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Marsden (marsden-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: Marsden (marsden-il)
Reynolds number: 1,000,000
Max Cl/Cd: 97.96 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-marsden-il-1000000-n5.txt
Download as CSV file: xf-marsden-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.1865   0.08708   0.08118  -0.1550   0.4301   0.0352
 -18.000  -0.2289   0.07774   0.07168  -0.1612   0.4301   0.0353
 -17.750  -0.2499   0.07163   0.06547  -0.1653   0.4300   0.0355
 -17.500  -0.2621   0.06681   0.06057  -0.1686   0.4299   0.0356
 -17.250  -0.2697   0.06263   0.05632  -0.1714   0.4297   0.0357
 -17.000  -0.2747   0.05885   0.05248  -0.1740   0.4295   0.0359
 -16.750  -0.2770   0.05542   0.04899  -0.1764   0.4293   0.0360
 -16.500  -0.2774   0.05229   0.04580  -0.1785   0.4291   0.0360
 -16.250  -0.2760   0.04944   0.04290  -0.1803   0.4288   0.0361
 -16.000  -0.2729   0.04683   0.04024  -0.1820   0.4285   0.0362
 -15.750  -0.2686   0.04444   0.03779  -0.1835   0.4281   0.0363
 -15.500  -0.2630   0.04225   0.03555  -0.1847   0.4277   0.0363
 -15.250  -0.2565   0.04023   0.03349  -0.1858   0.4274   0.0364
 -15.000  -0.2491   0.03839   0.03160  -0.1867   0.4270   0.0365
 -14.750  -0.2400   0.03678   0.02995  -0.1873   0.4267   0.0366
 -14.500  -0.2308   0.03525   0.02838  -0.1878   0.4264   0.0366
 -14.250  -0.2208   0.03385   0.02695  -0.1882   0.4260   0.0367
 -14.000  -0.2096   0.03262   0.02568  -0.1883   0.4257   0.0368
 -13.750  -0.1988   0.03143   0.02446  -0.1884   0.4254   0.0369
 -13.500  -0.1867   0.03039   0.02339  -0.1883   0.4250   0.0370
 -13.250  -0.1749   0.02938   0.02235  -0.1881   0.4247   0.0370
 -13.000  -0.1622   0.02850   0.02145  -0.1878   0.4243   0.0371
 -12.750  -0.1498   0.02766   0.02058  -0.1873   0.4240   0.0372
 -12.500  -0.1373   0.02688   0.01978  -0.1867   0.4236   0.0373
 -12.250  -0.1240   0.02620   0.01907  -0.1860   0.4233   0.0374
 -12.000  -0.1121   0.02547   0.01833  -0.1851   0.4232   0.0375
 -11.750  -0.0994   0.02484   0.01768  -0.1841   0.4231   0.0376
 -11.500  -0.0869   0.02424   0.01707  -0.1830   0.4230   0.0377
 -11.250  -0.0755   0.02363   0.01645  -0.1816   0.4230   0.0378
 -11.000  -0.0637   0.02310   0.01590  -0.1802   0.4229   0.0379
 -10.750  -0.0526   0.02259   0.01538  -0.1785   0.4228   0.0380
 -10.500  -0.0430   0.02209   0.01488  -0.1766   0.4227   0.0381
 -10.250  -0.0348   0.02163   0.01441  -0.1743   0.4226   0.0382
 -10.000  -0.0284   0.02120   0.01398  -0.1716   0.4225   0.0383
  -9.750  -0.0275   0.02079   0.01356  -0.1679   0.4224   0.0384
  -9.500  -0.0393   0.02040   0.01318  -0.1619   0.4223   0.0385
  -9.250  -0.0351   0.01995   0.01273  -0.1587   0.4222   0.0386
  -9.000  -0.0242   0.01951   0.01228  -0.1567   0.4221   0.0387
  -8.750  -0.0087   0.01910   0.01186  -0.1554   0.4220   0.0388
  -8.500   0.0100   0.01869   0.01145  -0.1547   0.4218   0.0389
  -8.250   0.0315   0.01831   0.01105  -0.1543   0.4217   0.0391
  -8.000   0.0554   0.01796   0.01069  -0.1544   0.4215   0.0392
  -7.750   0.0811   0.01762   0.01034  -0.1547   0.4213   0.0393
  -7.500   0.1085   0.01731   0.01002  -0.1553   0.4211   0.0395
  -7.250   0.1373   0.01703   0.00973  -0.1560   0.4209   0.0396
  -7.000   0.1673   0.01676   0.00945  -0.1570   0.4207   0.0397
  -6.750   0.1986   0.01646   0.00914  -0.1582   0.4205   0.0400
  -6.500   0.2313   0.01615   0.00883  -0.1597   0.4203   0.0403
  -6.250   0.2645   0.01591   0.00858  -0.1613   0.4201   0.0407
  -6.000   0.2976   0.01571   0.00839  -0.1626   0.4199   0.0411
  -5.750   0.3307   0.01556   0.00824  -0.1640   0.4196   0.0415
  -5.500   0.3637   0.01542   0.00811  -0.1652   0.4194   0.0419
  -5.250   0.3969   0.01531   0.00799  -0.1665   0.4192   0.0423
  -5.000   0.4302   0.01520   0.00788  -0.1678   0.4189   0.0426
  -4.750   0.4635   0.01509   0.00778  -0.1690   0.4186   0.0429
  -4.500   0.4969   0.01500   0.00769  -0.1703   0.4183   0.0433
  -4.250   0.5304   0.01493   0.00761  -0.1716   0.4179   0.0437
  -4.000   0.5642   0.01487   0.00756  -0.1730   0.4177   0.0441
  -3.750   0.5981   0.01483   0.00752  -0.1743   0.4174   0.0444
  -3.500   0.6322   0.01480   0.00749  -0.1757   0.4172   0.0448
  -3.250   0.6671   0.01475   0.00746  -0.1773   0.4169   0.0456
  -3.000   0.7016   0.01473   0.00745  -0.1788   0.4166   0.0465
  -2.750   0.7358   0.01473   0.00746  -0.1803   0.4164   0.0474
  -2.500   0.7697   0.01474   0.00748  -0.1816   0.4161   0.0484
  -2.250   0.8033   0.01475   0.00750  -0.1830   0.4158   0.0494
  -2.000   0.8372   0.01475   0.00751  -0.1844   0.4154   0.0507
  -1.750   0.8712   0.01475   0.00753  -0.1858   0.4151   0.0526
  -1.500   0.9044   0.01475   0.00755  -0.1871   0.4146   0.0548
  -1.250   0.9381   0.01476   0.00758  -0.1884   0.4142   0.0578
  -1.000   0.9714   0.01478   0.00762  -0.1897   0.4139   0.0617
  -0.750   1.0057   0.01481   0.00768  -0.1913   0.4136   0.0680
  -0.500   1.0414   0.01483   0.00775  -0.1932   0.4133   0.0798
  -0.250   1.0796   0.01482   0.00784  -0.1956   0.4130   0.1056
   0.000   1.1196   0.01481   0.00794  -0.1985   0.4128   0.1423
   0.250   1.1619   0.01478   0.00805  -0.2019   0.4125   0.1906
   0.500   1.2037   0.01477   0.00818  -0.2052   0.4122   0.2417
   0.750   1.2461   0.01477   0.00832  -0.2086   0.4120   0.2946
   1.000   1.3013   0.01467   0.00847  -0.2148   0.4116   0.3994
   1.250   1.3631   0.01459   0.00876  -0.2223   0.4113   0.5552
   1.500   1.3938   0.01474   0.00898  -0.2231   0.4109   0.5897
   1.750   1.4212   0.01491   0.00917  -0.2233   0.4105   0.6039
   2.000   1.4481   0.01509   0.00934  -0.2234   0.4101   0.6105
   2.250   1.4747   0.01529   0.00955  -0.2235   0.4098   0.6157
   2.500   1.5008   0.01551   0.00978  -0.2235   0.4094   0.6208
   2.750   1.5269   0.01575   0.01002  -0.2235   0.4090   0.6254
   3.000   1.5531   0.01603   0.01029  -0.2235   0.4085   0.6302
   3.250   1.5794   0.01634   0.01060  -0.2237   0.4079   0.6339
   3.500   1.6053   0.01662   0.01090  -0.2238   0.4076   0.6374
   3.750   1.6302   0.01680   0.01111  -0.2236   0.4074   0.6390
   4.000   1.6548   0.01700   0.01133  -0.2235   0.4073   0.6405
   4.250   1.6791   0.01720   0.01154  -0.2233   0.4071   0.6421
   4.500   1.7031   0.01741   0.01178  -0.2230   0.4070   0.6438
   4.750   1.7265   0.01763   0.01202  -0.2227   0.4068   0.6455
   5.000   1.7495   0.01786   0.01228  -0.2223   0.4065   0.6471
   5.250   1.7722   0.01810   0.01255  -0.2219   0.4063   0.6485
   5.500   1.7947   0.01835   0.01282  -0.2216   0.4061   0.6499
   5.750   1.8171   0.01861   0.01310  -0.2212   0.4058   0.6512
   6.000   1.8391   0.01888   0.01340  -0.2207   0.4055   0.6525
   6.250   1.8602   0.01917   0.01372  -0.2202   0.4051   0.6537
   6.500   1.8810   0.01947   0.01405  -0.2196   0.4048   0.6549
   6.750   1.9017   0.01979   0.01439  -0.2191   0.4044   0.6560
   7.000   1.9219   0.02012   0.01475  -0.2184   0.4040   0.6569
   7.250   1.9417   0.02046   0.01513  -0.2178   0.4036   0.6583
   7.500   1.9612   0.02082   0.01552  -0.2172   0.4032   0.6599
   7.750   1.9804   0.02119   0.01593  -0.2165   0.4027   0.6614
   8.000   1.9988   0.02158   0.01636  -0.2158   0.4022   0.6629
   8.250   2.0172   0.02197   0.01679  -0.2150   0.4017   0.6642
   8.500   2.0350   0.02239   0.01725  -0.2143   0.4012   0.6655
   8.750   2.0524   0.02281   0.01771  -0.2135   0.4006   0.6668
   9.000   2.0698   0.02327   0.01820  -0.2128   0.4001   0.6681
   9.250   2.0861   0.02378   0.01875  -0.2120   0.3996   0.6694
   9.500   2.1027   0.02430   0.01930  -0.2112   0.3991   0.6709
   9.750   2.1183   0.02487   0.01991  -0.2104   0.3986   0.6725
  10.000   2.1336   0.02547   0.02055  -0.2096   0.3981   0.6740
  10.250   2.1482   0.02611   0.02123  -0.2088   0.3976   0.6752
  10.500   2.1621   0.02682   0.02198  -0.2080   0.3971   0.6764
  10.750   2.1755   0.02760   0.02279  -0.2073   0.3965   0.6775
  11.000   2.1886   0.02842   0.02365  -0.2065   0.3960   0.6785
  11.250   2.2011   0.02932   0.02458  -0.2058   0.3953   0.6794
  11.500   2.2128   0.03029   0.02557  -0.2051   0.3944   0.6802
  11.750   2.2221   0.03147   0.02678  -0.2042   0.3934   0.6809
  12.000   2.2225   0.03335   0.02877  -0.2029   0.3927   0.6820
  12.250   2.2183   0.03574   0.03128  -0.2015   0.3915   0.6835
  12.500   2.2086   0.03877   0.03443  -0.2001   0.3897   0.6848
  12.750   2.1930   0.04252   0.03830  -0.1988   0.3876   0.6860
  13.000   2.1553   0.04864   0.04457  -0.1971   0.3845   0.6868
  13.250   2.0967   0.05705   0.05307  -0.1949   0.3798   0.6873
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