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Glenn Martin 2 (glennmartin2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: Glenn Martin 2 (glennmartin2-il)
Reynolds number: 1,000,000
Max Cl/Cd: 102.4 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-glennmartin2-il-1000000.txt
Download as CSV file: xf-glennmartin2-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.2490   0.15408   0.15241  -0.0416   0.9964   0.0116
 -14.750  -0.2356   0.15060   0.14893  -0.0446   0.9955   0.0121
 -13.000  -0.6447   0.02855   0.02578  -0.1230   0.9625   0.0123
 -12.750  -0.6248   0.02562   0.02262  -0.1245   0.9602   0.0126
 -12.500  -0.6000   0.02369   0.02050  -0.1258   0.9585   0.0130
 -12.250  -0.5833   0.02224   0.01888  -0.1248   0.9528   0.0132
 -12.000  -0.5586   0.02093   0.01739  -0.1252   0.9486   0.0135
 -11.750  -0.5290   0.01950   0.01577  -0.1266   0.9458   0.0139
 -11.500  -0.5056   0.01814   0.01426  -0.1267   0.9406   0.0145
 -11.250  -0.4806   0.01750   0.01355  -0.1263   0.9345   0.0149
 -11.000  -0.4476   0.01687   0.01284  -0.1276   0.9303   0.0154
 -10.750  -0.4240   0.01631   0.01218  -0.1269   0.9235   0.0159
 -10.500  -0.3958   0.01589   0.01167  -0.1270   0.9176   0.0164
 -10.250  -0.3674   0.01549   0.01113  -0.1271   0.9111   0.0169
 -10.000  -0.3498   0.01457   0.01008  -0.1253   0.9024   0.0176
  -9.750  -0.3253   0.01412   0.00955  -0.1246   0.8957   0.0182
  -9.500  -0.3025   0.01385   0.00923  -0.1234   0.8888   0.0188
  -9.250  -0.2755   0.01358   0.00889  -0.1231   0.8828   0.0196
  -9.000  -0.2543   0.01326   0.00850  -0.1216   0.8759   0.0202
  -8.750  -0.2292   0.01303   0.00815  -0.1208   0.8688   0.0207
  -8.500  -0.2104   0.01236   0.00739  -0.1189   0.8612   0.0218
  -8.250  -0.1868   0.01210   0.00708  -0.1179   0.8525   0.0225
  -8.000  -0.1633   0.01193   0.00688  -0.1168   0.8446   0.0234
  -7.750  -0.1392   0.01173   0.00659  -0.1158   0.8361   0.0244
  -7.500  -0.1157   0.01160   0.00639  -0.1146   0.8263   0.0251
  -7.250  -0.0952   0.01109   0.00577  -0.1130   0.8154   0.0262
  -7.000  -0.0738   0.01081   0.00542  -0.1114   0.8022   0.0272
  -6.750  -0.0520   0.01064   0.00519  -0.1099   0.7865   0.0282
  -6.500  -0.0310   0.01052   0.00497  -0.1082   0.7654   0.0293
  -6.250  -0.0123   0.01048   0.00477  -0.1060   0.7355   0.0302
  -6.000   0.0025   0.01054   0.00462  -0.1030   0.6935   0.0306
  -5.750   0.0180   0.01022   0.00413  -0.1003   0.6673   0.0322
  -5.500   0.0383   0.01011   0.00393  -0.0985   0.6516   0.0335
  -5.250   0.0605   0.01003   0.00378  -0.0971   0.6405   0.0349
  -5.000   0.0824   0.00995   0.00362  -0.0957   0.6298   0.0360
  -4.750   0.1056   0.00987   0.00347  -0.0945   0.6205   0.0369
  -4.500   0.1273   0.00965   0.00319  -0.0930   0.6123   0.0393
  -4.250   0.1504   0.00953   0.00305  -0.0919   0.6035   0.0413
  -4.000   0.1734   0.00946   0.00293  -0.0907   0.5953   0.0432
  -3.750   0.1963   0.00934   0.00277  -0.0894   0.5860   0.0466
  -3.500   0.2191   0.00926   0.00269  -0.0882   0.5761   0.0510
  -3.250   0.2409   0.00919   0.00261  -0.0868   0.5633   0.0576
  -3.000   0.2628   0.00922   0.00259  -0.0853   0.5445   0.0634
  -2.750   0.2780   0.00933   0.00254  -0.0826   0.4958   0.0703
  -2.500   0.2877   0.00977   0.00265  -0.0788   0.4262   0.0740
  -2.250   0.3063   0.00996   0.00270  -0.0768   0.4013   0.0766
  -2.000   0.3249   0.00998   0.00266  -0.0747   0.3860   0.0819
  -1.750   0.3441   0.01003   0.00265  -0.0728   0.3749   0.0854
  -1.500   0.3644   0.01007   0.00264  -0.0712   0.3663   0.0880
  -1.250   0.3844   0.01013   0.00264  -0.0694   0.3589   0.0896
  -1.000   0.4048   0.01009   0.00259  -0.0678   0.3539   0.0950
  -0.750   0.4249   0.01010   0.00258  -0.0661   0.3488   0.0998
  -0.500   0.4448   0.01015   0.00259  -0.0644   0.3435   0.1037
  -0.250   0.4659   0.01011   0.00258  -0.0629   0.3407   0.1137
   0.000   0.4843   0.01000   0.00261  -0.0610   0.3377   0.1608
   0.250   0.5038   0.01000   0.00272  -0.0592   0.3341   0.2139
   0.500   0.5245   0.01009   0.00282  -0.0578   0.3308   0.2306
   0.750   0.5447   0.01020   0.00293  -0.0562   0.3273   0.2430
   1.000   0.5674   0.01025   0.00299  -0.0551   0.3257   0.2513
   1.250   0.5897   0.01031   0.00307  -0.0540   0.3236   0.2591
   1.500   0.6114   0.01039   0.00314  -0.0528   0.3212   0.2649
   1.750   0.6326   0.01048   0.00323  -0.0514   0.3192   0.2713
   2.000   0.6535   0.01059   0.00333  -0.0501   0.3167   0.2767
   2.250   0.6735   0.01072   0.00344  -0.0486   0.3140   0.2829
   2.500   0.6932   0.01087   0.00359  -0.0471   0.3114   0.2907
   2.750   0.7152   0.01093   0.00368  -0.0460   0.3105   0.2982
   3.000   0.7369   0.01099   0.00378  -0.0448   0.3092   0.3067
   3.250   0.7582   0.01104   0.00388  -0.0437   0.3074   0.3212
   3.500   0.7776   0.01104   0.00402  -0.0421   0.3061   0.3697
   3.750   1.0072   0.01083   0.00516  -0.0879   0.2980   0.9954
   4.000   1.0550   0.01106   0.00536  -0.0928   0.2954   0.9982
   4.250   1.1012   0.01116   0.00546  -0.0971   0.2940   1.0000
   4.500   1.1170   0.01124   0.00555  -0.0948   0.2928   1.0000
   4.750   1.1337   0.01131   0.00562  -0.0928   0.2903   1.0000
   5.000   1.1499   0.01143   0.00575  -0.0906   0.2889   1.0000
   5.250   1.1663   0.01155   0.00585  -0.0885   0.2857   1.0000
   5.500   1.1814   0.01173   0.00601  -0.0862   0.2832   1.0000
   5.750   1.1955   0.01197   0.00624  -0.0838   0.2802   1.0000
   6.000   1.2155   0.01203   0.00633  -0.0825   0.2785   1.0000
   6.250   1.2352   0.01211   0.00643  -0.0811   0.2757   1.0000
   6.500   1.2533   0.01224   0.00658  -0.0795   0.2731   1.0000
   6.750   1.2699   0.01244   0.00674  -0.0777   0.2680   1.0000
   7.000   1.2867   0.01265   0.00695  -0.0759   0.2645   1.0000
   7.250   1.3066   0.01277   0.00710  -0.0747   0.2618   1.0000
   7.500   1.3250   0.01294   0.00728  -0.0733   0.2569   1.0000
   7.750   1.3413   0.01321   0.00750  -0.0715   0.2495   1.0000
   8.000   1.3590   0.01344   0.00771  -0.0701   0.2399   1.0000
   8.250   1.3724   0.01385   0.00803  -0.0679   0.2239   1.0000
   8.500   1.3692   0.01504   0.00889  -0.0631   0.1765   1.0000
   8.750   1.3635   0.01645   0.01003  -0.0582   0.1401   1.0000
   9.000   1.3615   0.01775   0.01113  -0.0540   0.1089   1.0000
   9.250   1.3325   0.02060   0.01358  -0.0463   0.0417   1.0000
   9.500   1.3297   0.02214   0.01507  -0.0425   0.0165   1.0000
   9.750   1.3397   0.02298   0.01595  -0.0406   0.0151   1.0000
  10.000   1.3492   0.02388   0.01691  -0.0387   0.0140   1.0000
  10.250   1.3594   0.02476   0.01784  -0.0370   0.0134   1.0000
  10.500   1.3686   0.02574   0.01888  -0.0353   0.0129   1.0000
  10.750   1.3763   0.02686   0.02005  -0.0336   0.0124   1.0000
  11.000   1.3826   0.02811   0.02137  -0.0318   0.0120   1.0000
  11.250   1.3849   0.02971   0.02304  -0.0298   0.0113   1.0000
  11.500   1.3854   0.03154   0.02497  -0.0278   0.0109   1.0000
  11.750   1.3937   0.03281   0.02629  -0.0267   0.0105   1.0000
  12.000   1.3973   0.03454   0.02809  -0.0253   0.0104   1.0000
  12.250   1.4012   0.03633   0.02995  -0.0242   0.0100   1.0000
  12.500   1.4033   0.03837   0.03206  -0.0231   0.0097   1.0000
  12.750   1.4029   0.04076   0.03453  -0.0221   0.0094   1.0000
  13.000   1.4021   0.04328   0.03714  -0.0213   0.0092   1.0000
  13.250   1.3987   0.04622   0.04016  -0.0207   0.0091   1.0000
  13.500   1.3934   0.04944   0.04348  -0.0202   0.0090   1.0000
  13.750   1.3830   0.05333   0.04749  -0.0198   0.0087   1.0000
  14.000   1.3745   0.05713   0.05139  -0.0196   0.0087   1.0000
  14.250   1.3521   0.06283   0.05725  -0.0197   0.0085   1.0000
  14.500   1.3393   0.06753   0.06206  -0.0201   0.0085   1.0000
  14.750   1.3205   0.07327   0.06794  -0.0209   0.0085   1.0000
  15.000   1.3138   0.07746   0.07222  -0.0216   0.0083   1.0000
  15.250   1.2865   0.08476   0.07967  -0.0229   0.0084   1.0000
  15.500   1.2875   0.08788   0.08286  -0.0235   0.0082   1.0000
  15.750   1.2703   0.09373   0.08881  -0.0247   0.0082   1.0000
  16.000   1.2622   0.09826   0.09343  -0.0257   0.0080   1.0000
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