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Glenn Martin 2 (glennmartin2-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: Glenn Martin 2 (glennmartin2-il)
Reynolds number: 100,000
Max Cl/Cd: 46.23 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-glennmartin2-il-100000.txt
Download as CSV file: xf-glennmartin2-il-100000.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 =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.250  -0.3268   0.11958   0.11567  -0.0214   1.0000   0.0887
  -9.000  -0.3537   0.11968   0.11588  -0.0210   1.0000   0.0892
  -8.750  -0.3788   0.11932   0.11563  -0.0201   0.9997   0.0894
  -8.500  -0.3534   0.11214   0.10845  -0.0245   0.9942   0.0908
  -8.250  -0.3062   0.10621   0.10246  -0.0252   0.9894   0.0946
  -8.000  -0.2850   0.10213   0.09835  -0.0309   0.9815   0.0986
  -7.750  -0.2853   0.09911   0.09533  -0.0382   0.9697   0.1029
  -7.500  -0.2952   0.09672   0.09278  -0.0521   0.9491   0.1050
  -7.250  -0.2576   0.09028   0.08648  -0.0465   0.9486   0.1090
  -7.000  -0.2364   0.08654   0.08270  -0.0501   0.9393   0.1155
  -6.750  -0.2370   0.08270   0.07865  -0.0598   0.9222   0.1213
  -6.500  -0.2091   0.07822   0.07426  -0.0585   0.9175   0.1243
  -6.250  -0.1903   0.07512   0.07111  -0.0600   0.9081   0.1309
  -6.000  -0.1699   0.07090   0.06676  -0.0644   0.8998   0.1395
  -5.500  -0.1248   0.06443   0.06013  -0.0677   0.8832   0.1591
  -5.250  -0.1154   0.06176   0.05731  -0.0680   0.8705   0.1693
  -5.000  -0.0983   0.05952   0.05487  -0.0686   0.8603   0.1833
  -4.750  -0.0710   0.05670   0.05192  -0.0699   0.8538   0.1989
  -4.500  -0.0541   0.05386   0.04915  -0.0681   0.8452   0.2055
  -4.250  -0.0346   0.04211   0.03603  -0.0707   0.8381   0.1169
  -4.000  -0.0195   0.03894   0.03247  -0.0686   0.8290   0.1143
  -3.750   0.0078   0.03460   0.02740  -0.0679   0.8231   0.1104
  -3.500   0.0516   0.03171   0.02401  -0.0697   0.8200   0.1149
  -3.250   0.0678   0.03034   0.02223  -0.0670   0.8084   0.1180
  -3.000   0.1183   0.02767   0.01916  -0.0699   0.8052   0.1242
  -2.750   0.1420   0.02676   0.01813  -0.0684   0.7938   0.1332
  -2.500   0.1991   0.02470   0.01594  -0.0726   0.7897   0.1476
  -2.250   0.2271   0.02385   0.01509  -0.0718   0.7779   0.1615
  -2.000   0.2804   0.02257   0.01376  -0.0755   0.7708   0.1843
  -1.750   0.3166   0.02185   0.01307  -0.0761   0.7587   0.2055
  -1.500   0.3504   0.02115   0.01227  -0.0762   0.7442   0.2299
  -1.250   0.3886   0.02025   0.01137  -0.0773   0.7280   0.2629
  -1.000   0.4280   0.01908   0.01030  -0.0787   0.7082   0.3237
  -0.750   0.4758   0.01799   0.00931  -0.0820   0.6819   0.3836
  -0.500   0.7057   0.01668   0.00877  -0.1220   0.6140   1.0000
  -0.250   0.7248   0.01706   0.00882  -0.1201   0.5862   1.0000
   0.000   0.7457   0.01740   0.00883  -0.1186   0.5651   1.0000
   0.250   0.7637   0.01770   0.00893  -0.1166   0.5465   1.0000
   0.500   0.7832   0.01799   0.00898  -0.1150   0.5320   1.0000
   0.750   0.8030   0.01826   0.00906  -0.1134   0.5196   1.0000
   1.000   0.8226   0.01857   0.00922  -0.1119   0.5086   1.0000
   1.250   0.8447   0.01889   0.00934  -0.1109   0.5002   1.0000
   1.500   0.8659   0.01923   0.00956  -0.1097   0.4920   1.0000
   1.750   0.8896   0.01959   0.00975  -0.1091   0.4856   1.0000
   2.000   0.9106   0.01999   0.01008  -0.1079   0.4790   1.0000
   2.250   0.9355   0.02038   0.01031  -0.1076   0.4735   1.0000
   2.500   0.9569   0.02084   0.01071  -0.1066   0.4681   1.0000
   2.750   0.9783   0.02128   0.01110  -0.1055   0.4625   1.0000
   3.000   1.0045   0.02173   0.01141  -0.1055   0.4579   1.0000
   3.250   1.0263   0.02227   0.01193  -0.1046   0.4537   1.0000
   3.500   1.0459   0.02281   0.01251  -0.1033   0.4496   1.0000
   3.750   1.0685   0.02336   0.01302  -0.1027   0.4458   1.0000
   4.000   1.0949   0.02392   0.01351  -0.1027   0.4423   1.0000
   4.250   1.1167   0.02457   0.01416  -0.1020   0.4388   1.0000
   4.500   1.1321   0.02522   0.01491  -0.1000   0.4349   1.0000
   4.750   1.1516   0.02587   0.01562  -0.0988   0.4313   1.0000
   5.000   1.1743   0.02653   0.01628  -0.0982   0.4282   1.0000
   5.250   1.2035   0.02727   0.01691  -0.0989   0.4248   1.0000
   5.500   1.2116   0.02803   0.01787  -0.0956   0.4207   1.0000
   5.750   1.2263   0.02870   0.01863  -0.0936   0.4157   1.0000
   6.000   1.2502   0.02930   0.01920  -0.0933   0.4111   1.0000
   6.250   1.2707   0.03013   0.02004  -0.0924   0.4071   1.0000
   6.500   1.2773   0.03102   0.02113  -0.0890   0.4031   1.0000
   6.750   1.2922   0.03183   0.02205  -0.0872   0.3991   1.0000
   7.000   1.3157   0.03254   0.02275  -0.0869   0.3950   1.0000
   7.250   1.3372   0.03350   0.02373  -0.0863   0.3914   1.0000
   7.500   1.3353   0.03463   0.02512  -0.0817   0.3875   1.0000
   7.750   1.3439   0.03565   0.02630  -0.0789   0.3835   1.0000
   8.000   1.3668   0.03638   0.02704  -0.0785   0.3793   1.0000
   8.250   1.3920   0.03734   0.02800  -0.0787   0.3752   1.0000
   8.500   1.3768   0.03879   0.02975  -0.0721   0.3709   1.0000
   8.750   1.3929   0.03927   0.03027  -0.0704   0.3646   1.0000
   9.000   1.4143   0.03947   0.03044  -0.0696   0.3569   1.0000
   9.250   1.4169   0.03987   0.03094  -0.0657   0.3494   1.0000
   9.500   1.4440   0.03962   0.03059  -0.0657   0.3410   1.0000
   9.750   1.4341   0.04068   0.03185  -0.0600   0.3357   1.0000
  10.000   1.4867   0.03967   0.03060  -0.0640   0.3272   1.0000
  10.250   1.4587   0.04120   0.03245  -0.0556   0.3233   1.0000
  10.500   1.4553   0.04164   0.03297  -0.0509   0.3173   1.0000
  10.750   1.4841   0.04084   0.03205  -0.0509   0.3094   1.0000
  11.000   1.4595   0.04221   0.03365  -0.0436   0.3049   1.0000
  11.250   1.5031   0.04044   0.03166  -0.0455   0.2961   1.0000
  11.500   1.4748   0.04229   0.03381  -0.0383   0.2924   1.0000
  11.750   1.4582   0.04377   0.03549  -0.0334   0.2874   1.0000
  12.000   1.4922   0.04220   0.03374  -0.0337   0.2799   1.0000
  12.250   1.4618   0.04493   0.03679  -0.0280   0.2762   1.0000
  12.500   1.4480   0.04658   0.03860  -0.0243   0.2706   1.0000
  12.750   1.4639   0.04604   0.03801  -0.0231   0.2639   1.0000
  13.000   1.4331   0.04972   0.04198  -0.0193   0.2596   1.0000
  13.250   1.4306   0.05092   0.04326  -0.0174   0.2532   1.0000
  13.500   1.4201   0.05330   0.04577  -0.0156   0.2480   1.0000
  13.750   1.3843   0.05889   0.05161  -0.0138   0.2442   1.0000
  14.000   1.4008   0.05849   0.05118  -0.0132   0.2361   1.0000
  14.250   1.3483   0.06706   0.06005  -0.0128   0.2335   1.0000
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