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Marsden (marsden-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: Marsden (marsden-il)
Reynolds number: 500,000
Max Cl/Cd: 59.1 at α=2°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-marsden-il-500000-n5.txt
Download as CSV file: xf-marsden-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.0718   0.06572   0.05865  -0.1699   0.4385   0.0399
 -15.250  -0.0964   0.05925   0.05203  -0.1747   0.4385   0.0400
 -15.000  -0.1083   0.05466   0.04733  -0.1780   0.4384   0.0401
 -14.750  -0.1134   0.05113   0.04370  -0.1804   0.4382   0.0402
 -14.500  -0.1146   0.04818   0.04067  -0.1823   0.4380   0.0403
 -14.250  -0.1130   0.04567   0.03810  -0.1838   0.4379   0.0404
 -14.000  -0.1095   0.04348   0.03585  -0.1850   0.4377   0.0405
 -13.750  -0.1043   0.04156   0.03387  -0.1859   0.4374   0.0406
 -13.500  -0.0978   0.03986   0.03212  -0.1866   0.4372   0.0407
 -13.250  -0.0900   0.03834   0.03056  -0.1870   0.4370   0.0408
 -13.000  -0.0819   0.03693   0.02912  -0.1873   0.4368   0.0409
 -12.750  -0.0727   0.03569   0.02783  -0.1873   0.4365   0.0410
 -12.500  -0.0631   0.03454   0.02665  -0.1873   0.4363   0.0411
 -12.250  -0.0527   0.03351   0.02559  -0.1870   0.4360   0.0412
 -12.000  -0.0422   0.03254   0.02458  -0.1867   0.4357   0.0413
 -11.750  -0.0305   0.03167   0.02368  -0.1862   0.4355   0.0415
 -11.500  -0.0191   0.03084   0.02281  -0.1856   0.4352   0.0416
 -11.250  -0.0069   0.03007   0.02202  -0.1849   0.4349   0.0417
 -11.000   0.0056   0.02937   0.02129  -0.1841   0.4347   0.0419
 -10.750   0.0179   0.02869   0.02059  -0.1832   0.4344   0.0420
 -10.500   0.0307   0.02808   0.01995  -0.1822   0.4341   0.0422
 -10.250   0.0436   0.02750   0.01935  -0.1810   0.4338   0.0423
 -10.000   0.0561   0.02695   0.01878  -0.1798   0.4335   0.0425
  -9.750   0.0685   0.02643   0.01824  -0.1784   0.4333   0.0427
  -9.500   0.0807   0.02596   0.01775  -0.1769   0.4330   0.0429
  -9.250   0.0921   0.02551   0.01728  -0.1751   0.4327   0.0430
  -9.000   0.1021   0.02509   0.01685  -0.1731   0.4324   0.0432
  -8.750   0.1102   0.02473   0.01648  -0.1707   0.4322   0.0434
  -8.500   0.1163   0.02442   0.01617  -0.1679   0.4319   0.0435
  -8.250   0.1268   0.02408   0.01581  -0.1658   0.4317   0.0437
  -8.000   0.1403   0.02374   0.01546  -0.1642   0.4314   0.0439
  -7.750   0.1558   0.02341   0.01511  -0.1630   0.4311   0.0441
  -7.500   0.1726   0.02308   0.01477  -0.1619   0.4308   0.0443
  -7.250   0.1914   0.02278   0.01445  -0.1611   0.4305   0.0445
  -7.000   0.2117   0.02250   0.01415  -0.1606   0.4303   0.0447
  -6.750   0.2318   0.02210   0.01377  -0.1601   0.4300   0.0451
  -6.500   0.2543   0.02176   0.01344  -0.1600   0.4296   0.0455
  -6.250   0.2786   0.02148   0.01316  -0.1601   0.4293   0.0458
  -6.000   0.3043   0.02122   0.01290  -0.1605   0.4289   0.0462
  -5.750   0.3312   0.02098   0.01265  -0.1610   0.4285   0.0466
  -5.500   0.3594   0.02076   0.01243  -0.1617   0.4282   0.0470
  -5.250   0.3886   0.02058   0.01224  -0.1625   0.4279   0.0475
  -5.000   0.4185   0.02042   0.01207  -0.1635   0.4276   0.0479
  -4.750   0.4489   0.02028   0.01192  -0.1645   0.4273   0.0484
  -4.500   0.4798   0.02016   0.01180  -0.1656   0.4270   0.0489
  -4.250   0.5110   0.02008   0.01170  -0.1666   0.4267   0.0494
  -4.000   0.5425   0.02002   0.01164  -0.1678   0.4264   0.0499
  -3.750   0.5756   0.01992   0.01155  -0.1693   0.4261   0.0507
  -3.500   0.6084   0.01989   0.01153  -0.1707   0.4258   0.0514
  -3.250   0.6413   0.01991   0.01155  -0.1721   0.4255   0.0523
  -3.000   0.6743   0.01995   0.01160  -0.1734   0.4251   0.0534
  -2.750   0.7073   0.02005   0.01170  -0.1748   0.4246   0.0546
  -2.500   0.7407   0.02023   0.01188  -0.1763   0.4240   0.0559
  -2.250   0.7742   0.02052   0.01221  -0.1779   0.4232   0.0576
  -2.000   0.8055   0.02054   0.01225  -0.1790   0.4231   0.0599
  -1.750   0.8369   0.02056   0.01230  -0.1801   0.4228   0.0626
  -1.500   0.8685   0.02058   0.01236  -0.1812   0.4226   0.0665
  -1.250   0.9004   0.02062   0.01244  -0.1824   0.4223   0.0718
  -1.000   0.9325   0.02066   0.01255  -0.1837   0.4220   0.0802
  -0.750   0.9667   0.02072   0.01271  -0.1855   0.4217   0.0989
  -0.500   1.0039   0.02076   0.01290  -0.1880   0.4215   0.1349
  -0.250   1.0444   0.02079   0.01312  -0.1912   0.4211   0.1877
   0.000   1.0856   0.02085   0.01339  -0.1946   0.4208   0.2454
   0.250   1.1297   0.02094   0.01367  -0.1986   0.4204   0.3130
   0.500   1.2039   0.02089   0.01414  -0.2090   0.4200   0.4886
   0.750   1.2374   0.02116   0.01465  -0.2106   0.4196   0.5664
   1.000   1.2604   0.02149   0.01505  -0.2099   0.4192   0.5929
   1.250   1.2826   0.02183   0.01542  -0.2092   0.4187   0.6116
   1.500   1.3007   0.02217   0.01582  -0.2076   0.4183   0.6217
   1.750   1.3236   0.02248   0.01613  -0.2071   0.4177   0.6283
   2.000   1.3480   0.02281   0.01644  -0.2069   0.4172   0.6332
   2.250   1.3669   0.02315   0.01684  -0.2056   0.4167   0.6373
   2.500   1.3856   0.02353   0.01726  -0.2043   0.4162   0.6416
   2.750   1.4038   0.02394   0.01770  -0.2030   0.4158   0.6466
   3.000   1.4231   0.02436   0.01813  -0.2020   0.4153   0.6516
   3.250   1.4441   0.02477   0.01854  -0.2014   0.4149   0.6551
   3.500   1.4655   0.02517   0.01894  -0.2009   0.4144   0.6568
   3.750   1.4852   0.02556   0.01935  -0.2002   0.4140   0.6582
   4.000   1.5037   0.02596   0.01979  -0.1992   0.4136   0.6597
   4.250   1.5220   0.02637   0.02023  -0.1983   0.4131   0.6611
   4.500   1.5393   0.02682   0.02070  -0.1972   0.4127   0.6626
   4.750   1.5565   0.02727   0.02118  -0.1961   0.4123   0.6643
   5.000   1.5739   0.02773   0.02166  -0.1951   0.4119   0.6658
   5.250   1.5912   0.02821   0.02216  -0.1942   0.4115   0.6672
   5.500   1.6088   0.02870   0.02267  -0.1934   0.4111   0.6687
   5.750   1.6262   0.02921   0.02319  -0.1926   0.4107   0.6702
   6.000   1.6438   0.02972   0.02372  -0.1919   0.4103   0.6717
   6.250   1.6613   0.03027   0.02428  -0.1913   0.4099   0.6732
   6.500   1.6789   0.03084   0.02486  -0.1907   0.4095   0.6749
   6.750   1.6962   0.03144   0.02548  -0.1901   0.4090   0.6767
   7.000   1.7130   0.03212   0.02616  -0.1895   0.4086   0.6782
   7.250   1.7299   0.03285   0.02690  -0.1890   0.4080   0.6795
   7.500   1.7194   0.03486   0.02902  -0.1858   0.4071   0.6805
   8.000   1.0357   0.10945   0.10505  -0.1655   0.3510   0.6774
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