   0.0198   0.01553   0.00969  -0.1078   0.6174   0.0313
  -5.750   0.0283   0.01517   0.00914  -0.1037   0.5943   0.0315
  -5.500   0.0392   0.01491   0.00870  -0.1001   0.5741   0.0317
  -5.250   0.0521   0.01463   0.00828  -0.0968   0.5591   0.0319
  -5.000   0.0673   0.01438   0.00789  -0.0941   0.5468   0.0321
  -4.750   0.0855   0.01410   0.00751  -0.0919   0.5378   0.0322
  -4.500   0.1036   0.01397   0.00727  -0.0897   0.5290   0.0324
  -4.250   0.1218   0.01324   0.00646  -0.0877   0.5222   0.0329
  -4.000   0.1418   0.01295   0.00613  -0.0859   0.5157   0.0332
  -3.750   0.1605   0.01279   0.00591  -0.0839   0.5089   0.0335
  -3.500   0.1811   0.01266   0.00576  -0.0823   0.5030   0.0339
  -3.250   0.2028   0.01256   0.00563  -0.0809   0.4978   0.0346
  -3.000   0.2230   0.01245   0.00546  -0.0791   0.4915   0.0349
  -2.750   0.2433   0.01237   0.00533  -0.0774   0.4859   0.0354
  -2.500   0.2660   0.01222   0.00516  -0.0762   0.4816   0.0358
  -2.250   0.2876   0.01210   0.00501  -0.0748   0.4767   0.0362
  -2.000   0.3078   0.01205   0.00491  -0.0730   0.4712   0.0366
  -1.750   0.3285   0.01201   0.00484  -0.0714   0.4660   0.0370
  -1.500   0.3494   0.01175   0.00457  -0.0699   0.4618   0.0376
  -1.250   0.3703   0.01165   0.00446  -0.0683   0.4564   0.0384
  -1.000   0.3904   0.01164   0.00441  -0.0667   0.4507   0.0391
  -0.750   0.4122   0.01161   0.00437  -0.0653   0.4458   0.0397
  -0.500   0.4341   0.01157   0.00431  -0.0640   0.4401   0.0407
  -0.250   0.4543   0.01159   0.00428  -0.0624   0.4340   0.0414
   0.000   0.4742   0.01157   0.00423  -0.0607   0.4283   0.0427
   0.250   0.4955   0.01154   0.00421  -0.0593   0.4228   0.0443
   0.500   0.5155   0.01157   0.00421  -0.0577   0.4166   0.0456
   0.750   0.5356   0.01164   0.00424  -0.0561   0.4106   0.0473
   1.000   0.5567   0.01161   0.00421  -0.0547   0.4052   0.0497
   1.250   0.5765   0.01167   0.00424  -0.0531   0.3988   0.0529
   1.500   0.5953   0.01172   0.00428  -0.0512   0.3929   0.0595
   1.750   0.6118   0.01153   0.00432  -0.0490   0.3881   0.1299
   2.000   0.6294   0.01156   0.00450  -0.0471   0.3824   0.1997
   2.250   0.6483   0.01172   0.00465  -0.0454   0.3761   0.2124
   2.500   0.6706   0.01183   0.00475  -0.0444   0.3722   0.2200
   2.750   0.6914   0.01195   0.00487  -0.0431   0.3675   0.2281
   3.000   0.7110   0.01212   0.00502  -0.0416   0.3625   0.2346
   3.250   0.7309   0.01231   0.00518  -0.0402   0.3581   0.2401
   3.500   0.7521   0.01241   0.00531  -0.0390   0.3545   0.2473
   3.750   0.7728   0.01256   0.00546  -0.0378   0.3513   0.2529
   4.000   0.7925   0.01276   0.00562  -0.0364   0.3471   0.2575
   4.250   0.8114   0.01297   0.00582  -0.0349   0.3431   0.2646
   4.500   0.8325   0.01312   0.00599  -0.0339   0.3407   0.2721
   4.750   0.8544   0.01326   0.00614  -0.0329   0.3385   0.2774
   5.000   0.8751   0.01341   0.00633  -0.0318   0.3360   0.2863
   5.250   0.8955   0.01360   0.00652  -0.0307   0.3337   0.2952
   5.500   0.9152   0.01380   0.00675  -0.0295   0.3309   0.3111
   5.750   1.1293   0.01354   0.00806  -0.0712   0.3232   0.9900
   6.000   1.1825   0.01391   0.00841  -0.0771   0.3201   0.9960
   6.250   1.2359   0.01423   0.00869  -0.0831   0.3176   0.9991
   6.500   1.2673   0.01451   0.00896  -0.0846   0.3150   1.0000
   6.750   1.2822   0.01481   0.00924  -0.0825   0.3125   1.0000
   7.000   1.2969   0.01515   0.00955  -0.0804   0.3102   1.0000
   7.250   1.3131   0.01544   0.00983  -0.0787   0.3076   1.0000
   7.500   1.3310   0.01566   0.01008  -0.0772   0.3063   1.0000
   7.750   1.3486   0.01590   0.01034  -0.0757   0.3048   1.0000
   8.000   1.3661   0.01616   0.01062  -0.0743   0.3034   1.0000
   8.250   1.3834   0.01644   0.01091  -0.0728   0.3019   1.0000
   8.500   1.4002   0.01675   0.01123  -0.0713   0.3002   1.0000
   8.750   1.4153   0.01713   0.01160  -0.0695   0.2978   1.0000
   9.000   1.4295   0.01756   0.01202  -0.0677   0.2951   1.0000
   9.250   1.4434   0.01803   0.01248  -0.0658   0.2927   1.0000
   9.500   1.4600   0.01840   0.01287  -0.0644   0.2913   1.0000
   9.750   1.4778   0.01871   0.01322  -0.0633   0.2901   1.0000
  10.000   1.4950   0.01906   0.01361  -0.0620   0.2888   1.0000
  10.250   1.5122   0.01942   0.01400  -0.0608   0.2873   1.0000
  10.500   1.5292   0.01980   0.01440  -0.0596   0.2858   1.0000
  10.750   1.5445   0.02026   0.01488  -0.0582   0.2840   1.0000
  11.000   1.5591   0.02076   0.01540  -0.0568   0.2821   1.0000
  11.250   1.5730   0.02133   0.01597  -0.0553   0.2799   1.0000
  11.500   1.5839   0.02205   0.01670  -0.0534   0.2769   1.0000
  11.750   1.5988   0.02260   0.01728  -0.0522   0.2753   1.0000
  12.000   1.6165   0.02301   0.01774  -0.0513   0.2736   1.0000
  12.250   1.6330   0.02350   0.01827  -0.0504   0.2714   1.0000
  12.500   1.6474   0.02411   0.01891  -0.0492   0.2691   1.0000
  12.750   1.6604   0.02481   0.01963  -0.0479   0.2660   1.0000
  13.000   1.6701   0.02573   0.02055  -0.0463   0.2626   1.0000
  13.250   1.6813   0.02659   0.02144  -0.0449   0.2599   1.0000
  13.500   1.6974   0.02717   0.02208  -0.0442   0.2576   1.0000
  13.750   1.7108   0.02794   0.02290  -0.0432   0.2542   1.0000
  14.000   1.7221   0.02887   0.02384  -0.0420   0.2509   1.0000
  14.250   1.7266   0.03028   0.02525  -0.0403   0.2457   1.0000
  14.500   1.7400   0.03111   0.02613  -0.0395   0.2419   1.0000
  14.750   1.7493   0.03225   0.02730  -0.0384   0.2371   1.0000
  15.000   1.7505   0.03403   0.02907  -0.0368   0.2307   1.0000
  15.250   1.7591   0.03529   0.03037  -0.0358   0.2246   1.0000
  15.500   1.7585   0.03730   0.03238  -0.0342   0.2175   1.0000
  15.750   1.7596   0.03923   0.03433  -0.0329   0.2096   1.0000
  16.000   1.7510   0.04202   0.03710  -0.0312   0.1996   1.0000
  16.250   1.7407   0.04506   0.04014  -0.0295   0.1909   1.0000
  16.500   1.7322   0.04805   0.04315  -0.0282   0.1838   1.0000
  16.750   1.7163   0.05185   0.04696  -0.0267   0.1770   1.0000
  17.000   1.7089   0.05491   0.05007  -0.0259   0.1724   1.0000
  17.250   1.6962   0.05863   0.05383  -0.0250   0.1679   1.0000
  17.500   1.6787   0.06293   0.05817  -0.0242   0.1632   1.0000
  17.750   1.6743   0.06588   0.06120  -0.0238   0.1609   1.0000
  18.000   1.6656   0.06932   0.06470  -0.0234   0.1578   1.0000
  18.250   1.6520   0.07338   0.06881  -0.0231   0.1549   1.0000
  18.500   1.6355   0.07784   0.07333  -0.0229   0.1520   1.0000
  18.750   1.6243   0.08173   0.07728  -0.0228   0.1497   1.0000
  19.000   1.6209   0.08471   0.08034  -0.0228   0.1475   1.0000
  19.250   1.6111   0.08852   0.08421  -0.0230   0.1452   1.0000
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