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Glenn Martin 3 (glennmartin3-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: Glenn Martin 3 (glennmartin3-il)
Reynolds number: 200,000
Max Cl/Cd: 47.06 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-glennmartin3-il-200000-n5.txt
Download as CSV file: xf-glennmartin3-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Glenn Martin 3                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.2985   0.10347   0.09982  -0.0573   0.9750   0.0227
 -10.250  -0.3043   0.09747   0.09385  -0.0611   0.9716   0.0238
 -10.000  -0.3089   0.09082   0.08721  -0.0661   0.9692   0.0236
  -9.750  -0.2931   0.09104   0.08745  -0.0652   0.9658   0.0249
  -9.250  -0.3159   0.07840   0.07485  -0.0749   0.9566   0.0245
  -9.000  -0.3680   0.06676   0.06308  -0.0803   0.9481   0.0239
  -8.750  -0.3844   0.06456   0.06084  -0.0763   0.9396   0.0242
  -8.500  -0.4183   0.05752   0.05357  -0.0727   0.9308   0.0241
  -8.250  -0.4283   0.05252   0.04834  -0.0701   0.9257   0.0246
  -8.000  -0.4478   0.04800   0.04353  -0.0644   0.9178   0.0248
  -7.750  -0.4534   0.04415   0.03932  -0.0602   0.9130   0.0260
  -7.500  -0.4686   0.03955   0.03418  -0.0537   0.9071   0.0266
  -7.250  -0.4872   0.03510   0.02886  -0.0454   0.8997   0.0279
  -7.000  -0.4667   0.03378   0.02744  -0.0442   0.8972   0.0285
  -6.750  -0.4420   0.03273   0.02628  -0.0437   0.8954   0.0292
  -6.500  -0.4451   0.03165   0.02500  -0.0376   0.8864   0.0295
  -6.250  -0.4254   0.03038   0.02349  -0.0358   0.8832   0.0305
  -6.000  -0.4021   0.02874   0.02145  -0.0345   0.8809   0.0319
  -5.750  -0.3924   0.02758   0.01988  -0.0304   0.8749   0.0330
  -5.500  -0.3724   0.02657   0.01879  -0.0287   0.8697   0.0336
  -5.250  -0.3448   0.02557   0.01765  -0.0284   0.8669   0.0341
  -5.000  -0.3141   0.02486   0.01687  -0.0287   0.8647   0.0359
  -4.750  -0.2831   0.02396   0.01577  -0.0290   0.8634   0.0376
  -4.500  -0.2703   0.02348   0.01515  -0.0257   0.8556   0.0381
  -4.250  -0.2422   0.02274   0.01426  -0.0254   0.8522   0.0391
  -4.000  -0.2079   0.02181   0.01333  -0.0264   0.8497   0.0401
  -3.750  -0.1752   0.02120   0.01272  -0.0272   0.8479   0.0419
  -3.500  -0.1365   0.02034   0.01180  -0.0290   0.8462   0.0436
  -3.250  -0.1193   0.02004   0.01147  -0.0266   0.8385   0.0442
  -3.000  -0.0889   0.01948   0.01085  -0.0268   0.8342   0.0454
  -2.750  -0.0531   0.01876   0.01017  -0.0282   0.8312   0.0472
  -2.500  -0.0138   0.01807   0.00949  -0.0303   0.8288   0.0495
  -2.250   0.0054   0.01780   0.00920  -0.0282   0.8194   0.0514
  -2.000   0.0460   0.01707   0.00844  -0.0303   0.8128   0.0538
  -1.750   0.0759   0.01660   0.00796  -0.0304   0.8028   0.0569
  -1.500   0.1225   0.01591   0.00723  -0.0339   0.7930   0.0627
  -1.250   0.1494   0.01554   0.00685  -0.0334   0.7779   0.0710
  -1.000   0.1771   0.01522   0.00655  -0.0332   0.7644   0.0822
  -0.750   0.4956   0.01304   0.00714  -0.0970   0.7163   0.9590
  -0.500   0.5569   0.01371   0.00726  -0.1037   0.6431   0.9832
  -0.250   0.6025   0.01420   0.00720  -0.1076   0.5698   0.9929
   0.000   0.6410   0.01456   0.00710  -0.1102   0.5015   1.0000
   0.250   0.6479   0.01495   0.00721  -0.1059   0.4647   1.0000
   0.500   0.6594   0.01525   0.00730  -0.1027   0.4423   1.0000
   0.750   0.6730   0.01552   0.00741  -0.0999   0.4251   1.0000
   1.000   0.6875   0.01578   0.00753  -0.0973   0.4105   1.0000
   1.250   0.7032   0.01603   0.00766  -0.0949   0.3969   1.0000
   1.500   0.7197   0.01625   0.00779  -0.0927   0.3835   1.0000
   1.750   0.7361   0.01650   0.00793  -0.0905   0.3710   1.0000
   2.000   0.7520   0.01676   0.00808  -0.0882   0.3557   1.0000
   2.250   0.7691   0.01700   0.00822  -0.0862   0.3427   1.0000
   2.500   0.7866   0.01724   0.00838  -0.0843   0.3302   1.0000
   2.750   0.8034   0.01750   0.00855  -0.0823   0.3172   1.0000
   3.000   0.8199   0.01779   0.00875  -0.0802   0.3057   1.0000
   3.250   0.8367   0.01807   0.00895  -0.0782   0.2931   1.0000
   3.500   0.8538   0.01837   0.00917  -0.0763   0.2829   1.0000
   3.750   0.8701   0.01870   0.00942  -0.0743   0.2738   1.0000
   4.000   0.8879   0.01899   0.00967  -0.0726   0.2662   1.0000
   4.250   0.9045   0.01934   0.00995  -0.0706   0.2589   1.0000
   4.500   0.9219   0.01967   0.01023  -0.0689   0.2526   1.0000
   4.750   0.9394   0.02000   0.01053  -0.0672   0.2466   1.0000
   5.000   0.9553   0.02041   0.01087  -0.0652   0.2410   1.0000
   5.250   0.9734   0.02073   0.01118  -0.0637   0.2371   1.0000
   5.500   0.9915   0.02107   0.01153  -0.0622   0.2326   1.0000
   5.750   1.0089   0.02145   0.01189  -0.0605   0.2289   1.0000
   6.000   1.0257   0.02186   0.01226  -0.0589   0.2258   1.0000
   6.250   1.0427   0.02229   0.01266  -0.0572   0.2229   1.0000
   6.500   1.0614   0.02264   0.01306  -0.0559   0.2204   1.0000
   6.750   1.0798   0.02301   0.01345  -0.0546   0.2175   1.0000
   7.000   1.0978   0.02342   0.01387  -0.0532   0.2151   1.0000
   7.250   1.1151   0.02385   0.01431  -0.0518   0.2125   1.0000
   7.500   1.1322   0.02433   0.01479  -0.0504   0.2104   1.0000
   7.750   1.1493   0.02483   0.01527  -0.0490   0.2082   1.0000
   8.000   1.1677   0.02529   0.01575  -0.0478   0.2063   1.0000
   8.250   1.1862   0.02571   0.01625  -0.0466   0.2044   1.0000
   8.500   1.2041   0.02615   0.01676  -0.0455   0.2024   1.0000
   8.750   1.2212   0.02662   0.01727  -0.0442   0.1999   1.0000
   9.000   1.2390   0.02712   0.01783  -0.0430   0.1983   1.0000
   9.250   1.2562   0.02763   0.01838  -0.0418   0.1966   1.0000
   9.500   1.2736   0.02817   0.01895  -0.0406   0.1951   1.0000
   9.750   1.2909   0.02873   0.01953  -0.0396   0.1936   1.0000
  10.000   1.3094   0.02931   0.02013  -0.0387   0.1923   1.0000
  10.250   1.3281   0.02990   0.02076  -0.0379   0.1907   1.0000
  10.500   1.3446   0.03046   0.02144  -0.0367   0.1895   1.0000
  10.750   1.3602   0.03105   0.02214  -0.0354   0.1880   1.0000
  11.000   1.3754   0.03167   0.02288  -0.0341   0.1863   1.0000
  11.250   1.3909   0.03231   0.02363  -0.0329   0.1848   1.0000
  11.500   1.4062   0.03298   0.02439  -0.0317   0.1833   1.0000
  11.750   1.4201   0.03367   0.02516  -0.0304   0.1817   1.0000
  12.000   1.4337   0.03438   0.02597  -0.0290   0.1800   1.0000
  12.250   1.4468   0.03512   0.02676  -0.0277   0.1784   1.0000
  12.500   1.4612   0.03589   0.02753  -0.0266   0.1762   1.0000
  12.750   1.4692   0.03680   0.02859  -0.0247   0.1740   1.0000
  13.000   1.4779   0.03773   0.02969  -0.0229   0.1721   1.0000
  13.250   1.4845   0.03871   0.03083  -0.0210   0.1695   1.0000
  13.500   1.4914   0.03974   0.03196  -0.0193   0.1669   1.0000
  13.750   1.4977   0.04080   0.03312  -0.0176   0.1644   1.0000
  14.000   1.5046   0.04190   0.03423  -0.0160   0.1620   1.0000
  14.250   1.5086   0.04323   0.03568  -0.0143   0.1591   1.0000
  14.500   1.5137   0.04459   0.03724  -0.0129   0.1569   1.0000
  14.750   1.5180   0.04603   0.03885  -0.0115   0.1543   1.0000
  15.000   1.5223   0.04754   0.04049  -0.0101   0.1521   1.0000
  15.250   1.5237   0.04924   0.04226  -0.0088   0.1490   1.0000
  15.500   1.5260   0.05096   0.04402  -0.0077   0.1467   1.0000
  15.750   1.5275   0.05294   0.04622  -0.0067   0.1440   1.0000
  16.000   1.5268   0.05518   0.04868  -0.0058   0.1400   1.0000
  16.250   1.5267   0.05741   0.05104  -0.0051   0.1373   1.0000
  16.500   1.5228   0.06011   0.05379  -0.0045   0.1338   1.0000
  16.750   1.5217   0.06271   0.05659  -0.0042   0.1311   1.0000
  17.000   1.5146   0.06613   0.06019  -0.0041   0.1249   1.0000
  17.250   1.5058   0.06983   0.06397  -0.0043   0.1212   1.0000
  17.500   1.4998   0.07335   0.06770  -0.0045   0.1176   1.0000
  17.750   1.4867   0.07795   0.07244  -0.0053   0.1122   1.0000
  18.000   1.4694   0.08332   0.07794  -0.0064   0.1071   1.0000
  18.250   1.4425   0.09036   0.08509  -0.0083   0.0996   1.0000
  18.500   1.4203   0.09682   0.09171  -0.0103   0.0974   1.0000
  18.750   1.3888   0.10496   0.10001  -0.0129   0.0940   1.0000
  19.000   1.3565   0.11339   0.10863  -0.0157   0.0938   1.0000
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