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Glenn Martin 3 (glennmartin3-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: Glenn Martin 3 (glennmartin3-il)
Reynolds number: 1,000,000
Max Cl/Cd: 78.23 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-glennmartin3-il-1000000-n5.txt
Download as CSV file: xf-glennmartin3-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.9380   0.03800   0.03490  -0.1360   0.9735   0.0096
 -16.000  -0.9515   0.03504   0.03177  -0.1345   0.9717   0.0099
 -15.750  -0.9515   0.03311   0.02970  -0.1329   0.9706   0.0098
 -15.500  -0.9470   0.03144   0.02789  -0.1313   0.9697   0.0101
 -15.250  -0.9391   0.02994   0.02625  -0.1298   0.9691   0.0102
 -15.000  -0.9514   0.02892   0.02514  -0.1232   0.9645   0.0103
 -14.750  -0.9485   0.02777   0.02387  -0.1197   0.9625   0.0104
 -14.500  -0.9394   0.02674   0.02272  -0.1171   0.9612   0.0105
 -14.250  -0.9259   0.02588   0.02175  -0.1151   0.9602   0.0106
 -14.000  -0.9123   0.02492   0.02070  -0.1130   0.9594   0.0109
 -13.750  -0.9198   0.02425   0.01996  -0.1063   0.9545   0.0112
 -13.500  -0.9100   0.02354   0.01917  -0.1031   0.9519   0.0112
 -13.250  -0.8949   0.02282   0.01837  -0.1008   0.9504   0.0114
 -13.000  -0.8775   0.02211   0.01758  -0.0989   0.9493   0.0115
 -12.750  -0.8563   0.02156   0.01699  -0.0977   0.9486   0.0122
 -12.500  -0.8641   0.02110   0.01645  -0.0903   0.9416   0.0121
 -12.250  -0.8453   0.02050   0.01577  -0.0885   0.9398   0.0125
 -12.000  -0.8246   0.01986   0.01505  -0.0870   0.9385   0.0126
 -11.750  -0.8012   0.01933   0.01445  -0.0861   0.9375   0.0132
 -11.500  -0.7956   0.01886   0.01390  -0.0813   0.9322   0.0132
 -11.250  -0.7786   0.01837   0.01335  -0.0790   0.9289   0.0135
 -11.000  -0.7565   0.01784   0.01277  -0.0776   0.9270   0.0138
 -10.750  -0.7320   0.01740   0.01231  -0.0767   0.9257   0.0143
 -10.500  -0.7065   0.01703   0.01192  -0.0761   0.9247   0.0149
 -10.250  -0.6961   0.01682   0.01167  -0.0721   0.9186   0.0154
 -10.000  -0.6763   0.01643   0.01122  -0.0701   0.9154   0.0157
  -9.750  -0.6533   0.01603   0.01075  -0.0688   0.9133   0.0162
  -9.500  -0.6292   0.01552   0.01020  -0.0678   0.9118   0.0165
  -9.000  -0.5864   0.01495   0.00959  -0.0645   0.9039   0.0174
  -8.750  -0.5601   0.01471   0.00933  -0.0639   0.9007   0.0179
  -8.500  -0.5301   0.01427   0.00883  -0.0641   0.8979   0.0184
  -8.250  -0.4957   0.01389   0.00841  -0.0652   0.8958   0.0190
  -8.000  -0.4727   0.01351   0.00796  -0.0639   0.8895   0.0193
  -7.750  -0.4433   0.01326   0.00768  -0.0639   0.8861   0.0199
  -7.500  -0.4101   0.01281   0.00719  -0.0649   0.8825   0.0202
  -7.250  -0.3717   0.01259   0.00697  -0.0669   0.8788   0.0210
  -7.000  -0.3449   0.01234   0.00668  -0.0665   0.8724   0.0215
  -6.750  -0.3116   0.01208   0.00638  -0.0674   0.8677   0.0220
  -6.250  -0.2449   0.01148   0.00567  -0.0694   0.8560   0.0230
  -6.000  -0.2132   0.01130   0.00543  -0.0700   0.8494   0.0234
  -5.750  -0.1817   0.01100   0.00511  -0.0707   0.8428   0.0245
  -5.500  -0.1559   0.01080   0.00487  -0.0701   0.8355   0.0248
  -5.250  -0.1265   0.01062   0.00466  -0.0702   0.8300   0.0253
  -5.000  -0.1006   0.01049   0.00449  -0.0696   0.8230   0.0259
  -4.750  -0.0751   0.01038   0.00433  -0.0689   0.8132   0.0267
  -4.500  -0.0519   0.01024   0.00412  -0.0676   0.8023   0.0270
  -4.250  -0.0274   0.01012   0.00394  -0.0667   0.7925   0.0275
  -4.000  -0.0074   0.01004   0.00381  -0.0647   0.7805   0.0276
  -3.750   0.0134   0.00991   0.00361  -0.0630   0.7642   0.0285
  -3.500   0.0293   0.00987   0.00349  -0.0601   0.7408   0.0292
  -3.250   0.0341   0.01000   0.00342  -0.0548   0.6925   0.0294
  -3.000   0.0371   0.01022   0.00342  -0.0492   0.6418   0.0297
  -2.750   0.0520   0.01033   0.00339  -0.0462   0.6101   0.0301
  -2.500   0.0631   0.01056   0.00339  -0.0425   0.5578   0.0307
  -2.250   0.0774   0.01077   0.00340  -0.0395   0.5050   0.0316
  -2.000   0.0927   0.01101   0.00342  -0.0369   0.4548   0.0322
  -1.500   0.1375   0.01114   0.00336  -0.0345   0.4148   0.0337
  -1.250   0.1625   0.01112   0.00332  -0.0338   0.4040   0.0355
  -1.000   0.1858   0.01117   0.00331  -0.0328   0.3925   0.0357
  -0.750   0.2105   0.01117   0.00328  -0.0322   0.3832   0.0386
  -0.500   0.2345   0.01119   0.00328  -0.0313   0.3749   0.0407
  -0.250   0.2583   0.01121   0.00329  -0.0305   0.3614   0.0484
   0.000   0.2824   0.01123   0.00330  -0.0297   0.3517   0.0593
   0.250   0.3065   0.01124   0.00332  -0.0290   0.3424   0.0757
   0.500   0.3329   0.01117   0.00337  -0.0289   0.3281   0.1322
   0.750   0.3560   0.01124   0.00342  -0.0280   0.3177   0.1450
   1.000   0.3785   0.01133   0.00348  -0.0270   0.3041   0.1583
   1.250   0.4004   0.01146   0.00355  -0.0259   0.2897   0.1664
   1.500   0.4227   0.01157   0.00364  -0.0248   0.2738   0.1829
   1.750   0.4457   0.01167   0.00373  -0.0240   0.2631   0.1961
   2.000   0.4857   0.01121   0.00393  -0.0275   0.2487   0.4595
   2.500   0.6855   0.01223   0.00617  -0.0613   0.2187   0.9762
   2.750   0.7534   0.01278   0.00660  -0.0706   0.2086   0.9838
   3.000   0.7725   0.01298   0.00678  -0.0689   0.2058   0.9847
   3.250   0.8280   0.01307   0.00682  -0.0755   0.2008   0.9880
   3.500   0.8553   0.01321   0.00692  -0.0758   0.1976   0.9889
   3.750   0.8898   0.01339   0.00704  -0.0777   0.1934   0.9914
   4.250   0.9718   0.01348   0.00709  -0.0844   0.1877   0.9975
   4.500   1.0126   0.01344   0.00703  -0.0878   0.1852   0.9999
   4.750   1.0335   0.01360   0.00717  -0.0867   0.1834   1.0000
   5.000   1.0530   0.01379   0.00734  -0.0853   0.1808   1.0000
   5.250   1.0721   0.01399   0.00753  -0.0838   0.1783   1.0000
   5.500   1.0906   0.01422   0.00775  -0.0822   0.1754   1.0000
   5.750   1.1103   0.01439   0.00793  -0.0809   0.1742   1.0000
   6.000   1.1299   0.01458   0.00813  -0.0795   0.1736   1.0000
   6.250   1.1495   0.01477   0.00833  -0.0782   0.1719   1.0000
   6.500   1.1690   0.01498   0.00855  -0.0769   0.1712   1.0000
   6.750   1.1883   0.01520   0.00877  -0.0756   0.1691   1.0000
   7.000   1.2071   0.01543   0.00901  -0.0742   0.1680   1.0000
   7.250   1.2254   0.01569   0.00927  -0.0728   0.1663   1.0000
   7.500   1.2440   0.01595   0.00954  -0.0714   0.1651   1.0000
   7.750   1.2623   0.01622   0.00983  -0.0700   0.1636   1.0000
   8.000   1.2805   0.01651   0.01013  -0.0686   0.1622   1.0000
   8.250   1.2981   0.01682   0.01046  -0.0671   0.1606   1.0000
   8.500   1.3165   0.01709   0.01076  -0.0658   0.1600   1.0000
   8.750   1.3347   0.01737   0.01108  -0.0645   0.1594   1.0000
   9.000   1.3531   0.01765   0.01140  -0.0632   0.1590   1.0000
   9.250   1.3714   0.01794   0.01172  -0.0620   0.1579   1.0000
   9.500   1.3890   0.01826   0.01207  -0.0607   0.1566   1.0000
   9.750   1.4065   0.01859   0.01240  -0.0594   0.1530   1.0000
  10.000   1.4236   0.01895   0.01277  -0.0581   0.1511   1.0000
  10.250   1.4393   0.01940   0.01321  -0.0565   0.1479   1.0000
  10.500   1.4550   0.01982   0.01367  -0.0550   0.1464   1.0000
  10.750   1.4732   0.02013   0.01401  -0.0540   0.1441   1.0000
  11.000   1.4901   0.02051   0.01442  -0.0527   0.1409   1.0000
  11.250   1.5065   0.02092   0.01489  -0.0514   0.1411   1.0000
  11.500   1.5205   0.02146   0.01541  -0.0499   0.1359   1.0000
  11.750   1.5361   0.02193   0.01592  -0.0485   0.1347   1.0000
  12.000   1.5510   0.02245   0.01647  -0.0471   0.1330   1.0000
  12.250   1.5662   0.02294   0.01699  -0.0458   0.1286   1.0000
  12.500   1.5803   0.02351   0.01758  -0.0444   0.1257   1.0000
  12.750   1.5933   0.02416   0.01824  -0.0429   0.1222   1.0000
  13.000   1.6059   0.02483   0.01893  -0.0414   0.1169   1.0000
  13.250   1.6150   0.02573   0.01979  -0.0395   0.1081   1.0000
  13.500   1.6103   0.02754   0.02143  -0.0359   0.0860   1.0000
  13.750   1.6206   0.02841   0.02235  -0.0343   0.0833   1.0000
  14.000   1.6207   0.03000   0.02390  -0.0316   0.0726   1.0000
  14.250   1.5785   0.03473   0.02836  -0.0246   0.0329   1.0000
  14.500   1.5637   0.03772   0.03134  -0.0212   0.0197   1.0000
  14.750   1.5655   0.03949   0.03316  -0.0195   0.0177   1.0000
  15.000   1.5653   0.04150   0.03523  -0.0178   0.0158   1.0000
  15.250   1.5601   0.04405   0.03783  -0.0160   0.0130   1.0000
  15.500   1.5624   0.04599   0.03986  -0.0150   0.0127   1.0000
  15.750   1.5618   0.04828   0.04223  -0.0138   0.0120   1.0000
  16.000   1.5558   0.05124   0.04526  -0.0127   0.0109   1.0000
  16.250   1.5547   0.05374   0.04785  -0.0121   0.0108   1.0000
  16.500   1.5500   0.05679   0.05099  -0.0115   0.0103   0.9999
  16.750   1.5446   0.06002   0.05432  -0.0112   0.0101   0.9999
  17.000   1.5370   0.06367   0.05808  -0.0111   0.0098   0.9999
  17.250   1.5264   0.06782   0.06233  -0.0113   0.0092   0.9999
  17.500   1.5146   0.07225   0.06688  -0.0118   0.0091   0.9999
  17.750   1.4945   0.07804   0.07279  -0.0128   0.0083   0.9998
  18.000   1.4776   0.08361   0.07850  -0.0140   0.0084   0.9998
  18.250   1.4602   0.08934   0.08438  -0.0154   0.0087   0.9998
  18.500   1.4377   0.09584   0.09102  -0.0171   0.0088   0.9998
  18.750   1.4090   0.10341   0.09874  -0.0192   0.0085   0.9998
  19.000   1.3823   0.11077   0.10624  -0.0213   0.0085   0.9998
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