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Glenn Martin 2 (glennmartin2-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: Glenn Martin 2 (glennmartin2-il)
Reynolds number: 200,000
Max Cl/Cd: 58.68 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-glennmartin2-il-200000.txt
Download as CSV file: xf-glennmartin2-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Glenn Martin 2                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.2262   0.11373   0.11062  -0.0402   0.9882   0.0499
 -10.000  -0.2238   0.10984   0.10675  -0.0495   0.9840   0.0526
  -9.750  -0.2248   0.10600   0.10294  -0.0568   0.9771   0.0530
  -9.500  -0.2061   0.10010   0.09704  -0.0588   0.9742   0.0537
  -9.250  -0.1756   0.09652   0.09342  -0.0590   0.9725   0.0552
  -9.000  -0.1586   0.09335   0.09025  -0.0612   0.9672   0.0575
  -8.750  -0.0527   0.07271   0.06975  -0.0803   0.9456   0.0650
  -8.500  -0.0256   0.06856   0.06558  -0.0827   0.9437   0.0671
  -8.250  -0.0224   0.06548   0.06251  -0.0833   0.9346   0.0692
  -8.000  -0.1376   0.07584   0.07274  -0.0821   0.9358   0.0650
  -7.750  -0.1114   0.07258   0.06947  -0.0839   0.9321   0.0669
  -7.500  -0.0856   0.06831   0.06514  -0.0893   0.9290   0.0699
  -7.250  -0.0833   0.06301   0.05951  -0.0980   0.9152   0.0754
  -7.000  -0.0818   0.05761   0.05409  -0.0974   0.9059   0.0766
  -6.750  -0.0528   0.05527   0.05181  -0.0979   0.9029   0.0786
  -6.500  -0.0210   0.05199   0.04845  -0.1011   0.9000   0.0817
  -6.250  -0.0413   0.03842   0.03407  -0.1004   0.8863   0.0614
  -6.000  -0.0202   0.03240   0.02746  -0.1014   0.8827   0.0604
  -5.750  -0.0159   0.02918   0.02379  -0.0973   0.8707   0.0606
  -5.500   0.0144   0.02566   0.01961  -0.0979   0.8670   0.0617
  -5.250   0.0283   0.02430   0.01781  -0.0946   0.8551   0.0637
  -5.000   0.0619   0.02208   0.01542  -0.0959   0.8493   0.0663
  -4.750   0.0868   0.02103   0.01422  -0.0949   0.8385   0.0687
  -4.500   0.1130   0.02015   0.01312  -0.0941   0.8277   0.0723
  -4.250   0.1504   0.01923   0.01184  -0.0953   0.8197   0.0755
  -4.000   0.1731   0.01779   0.01030  -0.0941   0.8070   0.0789
  -3.750   0.1994   0.01722   0.00968  -0.0934   0.7947   0.0843
  -3.500   0.2285   0.01672   0.00896  -0.0931   0.7827   0.0894
  -3.250   0.2593   0.01562   0.00785  -0.0936   0.7704   0.0971
  -3.000   0.2871   0.01505   0.00716  -0.0932   0.7561   0.1067
  -2.750   0.3124   0.01451   0.00662  -0.0924   0.7404   0.1176
  -2.500   0.3365   0.01404   0.00612  -0.0914   0.7237   0.1284
  -2.250   0.3603   0.01375   0.00577  -0.0902   0.7060   0.1401
  -2.000   0.3841   0.01355   0.00552  -0.0891   0.6876   0.1535
  -1.750   0.4073   0.01345   0.00538  -0.0880   0.6685   0.1719
  -1.500   0.4302   0.01345   0.00533  -0.0867   0.6484   0.1997
  -1.250   0.4498   0.01356   0.00542  -0.0847   0.6267   0.2401
  -1.000   0.4677   0.01375   0.00547  -0.0824   0.6027   0.2736
  -0.750   0.4823   0.01387   0.00547  -0.0795   0.5746   0.2951
  -0.500   0.4944   0.01393   0.00542  -0.0761   0.5407   0.3108
  -0.250   0.5053   0.01404   0.00534  -0.0725   0.5053   0.3243
   0.000   0.5167   0.01415   0.00529  -0.0692   0.4786   0.3364
   0.250   0.5302   0.01430   0.00530  -0.0663   0.4606   0.3492
   0.500   0.5461   0.01441   0.00535  -0.0639   0.4481   0.3662
   0.750   0.5635   0.01453   0.00543  -0.0619   0.4391   0.3893
   1.000   0.5783   0.01427   0.00550  -0.0594   0.4314   0.4953
   1.250   0.8357   0.01533   0.00702  -0.1088   0.4112   1.0000
   1.500   0.8587   0.01564   0.00720  -0.1080   0.4069   1.0000
   1.750   0.8797   0.01587   0.00738  -0.1068   0.4029   1.0000
   2.000   0.9012   0.01612   0.00757  -0.1057   0.3988   1.0000
   2.250   0.9241   0.01643   0.00777  -0.1050   0.3950   1.0000
   2.500   0.9495   0.01681   0.00802  -0.1048   0.3916   1.0000
   2.750   0.9700   0.01704   0.00826  -0.1035   0.3886   1.0000
   3.000   0.9917   0.01730   0.00852  -0.1025   0.3856   1.0000
   3.250   1.0144   0.01760   0.00878  -0.1017   0.3828   1.0000
   3.500   1.0383   0.01792   0.00905  -0.1012   0.3801   1.0000
   3.750   1.0644   0.01832   0.00937  -0.1012   0.3776   1.0000
   4.000   1.0903   0.01876   0.00978  -0.1012   0.3752   1.0000
   4.250   1.1094   0.01903   0.01012  -0.0997   0.3727   1.0000
   4.500   1.1295   0.01933   0.01046  -0.0984   0.3698   1.0000
   4.750   1.1510   0.01966   0.01080  -0.0975   0.3669   1.0000
   5.000   1.1736   0.02000   0.01111  -0.0968   0.3637   1.0000
   5.250   1.2018   0.02054   0.01153  -0.0973   0.3602   1.0000
   5.500   1.2174   0.02083   0.01192  -0.0952   0.3572   1.0000
   5.750   1.2339   0.02111   0.01230  -0.0933   0.3538   1.0000
   6.000   1.2536   0.02145   0.01267  -0.0921   0.3508   1.0000
   6.250   1.2759   0.02183   0.01306  -0.0914   0.3482   1.0000
   6.500   1.3014   0.02228   0.01349  -0.0914   0.3457   1.0000
   6.750   1.3261   0.02285   0.01407  -0.0914   0.3428   1.0000
   7.000   1.3356   0.02307   0.01444  -0.0881   0.3391   1.0000
   7.250   1.3480   0.02326   0.01469  -0.0854   0.3344   1.0000
   7.500   1.3683   0.02346   0.01480  -0.0844   0.3293   1.0000
   7.750   1.3801   0.02380   0.01522  -0.0817   0.3249   1.0000
   8.000   1.3875   0.02400   0.01553  -0.0782   0.3204   1.0000
   8.250   1.3996   0.02413   0.01565  -0.0755   0.3154   1.0000
   8.500   1.4175   0.02445   0.01593  -0.0741   0.3107   1.0000
   8.750   1.4164   0.02465   0.01629  -0.0689   0.3070   1.0000
   9.000   1.4197   0.02480   0.01652  -0.0647   0.3026   1.0000
   9.250   1.4280   0.02489   0.01658  -0.0615   0.2977   1.0000
   9.500   1.4276   0.02514   0.01692  -0.0569   0.2922   1.0000
   9.750   1.4281   0.02539   0.01728  -0.0526   0.2866   1.0000
  10.000   1.4354   0.02566   0.01754  -0.0497   0.2816   1.0000
  10.250   1.4383   0.02613   0.01816  -0.0462   0.2762   1.0000
  10.500   1.4412   0.02660   0.01874  -0.0429   0.2701   1.0000
  10.750   1.4448   0.02715   0.01930  -0.0400   0.2636   1.0000
  11.000   1.4471   0.02785   0.02015  -0.0370   0.2550   1.0000
  11.250   1.4495   0.02868   0.02104  -0.0343   0.2444   1.0000
  11.500   1.4534   0.02963   0.02205  -0.0320   0.2343   1.0000
  11.750   1.4568   0.03076   0.02322  -0.0299   0.2196   1.0000
  12.000   1.4582   0.03216   0.02461  -0.0278   0.2027   1.0000
  12.250   1.4536   0.03409   0.02646  -0.0254   0.1850   1.0000
  12.500   1.4391   0.03699   0.02921  -0.0227   0.1644   1.0000
  12.750   1.4275   0.03995   0.03212  -0.0206   0.1487   1.0000
  13.000   1.4190   0.04288   0.03505  -0.0191   0.1364   1.0000
  13.250   1.4090   0.04616   0.03834  -0.0179   0.1235   1.0000
  13.500   1.3964   0.04990   0.04209  -0.0170   0.1099   1.0000
  13.750   1.3756   0.05475   0.04690  -0.0163   0.0923   1.0000
  14.000   1.3516   0.06025   0.05240  -0.0161   0.0744   1.0000
  14.250   1.3230   0.06661   0.05877  -0.0163   0.0584   1.0000
  14.500   1.3026   0.07230   0.06454  -0.0170   0.0490   1.0000
  14.750   1.2764   0.07905   0.07136  -0.0180   0.0382   1.0000
  15.000   1.2544   0.08547   0.07786  -0.0193   0.0334   1.0000
  15.250   1.2378   0.09122   0.08372  -0.0205   0.0309   1.0000
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