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Glenn Martin 2 (glennmartin2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: Glenn Martin 2 (glennmartin2-il)
Reynolds number: 1,000,000
Max Cl/Cd: 101.34 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-glennmartin2-il-1000000-n5.txt
Download as CSV file: xf-glennmartin2-il-1000000-n5.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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.3510   0.08424   0.08230  -0.0881   0.9759   0.0082
 -13.500  -0.6516   0.02606   0.02286  -0.1339   0.9379   0.0070
 -13.250  -0.6314   0.02310   0.01965  -0.1355   0.9324   0.0073
 -13.000  -0.6106   0.02145   0.01782  -0.1357   0.9258   0.0075
 -12.750  -0.5859   0.02011   0.01632  -0.1363   0.9203   0.0078
 -12.500  -0.5661   0.01912   0.01518  -0.1354   0.9134   0.0080
 -12.250  -0.5434   0.01821   0.01413  -0.1350   0.9061   0.0082
 -12.000  -0.5232   0.01744   0.01321  -0.1338   0.8967   0.0084
 -11.750  -0.5015   0.01676   0.01238  -0.1329   0.8874   0.0086
 -11.500  -0.4820   0.01620   0.01170  -0.1314   0.8790   0.0088
 -11.250  -0.4618   0.01557   0.01094  -0.1300   0.8716   0.0091
 -11.000  -0.4428   0.01495   0.01024  -0.1284   0.8646   0.0096
 -10.750  -0.4219   0.01443   0.00961  -0.1270   0.8572   0.0100
 -10.500  -0.4013   0.01402   0.00911  -0.1255   0.8473   0.0105
 -10.250  -0.3803   0.01363   0.00861  -0.1240   0.8371   0.0110
 -10.000  -0.3589   0.01327   0.00815  -0.1226   0.8275   0.0114
  -9.750  -0.3377   0.01288   0.00766  -0.1211   0.8174   0.0120
  -9.500  -0.3164   0.01254   0.00724  -0.1196   0.8057   0.0127
  -9.250  -0.2953   0.01225   0.00687  -0.1181   0.7923   0.0137
  -9.000  -0.2747   0.01202   0.00652  -0.1164   0.7731   0.0144
  -8.750  -0.2570   0.01188   0.00622  -0.1140   0.7401   0.0151
  -8.500  -0.2417   0.01181   0.00595  -0.1112   0.6969   0.0161
  -8.250  -0.2248   0.01179   0.00577  -0.1087   0.6622   0.0173
  -8.000  -0.2042   0.01168   0.00554  -0.1070   0.6443   0.0183
  -7.750  -0.1821   0.01157   0.00534  -0.1056   0.6319   0.0194
  -7.500  -0.1592   0.01140   0.00513  -0.1045   0.6238   0.0205
  -7.250  -0.1354   0.01127   0.00495  -0.1034   0.6173   0.0217
  -7.000  -0.1115   0.01113   0.00475  -0.1024   0.6108   0.0226
  -6.750  -0.0881   0.01103   0.00458  -0.1013   0.6040   0.0234
  -6.500  -0.0639   0.01090   0.00440  -0.1003   0.5967   0.0242
  -6.250  -0.0409   0.01072   0.00416  -0.0991   0.5897   0.0254
  -6.000  -0.0166   0.01057   0.00399  -0.0982   0.5833   0.0266
  -5.750   0.0074   0.01047   0.00385  -0.0973   0.5762   0.0279
  -5.500   0.0312   0.01036   0.00368  -0.0962   0.5685   0.0287
  -5.250   0.0545   0.01027   0.00352  -0.0951   0.5577   0.0293
  -5.000   0.0780   0.01020   0.00339  -0.0940   0.5452   0.0300
  -4.750   0.0993   0.01010   0.00320  -0.0924   0.5244   0.0318
  -4.500   0.1097   0.01043   0.00317  -0.0888   0.4379   0.0328
  -4.250   0.1283   0.01054   0.00312  -0.0868   0.4057   0.0339
  -4.000   0.1495   0.01057   0.00305  -0.0852   0.3878   0.0351
  -3.750   0.1715   0.01056   0.00297  -0.0839   0.3752   0.0364
  -3.500   0.1936   0.01056   0.00290  -0.0826   0.3647   0.0377
  -3.250   0.2161   0.01050   0.00282  -0.0813   0.3572   0.0414
  -3.000   0.2382   0.01048   0.00276  -0.0800   0.3500   0.0449
  -2.750   0.2609   0.01043   0.00273  -0.0788   0.3451   0.0517
  -2.500   0.2827   0.01041   0.00270  -0.0775   0.3399   0.0580
  -2.000   0.3256   0.01041   0.00266  -0.0746   0.3314   0.0666
  -1.750   0.3469   0.01038   0.00262  -0.0731   0.3282   0.0702
  -1.500   0.3682   0.01037   0.00260  -0.0716   0.3249   0.0737
  -1.250   0.3895   0.01038   0.00259  -0.0702   0.3214   0.0768
  -0.750   0.4330   0.01043   0.00259  -0.0675   0.3159   0.0801
  -0.500   0.4548   0.01043   0.00258  -0.0662   0.3139   0.0835
  -0.250   0.4764   0.01043   0.00259  -0.0649   0.3118   0.0878
   0.000   0.4980   0.01045   0.00262  -0.0636   0.3097   0.0926
   0.500   0.5407   0.01052   0.00269  -0.0609   0.3049   0.1070
   0.750   0.5610   0.01054   0.00275  -0.0593   0.3023   0.1266
   1.000   0.5798   0.01049   0.00286  -0.0576   0.3003   0.1924
   1.250   0.6018   0.01053   0.00294  -0.0564   0.2993   0.2093
   1.500   0.6239   0.01059   0.00302  -0.0553   0.2979   0.2205
   1.750   0.6460   0.01065   0.00311  -0.0542   0.2965   0.2297
   2.000   0.6681   0.01073   0.00319  -0.0531   0.2950   0.2369
   2.250   0.6896   0.01081   0.00328  -0.0519   0.2934   0.2432
   2.500   0.7112   0.01090   0.00338  -0.0507   0.2919   0.2487
   3.000   0.7537   0.01111   0.00360  -0.0484   0.2887   0.2606
   3.250   0.7748   0.01123   0.00372  -0.0472   0.2870   0.2669
   3.500   0.7953   0.01136   0.00385  -0.0459   0.2847   0.2720
   3.750   0.8173   0.01143   0.00396  -0.0449   0.2834   0.2793
   4.000   0.8389   0.01153   0.00408  -0.0439   0.2819   0.2872
   4.250   0.8603   0.01162   0.00421  -0.0428   0.2806   0.2980
   4.500   0.8814   0.01172   0.00435  -0.0417   0.2788   0.3120
   4.750   0.9019   0.01182   0.00450  -0.0406   0.2775   0.3297
   5.250   1.1180   0.01147   0.00563  -0.0779   0.2687   0.9952
   5.500   1.1567   0.01164   0.00579  -0.0808   0.2657   0.9977
   5.750   1.1977   0.01183   0.00597  -0.0843   0.2617   0.9995
   6.000   1.2215   0.01207   0.00616  -0.0840   0.2561   1.0000
   6.250   1.2394   0.01223   0.00632  -0.0824   0.2509   1.0000
   6.500   1.2568   0.01242   0.00651  -0.0807   0.2469   1.0000
   6.750   1.2724   0.01268   0.00674  -0.0787   0.2403   1.0000
   7.000   1.2870   0.01301   0.00699  -0.0766   0.2277   1.0000
   7.250   1.3017   0.01335   0.00728  -0.0746   0.2159   1.0000
   7.500   1.3049   0.01420   0.00791  -0.0707   0.1822   1.0000
   7.750   1.3035   0.01533   0.00882  -0.0661   0.1491   1.0000
   8.000   1.3130   0.01600   0.00942  -0.0635   0.1351   1.0000
   8.250   1.3120   0.01723   0.01044  -0.0593   0.1037   1.0000
   8.500   1.2891   0.01969   0.01255  -0.0521   0.0381   1.0000
   8.750   1.2920   0.02085   0.01368  -0.0490   0.0146   1.0000
   9.000   1.3051   0.02148   0.01433  -0.0473   0.0132   1.0000
   9.250   1.3173   0.02216   0.01505  -0.0456   0.0121   1.0000
   9.500   1.3290   0.02291   0.01583  -0.0440   0.0112   1.0000
   9.750   1.3403   0.02370   0.01666  -0.0423   0.0102   1.0000
  10.000   1.3515   0.02452   0.01752  -0.0407   0.0098   1.0000
  10.250   1.3623   0.02540   0.01843  -0.0392   0.0092   1.0000
  10.500   1.3721   0.02636   0.01943  -0.0376   0.0087   1.0000
  10.750   1.3810   0.02741   0.02053  -0.0361   0.0083   1.0000
  11.000   1.3883   0.02862   0.02179  -0.0345   0.0078   1.0000
  11.250   1.3968   0.02979   0.02301  -0.0331   0.0075   1.0000
  11.500   1.4045   0.03105   0.02432  -0.0317   0.0071   1.0000
  11.750   1.4113   0.03244   0.02575  -0.0305   0.0067   1.0000
  12.000   1.4173   0.03394   0.02731  -0.0292   0.0065   1.0000
  12.250   1.4224   0.03560   0.02902  -0.0281   0.0063   1.0000
  12.500   1.4245   0.03760   0.03108  -0.0270   0.0059   1.0000
  12.750   1.4273   0.03961   0.03316  -0.0260   0.0058   1.0000
  13.000   1.4304   0.04169   0.03531  -0.0253   0.0056   1.0000
  13.250   1.4301   0.04421   0.03792  -0.0246   0.0056   1.0000
  13.500   1.4318   0.04659   0.04037  -0.0241   0.0053   1.0000
  13.750   1.4319   0.04917   0.04303  -0.0237   0.0052   1.0000
  14.000   1.4293   0.05213   0.04607  -0.0233   0.0050   1.0000
  14.250   1.4282   0.05496   0.04896  -0.0231   0.0048   1.0000
  14.500   1.4236   0.05828   0.05237  -0.0230   0.0048   1.0000
  14.750   1.4178   0.06182   0.05599  -0.0230   0.0046   1.0000
  15.000   1.4096   0.06575   0.06002  -0.0232   0.0045   1.0000
  15.250   1.3976   0.07036   0.06473  -0.0236   0.0043   1.0000
  15.500   1.3876   0.07484   0.06933  -0.0242   0.0044   1.0000
  15.750   1.3727   0.08009   0.07470  -0.0250   0.0043   1.0000
  16.000   1.3588   0.08533   0.08004  -0.0259   0.0042   1.0000
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