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Glenn Martin 3 (glennmartin3-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: Glenn Martin 3 (glennmartin3-il)
Reynolds number: 1,000,000
Max Cl/Cd: 78.74 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-glennmartin3-il-1000000.txt
Download as CSV file: xf-glennmartin3-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.7459   0.04494   0.04257  -0.1086   0.9785   0.0156
 -13.250  -0.8169   0.03695   0.03408  -0.1041   0.9709   0.0154
 -13.000  -0.8283   0.03387   0.03070  -0.1007   0.9683   0.0154
 -12.750  -0.8012   0.03374   0.03051  -0.1007   0.9676   0.0157
 -12.500  -0.8092   0.03227   0.02887  -0.0952   0.9618   0.0158
 -12.250  -0.8242   0.02938   0.02567  -0.0895   0.9581   0.0162
 -12.000  -0.8021   0.02897   0.02525  -0.0886   0.9571   0.0165
 -11.750  -0.8009   0.02787   0.02404  -0.0838   0.9517   0.0166
 -11.500  -0.7779   0.02774   0.02393  -0.0827   0.9493   0.0168
 -11.250  -0.7561   0.02713   0.02326  -0.0817   0.9478   0.0170
 -11.000  -0.7312   0.02668   0.02276  -0.0812   0.9467   0.0174
 -10.750  -0.7089   0.02582   0.02178  -0.0803   0.9458   0.0178
 -10.500  -0.7050   0.02499   0.02084  -0.0756   0.9398   0.0180
 -10.250  -0.6879   0.02400   0.01969  -0.0735   0.9371   0.0185
 -10.000  -0.6673   0.02300   0.01853  -0.0721   0.9356   0.0188
  -9.750  -0.6413   0.02255   0.01797  -0.0716   0.9346   0.0190
  -9.500  -0.6234   0.02075   0.01600  -0.0700   0.9337   0.0196
  -9.250  -0.6144   0.02070   0.01598  -0.0658   0.9269   0.0200
  -9.000  -0.5900   0.02037   0.01563  -0.0650   0.9248   0.0202
  -8.750  -0.5625   0.01994   0.01516  -0.0646   0.9234   0.0207
  -8.500  -0.5360   0.01918   0.01430  -0.0642   0.9223   0.0211
  -8.250  -0.5080   0.01861   0.01364  -0.0640   0.9214   0.0218
  -8.000  -0.4785   0.01788   0.01281  -0.0641   0.9205   0.0222
  -7.750  -0.4708   0.01774   0.01258  -0.0594   0.9128   0.0226
  -7.500  -0.4471   0.01653   0.01126  -0.0585   0.9110   0.0231
  -7.250  -0.4197   0.01595   0.01067  -0.0582   0.9097   0.0237
  -7.000  -0.3904   0.01560   0.01032  -0.0583   0.9084   0.0243
  -6.750  -0.3591   0.01502   0.00968  -0.0588   0.9072   0.0247
  -6.500  -0.3425   0.01475   0.00937  -0.0560   0.9007   0.0255
  -6.250  -0.3150   0.01425   0.00880  -0.0557   0.8975   0.0260
  -6.000  -0.2838   0.01407   0.00855  -0.0560   0.8950   0.0267
  -5.750  -0.2469   0.01292   0.00734  -0.0580   0.8936   0.0275
  -5.500  -0.2098   0.01243   0.00687  -0.0598   0.8924   0.0283
  -5.250  -0.1924   0.01229   0.00671  -0.0573   0.8849   0.0291
  -5.000  -0.1577   0.01190   0.00629  -0.0586   0.8815   0.0299
  -4.750  -0.1133   0.01142   0.00576  -0.0620   0.8777   0.0309
  -4.500  -0.0892   0.01123   0.00554  -0.0610   0.8702   0.0313
  -4.250  -0.0513   0.01059   0.00486  -0.0631   0.8644   0.0324
  -4.000  -0.0185   0.01024   0.00448  -0.0640   0.8554   0.0332
  -3.750   0.0179   0.00996   0.00417  -0.0658   0.8472   0.0342
  -3.500   0.0471   0.00978   0.00396  -0.0659   0.8390   0.0353
  -3.250   0.0842   0.00958   0.00370  -0.0678   0.8291   0.0364
  -3.000   0.1072   0.00945   0.00353  -0.0665   0.8200   0.0367
  -2.750   0.1398   0.00914   0.00317  -0.0675   0.8084   0.0389
  -2.500   0.1627   0.00905   0.00305  -0.0662   0.7984   0.0398
  -2.250   0.1855   0.00896   0.00293  -0.0649   0.7878   0.0412
  -2.000   0.2081   0.00891   0.00283  -0.0636   0.7762   0.0424
  -1.750   0.2250   0.00888   0.00273  -0.0610   0.7588   0.0444
  -1.500   0.2413   0.00885   0.00267  -0.0583   0.7366   0.0486
  -1.250   0.2516   0.00893   0.00262  -0.0542   0.7001   0.0524
  -1.000   0.2568   0.00914   0.00265  -0.0490   0.6534   0.0591
  -0.750   0.2672   0.00929   0.00268  -0.0451   0.6115   0.0811
  -0.500   0.2823   0.00933   0.00278  -0.0425   0.5722   0.1517
  -0.250   0.2927   0.00962   0.00289  -0.0388   0.5157   0.1686
   0.000   0.3049   0.00994   0.00301  -0.0355   0.4615   0.1827
   0.250   0.3235   0.01012   0.00310  -0.0336   0.4331   0.2029
   0.500   0.3475   0.01011   0.00317  -0.0330   0.4159   0.2543
   0.750   0.5685   0.01064   0.00558  -0.0776   0.3763   0.9764
   1.000   0.6283   0.01114   0.00595  -0.0849   0.3593   0.9841
   1.250   0.6961   0.01120   0.00586  -0.0940   0.3381   0.9894
   1.500   0.7296   0.01135   0.00591  -0.0955   0.3226   0.9923
   1.750   0.7723   0.01143   0.00584  -0.0991   0.3007   0.9959
   2.000   0.8165   0.01139   0.00564  -0.1031   0.2780   0.9993
   2.250   0.8407   0.01152   0.00566  -0.1026   0.2617   1.0000
   2.500   0.8582   0.01168   0.00576  -0.1006   0.2513   1.0000
   2.750   0.8761   0.01186   0.00587  -0.0988   0.2420   1.0000
   3.000   0.8942   0.01203   0.00599  -0.0969   0.2343   1.0000
   3.250   0.9128   0.01221   0.00612  -0.0952   0.2269   1.0000
   3.500   0.9321   0.01237   0.00625  -0.0936   0.2227   1.0000
   3.750   0.9507   0.01257   0.00640  -0.0919   0.2167   1.0000
   4.000   0.9699   0.01274   0.00656  -0.0903   0.2129   1.0000
   4.250   0.9897   0.01289   0.00670  -0.0889   0.2100   1.0000
   4.500   1.0085   0.01307   0.00686  -0.0872   0.2069   1.0000
   4.750   1.0270   0.01329   0.00705  -0.0856   0.2033   1.0000
   5.000   1.0442   0.01356   0.00729  -0.0837   0.1983   1.0000
   5.250   1.0642   0.01371   0.00745  -0.0823   0.1974   1.0000
   5.500   1.0843   0.01387   0.00763  -0.0810   0.1954   1.0000
   5.750   1.1039   0.01406   0.00781  -0.0796   0.1933   1.0000
   6.000   1.1231   0.01427   0.00802  -0.0782   0.1911   1.0000
   6.250   1.1417   0.01450   0.00825  -0.0767   0.1891   1.0000
   6.500   1.1591   0.01479   0.00852  -0.0750   0.1863   1.0000
   6.750   1.1753   0.01513   0.00887  -0.0731   0.1832   1.0000
   7.000   1.1948   0.01534   0.00909  -0.0718   0.1823   1.0000
   7.250   1.2143   0.01555   0.00933  -0.0705   0.1812   1.0000
   7.500   1.2341   0.01575   0.00957  -0.0693   0.1801   1.0000
   7.750   1.2524   0.01602   0.00986  -0.0679   0.1791   1.0000
   8.000   1.2708   0.01628   0.01013  -0.0665   0.1775   1.0000
   8.250   1.2889   0.01656   0.01044  -0.0650   0.1761   1.0000
   8.500   1.3067   0.01686   0.01075  -0.0636   0.1748   1.0000
   8.750   1.3239   0.01720   0.01108  -0.0621   0.1713   1.0000
   9.000   1.3393   0.01761   0.01150  -0.0603   0.1697   1.0000
   9.250   1.3562   0.01795   0.01187  -0.0588   0.1674   1.0000
   9.500   1.3756   0.01817   0.01214  -0.0578   0.1664   1.0000
   9.750   1.3938   0.01847   0.01247  -0.0565   0.1652   1.0000
  10.000   1.4131   0.01871   0.01273  -0.0555   0.1628   1.0000
  10.250   1.4286   0.01913   0.01320  -0.0539   0.1625   1.0000
  10.500   1.4460   0.01947   0.01355  -0.0526   0.1603   1.0000
  10.750   1.4621   0.01987   0.01398  -0.0512   0.1589   1.0000
  11.000   1.4754   0.02041   0.01452  -0.0493   0.1556   1.0000
  11.250   1.4895   0.02093   0.01507  -0.0476   0.1539   1.0000
  11.500   1.5073   0.02126   0.01546  -0.0465   0.1531   1.0000
  11.750   1.5246   0.02162   0.01587  -0.0454   0.1519   1.0000
  12.000   1.5425   0.02194   0.01625  -0.0445   0.1494   1.0000
  12.250   1.5582   0.02240   0.01674  -0.0432   0.1478   1.0000
  12.500   1.5735   0.02288   0.01724  -0.0419   0.1449   1.0000
  12.750   1.5855   0.02356   0.01792  -0.0402   0.1417   1.0000
  13.000   1.6010   0.02406   0.01847  -0.0390   0.1398   1.0000
  13.250   1.6180   0.02446   0.01893  -0.0381   0.1371   1.0000
  13.500   1.6324   0.02502   0.01950  -0.0369   0.1324   1.0000
  13.750   1.6438   0.02579   0.02026  -0.0353   0.1280   1.0000
  14.000   1.6582   0.02637   0.02091  -0.0342   0.1250   1.0000
  14.250   1.6690   0.02720   0.02172  -0.0326   0.1181   1.0000
  14.500   1.6737   0.02845   0.02290  -0.0304   0.1045   1.0000
  14.750   1.6607   0.03094   0.02520  -0.0264   0.0794   1.0000
  15.000   1.6390   0.03420   0.02831  -0.0219   0.0561   1.0000
  15.250   1.6241   0.03717   0.03122  -0.0184   0.0412   1.0000
  15.500   1.5986   0.04122   0.03522  -0.0147   0.0254   1.0000
  15.750   1.5894   0.04412   0.03817  -0.0127   0.0210   1.0000
  16.000   1.5832   0.04692   0.04104  -0.0112   0.0189   1.0000
  16.250   1.5767   0.04989   0.04410  -0.0101   0.0175   1.0000
  16.500   1.5615   0.05396   0.04826  -0.0090   0.0154   1.0000
  16.750   1.5570   0.05703   0.05142  -0.0086   0.0147   1.0000
  17.000   1.5499   0.06056   0.05506  -0.0084   0.0147   1.0000
  17.250   1.5420   0.06430   0.05892  -0.0085   0.0146   1.0000
  17.500   1.5287   0.06891   0.06366  -0.0089   0.0144   1.0000
  17.750   1.5111   0.07427   0.06916  -0.0098   0.0138   1.0000
  18.000   1.4945   0.07973   0.07476  -0.0110   0.0139   1.0000
  18.250   1.4694   0.08663   0.08180  -0.0127   0.0134   1.0000
  18.500   1.4460   0.09333   0.08864  -0.0145   0.0133   1.0000
  18.750   1.4137   0.10150   0.09698  -0.0168   0.0133   1.0000
  19.000   1.3907   0.10831   0.10394  -0.0189   0.0135   1.0000
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