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GOE 776 AIRFOIL (goe776-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 776 AIRFOIL (goe776-il)
Reynolds number: 1,000,000
Max Cl/Cd: 66.32 at α=9.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe776-il-1000000.txt
Download as CSV file: xf-goe776-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 776 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.2945   0.07811   0.07350  -0.0449   1.0000   0.0900
 -19.500  -1.2920   0.07549   0.07082  -0.0455   1.0000   0.0914
 -19.250  -1.3006   0.07166   0.06694  -0.0463   1.0000   0.0931
 -19.000  -1.3073   0.06803   0.06328  -0.0469   1.0000   0.0949
 -18.750  -1.3079   0.06515   0.06035  -0.0474   1.0000   0.0966
 -18.500  -1.3075   0.06237   0.05752  -0.0479   1.0000   0.0982
 -18.250  -1.3020   0.06018   0.05527  -0.0482   1.0000   0.0994
 -18.000  -1.3078   0.05684   0.05190  -0.0485   1.0000   0.1013
 -17.750  -1.3104   0.05385   0.04887  -0.0488   1.0000   0.1030
 -17.500  -1.3082   0.05140   0.04639  -0.0489   1.0000   0.1048
 -17.250  -1.3042   0.04916   0.04410  -0.0490   1.0000   0.1065
 -17.000  -1.2963   0.04733   0.04221  -0.0491   1.0000   0.1079
 -16.750  -1.2972   0.04470   0.03955  -0.0489   1.0000   0.1100
 -16.500  -1.2956   0.04233   0.03716  -0.0488   1.0000   0.1120
 -16.250  -1.2900   0.04038   0.03519  -0.0486   1.0000   0.1140
 -16.000  -1.2821   0.03866   0.03343  -0.0484   1.0000   0.1158
 -15.750  -1.2727   0.03712   0.03184  -0.0481   1.0000   0.1174
 -15.500  -1.2696   0.03509   0.02980  -0.0475   1.0000   0.1199
 -15.250  -1.2638   0.03333   0.02802  -0.0470   1.0000   0.1222
 -15.000  -1.2547   0.03189   0.02657  -0.0464   1.0000   0.1244
 -14.750  -1.2438   0.03066   0.02530  -0.0458   1.0000   0.1263
 -14.500  -1.2369   0.02920   0.02382  -0.0449   1.0000   0.1287
 -14.250  -1.2304   0.02783   0.02245  -0.0437   1.0000   0.1314
 -14.000  -1.2232   0.02665   0.02126  -0.0423   1.0000   0.1340
 -13.750  -1.2150   0.02574   0.02033  -0.0406   1.0000   0.1363
 -13.500  -1.2116   0.02477   0.01934  -0.0383   1.0000   0.1386
 -13.250  -1.2140   0.02378   0.01835  -0.0349   1.0000   0.1413
 -13.000  -1.2178   0.02303   0.01759  -0.0309   1.0000   0.1438
 -12.750  -1.1929   0.02215   0.01670  -0.0320   0.9986   0.1472
 -12.500  -1.1686   0.02119   0.01575  -0.0331   0.9966   0.1513
 -12.250  -1.1437   0.02027   0.01485  -0.0343   0.9946   0.1556
 -12.000  -1.1146   0.01960   0.01417  -0.0358   0.9930   0.1595
 -11.750  -1.0884   0.01870   0.01331  -0.0372   0.9915   0.1647
 -11.500  -1.0609   0.01799   0.01261  -0.0384   0.9895   0.1694
 -11.250  -1.0349   0.01737   0.01199  -0.0391   0.9851   0.1739
 -11.000  -1.0106   0.01664   0.01130  -0.0396   0.9802   0.1794
 -10.750  -0.9831   0.01611   0.01077  -0.0404   0.9758   0.1842
 -10.500  -0.9666   0.01555   0.01022  -0.0390   0.9659   0.1891
 -10.250  -0.9486   0.01501   0.00969  -0.0379   0.9572   0.1945
 -10.000  -0.9304   0.01465   0.00930  -0.0365   0.9464   0.1988
  -9.750  -0.9151   0.01414   0.00880  -0.0347   0.9356   0.2046
  -9.500  -0.8978   0.01374   0.00838  -0.0331   0.9239   0.2099
  -9.250  -0.8772   0.01344   0.00806  -0.0320   0.9127   0.2143
  -9.000  -0.8603   0.01302   0.00763  -0.0304   0.9003   0.2204
  -8.750  -0.8400   0.01271   0.00731  -0.0293   0.8885   0.2258
  -8.500  -0.8187   0.01246   0.00701  -0.0282   0.8764   0.2307
  -8.250  -0.7991   0.01212   0.00668  -0.0270   0.8637   0.2371
  -8.000  -0.7774   0.01188   0.00640  -0.0260   0.8513   0.2426
  -7.750  -0.7554   0.01165   0.00614  -0.0251   0.8380   0.2480
  -7.500  -0.7345   0.01139   0.00588  -0.0240   0.8254   0.2546
  -7.250  -0.7116   0.01122   0.00565  -0.0232   0.8114   0.2603
  -7.000  -0.6894   0.01100   0.00542  -0.0222   0.7986   0.2664
  -6.750  -0.6674   0.01081   0.00520  -0.0212   0.7846   0.2728
  -6.500  -0.6432   0.01067   0.00503  -0.0206   0.7717   0.2782
  -6.250  -0.6216   0.01048   0.00482  -0.0194   0.7585   0.2851
  -6.000  -0.5987   0.01032   0.00465  -0.0185   0.7452   0.2918
  -5.750  -0.5744   0.01024   0.00452  -0.0179   0.7325   0.2968
  -5.500  -0.5540   0.01009   0.00435  -0.0164   0.7195   0.3040
  -5.250  -0.5326   0.00999   0.00424  -0.0152   0.7077   0.3106
  -5.000  -0.5096   0.00995   0.00415  -0.0141   0.6950   0.3158
  -4.750  -0.4889   0.00982   0.00403  -0.0127   0.6841   0.3235
  -4.500  -0.4649   0.00974   0.00393  -0.0119   0.6726   0.3301
  -4.250  -0.4402   0.00969   0.00384  -0.0113   0.6616   0.3361
  -4.000  -0.4170   0.00957   0.00374  -0.0104   0.6506   0.3443
  -3.750  -0.3923   0.00953   0.00367  -0.0097   0.6400   0.3515
  -3.500  -0.3675   0.00944   0.00359  -0.0090   0.6300   0.3589
  -3.250  -0.3438   0.00939   0.00351  -0.0082   0.6185   0.3668
  -3.000  -0.3172   0.00934   0.00346  -0.0078   0.6096   0.3731
  -2.750  -0.2933   0.00927   0.00339  -0.0070   0.5990   0.3813
  -2.500  -0.2680   0.00921   0.00333  -0.0064   0.5893   0.3891
  -2.250  -0.2417   0.00920   0.00329  -0.0060   0.5787   0.3952
  -2.000  -0.2178   0.00914   0.00323  -0.0052   0.5687   0.4041
  -1.750  -0.1918   0.00910   0.00319  -0.0048   0.5585   0.4119
  -1.500  -0.1668   0.00910   0.00316  -0.0041   0.5473   0.4194
  -1.250  -0.1414   0.00903   0.00312  -0.0035   0.5378   0.4285
  -1.000  -0.1160   0.00906   0.00310  -0.0030   0.5261   0.4359
  -0.750  -0.0906   0.00899   0.00307  -0.0024   0.5167   0.4453
  -0.500  -0.0657   0.00901   0.00306  -0.0017   0.5054   0.4545
  -0.250  -0.0397   0.00899   0.00304  -0.0013   0.4960   0.4632
   0.000  -0.0150   0.00898   0.00303  -0.0006   0.4855   0.4733
   0.250   0.0111   0.00900   0.00304  -0.0002   0.4760   0.4821
   0.500   0.0357   0.00897   0.00304   0.0006   0.4663   0.4930
   0.750   0.0615   0.00902   0.00306   0.0011   0.4569   0.5022
   1.000   0.0866   0.00899   0.00306   0.0017   0.4484   0.5137
   1.250   0.1115   0.00905   0.00309   0.0023   0.4383   0.5235
   1.500   0.1372   0.00903   0.00311   0.0029   0.4312   0.5347
   1.750   0.1627   0.00907   0.00315   0.0034   0.4224   0.5450
   2.000   0.1874   0.00910   0.00319   0.0041   0.4141   0.5554
   2.250   0.2135   0.00912   0.00322   0.0045   0.4069   0.5663
   2.500   0.2382   0.00918   0.00327   0.0052   0.3983   0.5759
   2.750   0.2635   0.00921   0.00332   0.0058   0.3914   0.5867
   3.000   0.2896   0.00926   0.00337   0.0062   0.3841   0.5960
   3.250   0.3130   0.00932   0.00344   0.0071   0.3755   0.6070
   3.500   0.3394   0.00937   0.00350   0.0075   0.3694   0.6165
   3.750   0.3639   0.00941   0.00357   0.0082   0.3619   0.6274
   4.000   0.3876   0.00952   0.00366   0.0091   0.3536   0.6379
   4.250   0.4132   0.00955   0.00372   0.0096   0.3474   0.6480
   4.500   0.4369   0.00964   0.00381   0.0104   0.3397   0.6593
   4.750   0.4609   0.00973   0.00391   0.0112   0.3325   0.6699
   5.000   0.4852   0.00979   0.00400   0.0119   0.3263   0.6818
   5.250   0.5073   0.00990   0.00411   0.0131   0.3192   0.6924
   5.500   0.5288   0.00997   0.00422   0.0143   0.3131   0.7052
   5.750   0.5511   0.01005   0.00432   0.0154   0.3068   0.7168
   6.000   0.5715   0.01019   0.00447   0.0169   0.2998   0.7300
   6.250   0.5950   0.01030   0.00462   0.0177   0.2942   0.7424
   6.500   0.6185   0.01043   0.00478   0.0185   0.2880   0.7561
   6.750   0.6399   0.01063   0.00499   0.0196   0.2807   0.7690
   7.000   0.6638   0.01077   0.00516   0.0203   0.2753   0.7826
   7.250   0.6866   0.01093   0.00537   0.0212   0.2691   0.7962
   7.750   0.7314   0.01134   0.00582   0.0230   0.2571   0.8229
   8.000   0.7531   0.01158   0.00607   0.0240   0.2507   0.8357
   8.250   0.7739   0.01184   0.00636   0.0251   0.2445   0.8493
   8.500   0.7966   0.01205   0.00661   0.0259   0.2395   0.8614
   8.750   0.8168   0.01236   0.00692   0.0271   0.2334   0.8744
   9.000   0.8370   0.01266   0.00725   0.0283   0.2277   0.8864
   9.250   0.8582   0.01294   0.00755   0.0292   0.2226   0.8984
   9.500   0.8760   0.01332   0.00795   0.0308   0.2168   0.9105
   9.750   0.8954   0.01367   0.00831   0.0320   0.2117   0.9222
  10.000   0.9137   0.01403   0.00870   0.0334   0.2067   0.9336
  10.250   0.9293   0.01452   0.00918   0.0352   0.2010   0.9446
  10.500   0.9471   0.01492   0.00959   0.0366   0.1965   0.9555
  10.750   0.9654   0.01540   0.01007   0.0378   0.1914   0.9644
  11.000   0.9808   0.01602   0.01067   0.0393   0.1858   0.9746
  11.250   1.0080   0.01650   0.01116   0.0387   0.1816   0.9795
  11.500   1.0333   0.01715   0.01179   0.0381   0.1764   0.9844
  11.750   1.0579   0.01786   0.01248   0.0375   0.1714   0.9891
  12.000   1.0862   0.01849   0.01311   0.0362   0.1670   0.9914
  12.250   1.1132   0.01934   0.01392   0.0348   0.1619   0.9928
  12.500   1.1414   0.02007   0.01465   0.0334   0.1577   0.9945
  12.750   1.1679   0.02090   0.01547   0.0321   0.1535   0.9964
  13.000   1.1909   0.02194   0.01649   0.0310   0.1489   0.9984
  13.250   1.2176   0.02277   0.01733   0.0297   0.1456   1.0000
  13.500   1.2153   0.02347   0.01805   0.0335   0.1432   1.0000
  13.750   1.2140   0.02438   0.01896   0.0368   0.1405   1.0000
  14.000   1.2143   0.02550   0.02008   0.0395   0.1375   1.0000
  14.250   1.2234   0.02636   0.02096   0.0411   0.1355   1.0000
  14.500   1.2322   0.02743   0.02205   0.0424   0.1330   1.0000
  14.750   1.2401   0.02870   0.02332   0.0435   0.1303   1.0000
  15.000   1.2448   0.03031   0.02493   0.0445   0.1274   1.0000
  15.250   1.2566   0.03148   0.02614   0.0451   0.1255   1.0000
  15.500   1.2661   0.03288   0.02757   0.0457   0.1233   1.0000
  15.750   1.2736   0.03449   0.02919   0.0462   0.1210   1.0000
  16.000   1.2782   0.03638   0.03110   0.0467   0.1185   1.0000
  16.250   1.2845   0.03821   0.03296   0.0470   0.1166   1.0000
  16.500   1.2939   0.03978   0.03457   0.0472   0.1148   1.0000
  16.750   1.2995   0.04173   0.03656   0.0474   0.1128   1.0000
  17.000   1.3025   0.04396   0.03880   0.0476   0.1108   1.0000
  17.250   1.3024   0.04651   0.04137   0.0477   0.1086   1.0000
  17.500   1.3082   0.04856   0.04348   0.0477   0.1070   1.0000
  17.750   1.3139   0.05062   0.04558   0.0476   0.1053   1.0000
  18.000   1.3154   0.05314   0.04814   0.0475   0.1035   1.0000
  18.250   1.3137   0.05604   0.05107   0.0472   0.1017   1.0000
  18.500   1.3085   0.05929   0.05436   0.0469   0.0998   1.0000
  18.750   1.3127   0.06163   0.05676   0.0466   0.0985   1.0000
  19.000   1.3147   0.06423   0.05942   0.0462   0.0969   1.0000
  19.250   1.3131   0.06725   0.06247   0.0457   0.0952   1.0000
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