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Glenn Martin 3 (glennmartin3-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: Glenn Martin 3 (glennmartin3-il)
Reynolds number: 100,000
Max Cl/Cd: 38.37 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-glennmartin3-il-100000-n5.txt
Download as CSV file: xf-glennmartin3-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.500  -0.4186   0.08417   0.07946  -0.0523   0.9716   0.0387
  -8.250  -0.4331   0.08041   0.07565  -0.0514   0.9661   0.0387
  -8.000  -0.4494   0.07472   0.06981  -0.0512   0.9596   0.0388
  -7.500  -0.4669   0.06527   0.05996  -0.0475   0.9477   0.0388
  -7.250  -0.4799   0.06078   0.05518  -0.0434   0.9398   0.0388
  -6.750  -0.4657   0.05698   0.05125  -0.0390   0.9295   0.0401
  -6.500  -0.4642   0.05288   0.04678  -0.0360   0.9249   0.0402
  -6.250  -0.4624   0.05103   0.04477  -0.0321   0.9187   0.0410
  -5.750  -0.4476   0.04519   0.03812  -0.0257   0.9101   0.0433
  -5.500  -0.4503   0.04320   0.03580  -0.0200   0.9023   0.0435
  -5.250  -0.4379   0.04090   0.03304  -0.0169   0.8981   0.0439
  -5.000  -0.4260   0.03871   0.03021  -0.0133   0.8937   0.0461
  -4.750  -0.4128   0.03775   0.02923  -0.0106   0.8863   0.0474
  -4.500  -0.3864   0.03623   0.02742  -0.0100   0.8819   0.0482
  -4.250  -0.3628   0.03484   0.02574  -0.0087   0.8767   0.0494
  -4.000  -0.3442   0.03374   0.02437  -0.0065   0.8695   0.0507
  -3.750  -0.3111   0.03256   0.02276  -0.0068   0.8653   0.0532
  -3.500  -0.2697   0.03109   0.02119  -0.0091   0.8626   0.0550
  -3.250  -0.2547   0.03049   0.02050  -0.0065   0.8531   0.0557
  -3.000  -0.2177   0.02957   0.01951  -0.0080   0.8489   0.0580
  -2.750  -0.1741   0.02861   0.01840  -0.0106   0.8459   0.0612
  -2.500  -0.1536   0.02807   0.01776  -0.0089   0.8358   0.0626
  -2.250  -0.1134   0.02702   0.01679  -0.0111   0.8313   0.0654
  -2.000  -0.0718   0.02615   0.01592  -0.0134   0.8283   0.0694
  -1.750  -0.0541   0.02588   0.01559  -0.0112   0.8181   0.0730
  -1.500  -0.0172   0.02509   0.01484  -0.0127   0.8135   0.0779
  -1.250   0.3274   0.02076   0.01391  -0.0791   0.8275   0.9362
  -1.000   0.3783   0.02167   0.01457  -0.0833   0.8150   1.0000
  -0.750   0.4058   0.02127   0.01400  -0.0827   0.8017   1.0000
  -0.500   0.4365   0.02085   0.01342  -0.0828   0.7886   1.0000
  -0.250   0.4628   0.02057   0.01300  -0.0821   0.7722   1.0000
   0.000   0.4837   0.02044   0.01274  -0.0804   0.7513   1.0000
   0.250   0.5104   0.02017   0.01233  -0.0798   0.7271   1.0000
   0.500   0.5428   0.01979   0.01175  -0.0802   0.6950   1.0000
   0.750   0.5965   0.01905   0.01062  -0.0847   0.6475   1.0000
   1.000   0.6421   0.01880   0.00989  -0.0879   0.5923   1.0000
   1.250   0.6689   0.01899   0.00971  -0.0877   0.5429   1.0000
   1.500   0.6885   0.01934   0.00971  -0.0860   0.4977   1.0000
   1.750   0.7058   0.01975   0.00979  -0.0840   0.4662   1.0000
   2.000   0.7238   0.02012   0.00994  -0.0822   0.4440   1.0000
   2.250   0.7420   0.02050   0.01011  -0.0804   0.4244   1.0000
   2.500   0.7605   0.02086   0.01032  -0.0788   0.4080   1.0000
   2.750   0.7792   0.02123   0.01054  -0.0772   0.3930   1.0000
   3.000   0.7978   0.02157   0.01078  -0.0756   0.3788   1.0000
   3.250   0.8157   0.02192   0.01105  -0.0738   0.3643   1.0000
   3.500   0.8336   0.02228   0.01131  -0.0721   0.3511   1.0000
   3.750   0.8509   0.02267   0.01159  -0.0703   0.3392   1.0000
   4.000   0.8685   0.02303   0.01189  -0.0686   0.3272   1.0000
   4.250   0.8859   0.02342   0.01221  -0.0669   0.3162   1.0000
   4.500   0.9029   0.02384   0.01253  -0.0651   0.3070   1.0000
   4.750   0.9217   0.02422   0.01288  -0.0636   0.2984   1.0000
   5.000   0.9388   0.02467   0.01324  -0.0619   0.2909   1.0000
   5.250   0.9580   0.02508   0.01362  -0.0607   0.2844   1.0000
   5.500   0.9762   0.02552   0.01403  -0.0592   0.2778   1.0000
   5.750   0.9942   0.02602   0.01443  -0.0578   0.2729   1.0000
   6.000   1.0138   0.02644   0.01489  -0.0566   0.2672   1.0000
   6.250   1.0330   0.02692   0.01536  -0.0554   0.2626   1.0000
   6.500   1.0512   0.02743   0.01582  -0.0541   0.2584   1.0000
   6.750   1.0709   0.02793   0.01631  -0.0531   0.2543   1.0000
   7.000   1.0906   0.02843   0.01685  -0.0521   0.2502   1.0000
   7.250   1.1100   0.02895   0.01739  -0.0511   0.2466   1.0000
   7.500   1.1299   0.02949   0.01794  -0.0502   0.2435   1.0000
   7.750   1.1512   0.03007   0.01847  -0.0495   0.2409   1.0000
   8.000   1.1722   0.03066   0.01911  -0.0489   0.2382   1.0000
   8.250   1.1918   0.03125   0.01982  -0.0480   0.2354   1.0000
   8.500   1.2113   0.03185   0.02050  -0.0471   0.2327   1.0000
   8.750   1.2291   0.03246   0.02116  -0.0460   0.2296   1.0000
   9.000   1.2493   0.03310   0.02184  -0.0453   0.2273   1.0000
   9.250   1.2704   0.03376   0.02249  -0.0448   0.2250   1.0000
   9.500   1.2923   0.03448   0.02325  -0.0445   0.2229   1.0000
   9.750   1.3086   0.03523   0.02417  -0.0432   0.2210   1.0000
  10.000   1.3252   0.03603   0.02514  -0.0420   0.2191   1.0000
  10.250   1.3414   0.03687   0.02612  -0.0408   0.2170   1.0000
  10.500   1.3575   0.03771   0.02708  -0.0396   0.2151   1.0000
  10.750   1.3730   0.03852   0.02799  -0.0384   0.2131   1.0000
  11.000   1.3896   0.03934   0.02890  -0.0373   0.2110   1.0000
  11.250   1.4089   0.04014   0.02975  -0.0368   0.2092   1.0000
  11.500   1.4325   0.04103   0.03067  -0.0370   0.2075   1.0000
  11.750   1.4383   0.04218   0.03204  -0.0344   0.2059   1.0000
  12.000   1.4409   0.04344   0.03356  -0.0314   0.2041   1.0000
  12.250   1.4439   0.04473   0.03507  -0.0287   0.2022   1.0000
  12.500   1.4465   0.04606   0.03660  -0.0260   0.2001   1.0000
  12.750   1.4509   0.04736   0.03808  -0.0237   0.1982   1.0000
  13.000   1.4572   0.04869   0.03956  -0.0217   0.1966   1.0000
  13.250   1.4662   0.04982   0.04082  -0.0201   0.1948   1.0000
  13.500   1.4794   0.05089   0.04196  -0.0192   0.1931   1.0000
  13.750   1.5012   0.05182   0.04291  -0.0193   0.1914   1.0000
  14.000   1.4902   0.05397   0.04533  -0.0157   0.1903   1.0000
  14.250   1.4688   0.05685   0.04853  -0.0116   0.1887   1.0000
  14.500   1.4453   0.06018   0.05215  -0.0080   0.1870   1.0000
  14.750   1.4210   0.06394   0.05617  -0.0051   0.1853   1.0000
  15.000   1.3946   0.06815   0.06062  -0.0027   0.1834   1.0000
  15.250   1.3721   0.07238   0.06504  -0.0012   0.1812   1.0000
  15.500   1.3363   0.07864   0.07152  -0.0004   0.1799   1.0000
  15.750   1.4361   0.07019   0.06274  -0.0013   0.1754   1.0000
  16.000   1.3764   0.07866   0.07156   0.0003   0.1747   1.0000
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