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KENNEDY AND MARSDEN AIRFOIL (kenmar-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: KENNEDY AND MARSDEN AIRFOIL (kenmar-il)
Reynolds number: 1,000,000
Max Cl/Cd: 97.86 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-kenmar-il-1000000-n5.txt
Download as CSV file: xf-kenmar-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: KENNEDY AND MARSDEN AIRFOIL                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.2074   0.08298   0.07701  -0.1572   0.4301   0.0353
 -16.250  -0.2390   0.07533   0.06923  -0.1620   0.4300   0.0354
 -16.000  -0.2551   0.06993   0.06374  -0.1655   0.4299   0.0356
 -15.750  -0.2644   0.06549   0.05923  -0.1684   0.4298   0.0357
 -15.500  -0.2705   0.06151   0.05519  -0.1710   0.4296   0.0358
 -15.250  -0.2743   0.05788   0.05150  -0.1734   0.4294   0.0359
 -15.000  -0.2762   0.05452   0.04808  -0.1757   0.4292   0.0360
 -14.750  -0.2762   0.05145   0.04496  -0.1777   0.4289   0.0361
 -14.500  -0.2746   0.04864   0.04209  -0.1795   0.4287   0.0362
 -14.250  -0.2717   0.04603   0.03942  -0.1812   0.4283   0.0362
 -14.000  -0.2667   0.04373   0.03707  -0.1826   0.4280   0.0363
 -13.750  -0.2605   0.04164   0.03493  -0.1837   0.4276   0.0364
 -13.500  -0.2536   0.03969   0.03293  -0.1848   0.4272   0.0364
 -13.250  -0.2458   0.03790   0.03110  -0.1856   0.4269   0.0365
 -13.000  -0.2371   0.03629   0.02945  -0.1863   0.4265   0.0366
 -12.750  -0.2271   0.03484   0.02796  -0.1868   0.4262   0.0366
 -12.500  -0.2172   0.03346   0.02655  -0.1872   0.4259   0.0367
 -12.250  -0.2060   0.03225   0.02531  -0.1873   0.4255   0.0368
 -12.000  -0.1950   0.03109   0.02412  -0.1874   0.4252   0.0369
 -11.750  -0.1826   0.03009   0.02308  -0.1873   0.4248   0.0370
 -11.500  -0.1710   0.02909   0.02205  -0.1872   0.4245   0.0371
 -11.250  -0.1580   0.02824   0.02118  -0.1869   0.4241   0.0371
 -11.000  -0.1460   0.02740   0.02031  -0.1864   0.4238   0.0372
 -10.750  -0.1330   0.02667   0.01956  -0.1859   0.4234   0.0373
 -10.500  -0.1200   0.02598   0.01885  -0.1852   0.4231   0.0374
 -10.250  -0.1081   0.02527   0.01812  -0.1843   0.4230   0.0375
 -10.000  -0.0954   0.02464   0.01748  -0.1833   0.4230   0.0376
  -9.750  -0.0830   0.02405   0.01688  -0.1822   0.4229   0.0377
  -9.500  -0.0718   0.02346   0.01627  -0.1809   0.4228   0.0378
  -9.250  -0.0601   0.02293   0.01573  -0.1794   0.4227   0.0379
  -9.000  -0.0492   0.02244   0.01523  -0.1777   0.4226   0.0380
  -8.750  -0.0403   0.02194   0.01472  -0.1757   0.4225   0.0381
  -8.500  -0.0324   0.02149   0.01427  -0.1733   0.4224   0.0382
  -8.250  -0.0272   0.02107   0.01384  -0.1704   0.4223   0.0383
  -8.000  -0.0311   0.02066   0.01344  -0.1659   0.4223   0.0384
  -7.750  -0.0391   0.02025   0.01303  -0.1605   0.4222   0.0385
  -7.500  -0.0327   0.01980   0.01258  -0.1578   0.4220   0.0386
  -7.250  -0.0197   0.01938   0.01215  -0.1561   0.4219   0.0387
  -7.000  -0.0035   0.01896   0.01173  -0.1550   0.4218   0.0388
  -6.750   0.0162   0.01857   0.01132  -0.1545   0.4216   0.0390
  -6.500   0.0384   0.01819   0.01093  -0.1543   0.4215   0.0391
  -6.250   0.0629   0.01784   0.01057  -0.1545   0.4213   0.0392
  -6.000   0.0892   0.01752   0.01023  -0.1550   0.4211   0.0394
  -5.750   0.1171   0.01722   0.00992  -0.1557   0.4209   0.0395
  -5.500   0.1463   0.01693   0.00963  -0.1566   0.4208   0.0396
  -5.250   0.1765   0.01668   0.00936  -0.1576   0.4205   0.0397
  -5.000   0.2082   0.01638   0.00905  -0.1590   0.4203   0.0400
  -4.750   0.2412   0.01607   0.00874  -0.1607   0.4201   0.0404
  -4.500   0.2744   0.01584   0.00851  -0.1622   0.4199   0.0408
  -4.250   0.3076   0.01565   0.00833  -0.1637   0.4197   0.0412
  -4.000   0.3406   0.01551   0.00820  -0.1650   0.4195   0.0416
  -3.750   0.3737   0.01538   0.00807  -0.1663   0.4192   0.0420
  -3.500   0.4070   0.01526   0.00795  -0.1676   0.4190   0.0423
  -3.250   0.4403   0.01516   0.00784  -0.1689   0.4187   0.0426
  -3.000   0.4736   0.01506   0.00775  -0.1702   0.4184   0.0431
  -2.750   0.5070   0.01497   0.00766  -0.1715   0.4180   0.0434
  -2.500   0.5406   0.01490   0.00759  -0.1728   0.4177   0.0438
  -2.250   0.5743   0.01486   0.00754  -0.1741   0.4175   0.0442
  -2.000   0.6080   0.01483   0.00752  -0.1754   0.4172   0.0446
  -1.750   0.6430   0.01477   0.00747  -0.1770   0.4170   0.0453
  -1.500   0.6774   0.01474   0.00745  -0.1785   0.4167   0.0460
  -1.250   0.7118   0.01473   0.00746  -0.1799   0.4164   0.0469
  -1.000   0.7458   0.01473   0.00747  -0.1813   0.4162   0.0478
  -0.750   0.7796   0.01474   0.00749  -0.1826   0.4159   0.0489
  -0.500   0.8130   0.01475   0.00750  -0.1839   0.4156   0.0497
  -0.250   0.8472   0.01474   0.00752  -0.1853   0.4152   0.0515
   0.000   0.8808   0.01474   0.00753  -0.1866   0.4148   0.0535
   0.500   0.9477   0.01476   0.00759  -0.1891   0.4140   0.0592
   0.750   0.9815   0.01479   0.00764  -0.1905   0.4137   0.0635
   1.000   1.0159   0.01482   0.00770  -0.1920   0.4134   0.0707
   1.250   1.0521   0.01484   0.00778  -0.1939   0.4131   0.0857
   1.500   1.0916   0.01482   0.00787  -0.1965   0.4129   0.1184
   1.750   1.1326   0.01479   0.00798  -0.1995   0.4126   0.1596
   2.000   1.1752   0.01476   0.00810  -0.2028   0.4123   0.2106
   2.250   1.2167   0.01477   0.00823  -0.2059   0.4121   0.2603
   2.500   1.2609   0.01475   0.00838  -0.2096   0.4118   0.3209
   2.750   1.3362   0.01454   0.00862  -0.2200   0.4115   0.5135
   3.000   1.3727   0.01464   0.00885  -0.2219   0.4111   0.5691
   3.250   1.4019   0.01481   0.00906  -0.2222   0.4108   0.5942
   3.500   1.4289   0.01498   0.00924  -0.2222   0.4104   0.6067
   3.750   1.4558   0.01515   0.00941  -0.2221   0.4100   0.6119
   4.000   1.4819   0.01535   0.00962  -0.2220   0.4096   0.6174
   4.250   1.5080   0.01558   0.00985  -0.2218   0.4092   0.6221
   4.500   1.5341   0.01582   0.01010  -0.2217   0.4088   0.6267
   4.750   1.5602   0.01610   0.01037  -0.2216   0.4083   0.6313
   5.000   1.5866   0.01642   0.01068  -0.2215   0.4078   0.6350
   5.250   1.6122   0.01668   0.01097  -0.2214   0.4074   0.6379
   5.500   1.6370   0.01687   0.01118  -0.2210   0.4073   0.6395
   5.750   1.6615   0.01706   0.01140  -0.2207   0.4071   0.6410
   6.000   1.6857   0.01727   0.01162  -0.2203   0.4070   0.6426
   6.250   1.7096   0.01748   0.01186  -0.2198   0.4068   0.6444
   6.500   1.7328   0.01771   0.01211  -0.2193   0.4066   0.6460
   6.750   1.7556   0.01794   0.01237  -0.2187   0.4064   0.6475
   7.000   1.7782   0.01818   0.01263  -0.2181   0.4061   0.6489
   7.250   1.8007   0.01844   0.01291  -0.2175   0.4059   0.6503
   7.500   1.8230   0.01870   0.01320  -0.2169   0.4056   0.6516
   7.750   1.8447   0.01897   0.01350  -0.2162   0.4053   0.6528
   8.000   1.8656   0.01927   0.01383  -0.2154   0.4049   0.6540
   8.250   1.8864   0.01957   0.01416  -0.2146   0.4046   0.6552
   8.500   1.9071   0.01989   0.01450  -0.2138   0.4042   0.6563
   8.750   1.9269   0.02024   0.01487  -0.2129   0.4038   0.6571
   9.000   1.9466   0.02058   0.01526  -0.2120   0.4034   0.6587
   9.250   1.9661   0.02094   0.01565  -0.2112   0.4030   0.6603
   9.500   1.9849   0.02131   0.01607  -0.2102   0.4025   0.6618
   9.750   2.0032   0.02170   0.01650  -0.2092   0.4020   0.6632
  10.000   2.0217   0.02209   0.01692  -0.2083   0.4014   0.6645
  10.250   2.0391   0.02251   0.01739  -0.2072   0.4009   0.6659
  10.500   2.0565   0.02296   0.01787  -0.2062   0.4004   0.6672
  10.750   2.0735   0.02344   0.01839  -0.2052   0.3999   0.6685
  11.000   2.0897   0.02396   0.01895  -0.2041   0.3994   0.6698
  11.250   2.1062   0.02449   0.01951  -0.2032   0.3989   0.6713
  11.500   2.1214   0.02508   0.02014  -0.2021   0.3984   0.6729
  11.750   2.1368   0.02568   0.02077  -0.2011   0.3979   0.6743
  12.000   2.1508   0.02636   0.02149  -0.2000   0.3974   0.6756
  12.250   2.1649   0.02708   0.02224  -0.1990   0.3968   0.6767
  12.500   2.1778   0.02789   0.02309  -0.1979   0.3963   0.6777
  12.750   2.1911   0.02871   0.02395  -0.1970   0.3957   0.6787
  13.000   2.2027   0.02967   0.02494  -0.1959   0.3949   0.6796
  13.250   2.2147   0.03064   0.02593  -0.1950   0.3941   0.6804
  13.500   2.2212   0.03202   0.02737  -0.1937   0.3931   0.6811
  13.750   2.2197   0.03409   0.02955  -0.1921   0.3923   0.6824
  14.000   2.2139   0.03667   0.03225  -0.1906   0.3909   0.6838
  14.250   2.2035   0.03982   0.03552  -0.1892   0.3891   0.6851
  14.500   2.1795   0.04442   0.04026  -0.1876   0.3866   0.6861
  14.750   2.1339   0.05146   0.04743  -0.1859   0.3830   0.6869
  15.250   1.6476   0.10756   0.10396  -0.1743   0.3396   0.6824
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