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Marsden (marsden-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: Marsden (marsden-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.22 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-marsden-il-1000000.txt
Download as CSV file: xf-marsden-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Marsden                                         
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.1003   0.05490   0.04911  -0.1826   0.4405   0.0414
 -15.000  -0.1205   0.04952   0.04360  -0.1866   0.4404   0.0414
 -14.750  -0.1281   0.04593   0.03991  -0.1891   0.4403   0.0415
 -14.500  -0.1305   0.04309   0.03699  -0.1909   0.4402   0.0416
 -14.250  -0.1295   0.04076   0.03458  -0.1922   0.4401   0.0417
 -14.000  -0.1267   0.03873   0.03249  -0.1931   0.4400   0.0418
 -13.750  -0.1222   0.03696   0.03066  -0.1938   0.4399   0.0419
 -13.500  -0.1154   0.03546   0.02911  -0.1941   0.4397   0.0420
 -13.250  -0.1076   0.03414   0.02775  -0.1942   0.4396   0.0422
 -13.000  -0.0993   0.03291   0.02647  -0.1942   0.4394   0.0423
 -12.750  -0.0894   0.03183   0.02535  -0.1940   0.4393   0.0425
 -12.500  -0.0789   0.03086   0.02434  -0.1937   0.4391   0.0426
 -12.250  -0.0675   0.02998   0.02343  -0.1933   0.4389   0.0428
 -12.000  -0.0557   0.02915   0.02256  -0.1928   0.4388   0.0430
 -11.750  -0.0438   0.02837   0.02174  -0.1922   0.4386   0.0432
 -11.500  -0.0310   0.02762   0.02096  -0.1914   0.4384   0.0434
 -11.250  -0.0180   0.02691   0.02021  -0.1906   0.4382   0.0435
 -11.000  -0.0045   0.02628   0.01955  -0.1897   0.4380   0.0436
 -10.750   0.0096   0.02568   0.01893  -0.1887   0.4378   0.0438
 -10.500   0.0236   0.02513   0.01835  -0.1876   0.4376   0.0439
 -10.250   0.0374   0.02462   0.01781  -0.1864   0.4374   0.0440
 -10.000   0.0516   0.02415   0.01732  -0.1851   0.4372   0.0441
  -9.750   0.0648   0.02373   0.01689  -0.1835   0.4370   0.0442
  -9.500   0.0761   0.02337   0.01651  -0.1816   0.4368   0.0443
  -9.250   0.0855   0.02310   0.01622  -0.1793   0.4366   0.0444
  -9.000   0.0971   0.02281   0.01592  -0.1773   0.4363   0.0445
  -8.750   0.1128   0.02249   0.01559  -0.1760   0.4361   0.0445
  -8.500   0.1300   0.02218   0.01526  -0.1749   0.4358   0.0446
  -8.250   0.1466   0.02171   0.01478  -0.1736   0.4354   0.0448
  -8.000   0.1629   0.02122   0.01429  -0.1721   0.4351   0.0450
  -7.750   0.1807   0.02082   0.01389  -0.1710   0.4348   0.0453
  -7.500   0.2004   0.02046   0.01354  -0.1703   0.4346   0.0455
  -7.250   0.2222   0.02016   0.01324  -0.1700   0.4343   0.0458
  -7.000   0.2457   0.01988   0.01298  -0.1699   0.4340   0.0461
  -6.750   0.2708   0.01964   0.01274  -0.1701   0.4338   0.0464
  -6.500   0.2972   0.01941   0.01251  -0.1704   0.4335   0.0467
  -6.250   0.3247   0.01920   0.01231  -0.1710   0.4332   0.0470
  -6.000   0.3533   0.01901   0.01212  -0.1717   0.4329   0.0473
  -5.750   0.3828   0.01883   0.01194  -0.1726   0.4326   0.0477
  -5.500   0.4131   0.01868   0.01179  -0.1735   0.4323   0.0482
  -5.250   0.4441   0.01854   0.01164  -0.1746   0.4320   0.0486
  -5.000   0.4752   0.01844   0.01154  -0.1756   0.4316   0.0491
  -4.750   0.5063   0.01836   0.01146  -0.1766   0.4313   0.0495
  -4.500   0.5373   0.01829   0.01138  -0.1775   0.4309   0.0498
  -4.250   0.5719   0.01799   0.01107  -0.1794   0.4305   0.0506
  -4.000   0.6058   0.01781   0.01090  -0.1810   0.4300   0.0514
  -3.750   0.6391   0.01772   0.01080  -0.1824   0.4296   0.0521
  -3.500   0.6724   0.01766   0.01075  -0.1837   0.4292   0.0528
  -3.250   0.7059   0.01761   0.01070  -0.1851   0.4288   0.0536
  -3.000   0.7395   0.01761   0.01069  -0.1865   0.4284   0.0545
  -2.750   0.7728   0.01765   0.01073  -0.1878   0.4281   0.0553
  -2.500   0.8093   0.01762   0.01071  -0.1899   0.4278   0.0570
  -2.250   0.8441   0.01767   0.01076  -0.1915   0.4274   0.0588
  -2.000   0.8780   0.01776   0.01086  -0.1930   0.4271   0.0609
  -1.750   0.9139   0.01783   0.01096  -0.1949   0.4267   0.0644
  -1.500   0.9494   0.01796   0.01111  -0.1968   0.4263   0.0699
  -1.250   0.9868   0.01811   0.01133  -0.1991   0.4259   0.0826
  -1.000   1.0344   0.01823   0.01168  -0.2038   0.4253   0.1439
  -0.750   1.0743   0.01981   0.01362  -0.2079   0.4232   0.2216
  -0.500   1.1245   0.01965   0.01370  -0.2130   0.4231   0.3032
  -0.250   1.1870   0.01942   0.01380  -0.2208   0.4229   0.4289
   0.000   1.2410   0.01940   0.01406  -0.2265   0.4228   0.5465
   0.250   1.2722   0.01956   0.01429  -0.2274   0.4226   0.5744
   0.500   1.3008   0.01975   0.01449  -0.2278   0.4225   0.5900
   0.750   1.3282   0.01994   0.01471  -0.2279   0.4223   0.6027
   1.000   1.3554   0.02015   0.01492  -0.2280   0.4221   0.6120
   1.250   1.3798   0.02039   0.01521  -0.2275   0.4218   0.6223
   1.500   1.4039   0.02067   0.01549  -0.2270   0.4216   0.6319
   1.750   1.4281   0.02089   0.01575  -0.2265   0.4213   0.6383
   2.000   1.4509   0.02114   0.01603  -0.2258   0.4210   0.6425
   2.250   1.4743   0.02138   0.01629  -0.2253   0.4207   0.6455
   2.500   1.4975   0.02164   0.01656  -0.2247   0.4204   0.6489
   2.750   1.5205   0.02190   0.01684  -0.2242   0.4200   0.6523
   3.000   1.5426   0.02219   0.01714  -0.2235   0.4197   0.6556
   3.250   1.5650   0.02244   0.01741  -0.2229   0.4193   0.6592
   3.500   1.5841   0.02266   0.01766  -0.2217   0.4189   0.6625
   3.750   1.6032   0.02291   0.01795  -0.2205   0.4184   0.6646
   4.000   1.6239   0.02318   0.01824  -0.2196   0.4180   0.6663
   4.250   1.6452   0.02345   0.01853  -0.2190   0.4175   0.6678
   4.500   1.6664   0.02373   0.01883  -0.2183   0.4171   0.6693
   4.750   1.6867   0.02403   0.01915  -0.2175   0.4166   0.6709
   5.000   1.7060   0.02433   0.01947  -0.2166   0.4162   0.6724
   5.250   1.7249   0.02464   0.01980  -0.2156   0.4157   0.6741
   5.500   1.7435   0.02496   0.02015  -0.2146   0.4152   0.6758
   5.750   1.7622   0.02528   0.02048  -0.2137   0.4148   0.6773
   6.000   1.7805   0.02558   0.02079  -0.2127   0.4143   0.6785
   6.250   1.7990   0.02586   0.02109  -0.2118   0.4139   0.6795
   6.500   1.8182   0.02611   0.02135  -0.2110   0.4134   0.6804
   6.750   1.8371   0.02640   0.02165  -0.2102   0.4130   0.6811
   7.000   1.8589   0.02665   0.02191  -0.2100   0.4126   0.6833
   7.250   1.8790   0.02694   0.02222  -0.2095   0.4122   0.6850
   7.500   1.8978   0.02727   0.02257  -0.2088   0.4118   0.6866
   7.750   1.9169   0.02758   0.02290  -0.2082   0.4114   0.6882
   8.000   1.9363   0.02792   0.02325  -0.2076   0.4110   0.6896
   8.250   1.9555   0.02829   0.02364  -0.2071   0.4106   0.6910
   8.500   1.9750   0.02869   0.02406  -0.2067   0.4101   0.6923
   8.750   1.9940   0.02916   0.02454  -0.2062   0.4096   0.6936
   9.000   2.0064   0.03011   0.02552  -0.2050   0.4087   0.6949
   9.250   1.4029   0.08464   0.08119  -0.1750   0.3795   0.6918
   9.500   1.4321   0.08423   0.08077  -0.1754   0.3798   0.6931
   9.750   1.4611   0.08383   0.08036  -0.1759   0.3799   0.6944
  10.000   1.4902   0.08342   0.07995  -0.1764   0.3801   0.6957
  10.250   1.6668   0.06691   0.06330  -0.1801   0.3922   0.6985
  10.500   1.7001   0.06608   0.06245  -0.1807   0.3924   0.6998
  10.750   1.7342   0.06516   0.06151  -0.1813   0.3925   0.7010
  11.000   1.7701   0.06406   0.06039  -0.1819   0.3927   0.7023
  11.250   1.8063   0.06291   0.05921  -0.1826   0.3929   0.7034
  11.500   1.8446   0.06155   0.05783  -0.1833   0.3931   0.7043
  11.750   1.8863   0.06002   0.05628  -0.1843   0.3933   0.7065
  12.000   1.9302   0.05821   0.05444  -0.1853   0.3935   0.7085
  12.250   1.4168   0.11809   0.11482  -0.1753   0.3446   0.7029
  12.500   1.4398   0.11823   0.11495  -0.1757   0.3444   0.7038
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