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DEFIANT CANARD BL20 AIRFOIL (defcnd1-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: DEFIANT CANARD BL20 AIRFOIL (defcnd1-il)
Reynolds number: 100,000
Max Cl/Cd: 32.28 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-defcnd1-il-100000-n5.txt
Download as CSV file: xf-defcnd1-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: DEFIANT CANARD BL20 AIRFOIL                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.5138   0.06500   0.05845  -0.0963   0.7783   0.0645
 -13.750  -0.5272   0.06010   0.05340  -0.0996   0.7683   0.0660
 -13.500  -0.5382   0.05580   0.04897  -0.1024   0.7593   0.0675
 -13.250  -0.5546   0.05110   0.04405  -0.1053   0.7514   0.0694
 -13.000  -0.5706   0.04672   0.03938  -0.1077   0.7447   0.0715
 -12.750  -0.5708   0.04451   0.03715  -0.1087   0.7368   0.0734
 -12.500  -0.5753   0.04206   0.03455  -0.1095   0.7299   0.0758
 -12.250  -0.5815   0.03960   0.03182  -0.1096   0.7241   0.0786
 -12.000  -0.5790   0.03831   0.03054  -0.1091   0.7176   0.0809
 -11.750  -0.5799   0.03686   0.02892  -0.1080   0.7116   0.0840
 -11.500  -0.5792   0.03565   0.02754  -0.1063   0.7063   0.0871
 -11.250  -0.5751   0.03486   0.02669  -0.1044   0.7006   0.0901
 -11.000  -0.5753   0.03381   0.02541  -0.1017   0.6949   0.0939
 -10.750  -0.5690   0.03340   0.02497  -0.0993   0.6897   0.0967
 -10.500  -0.5617   0.03289   0.02428  -0.0970   0.6855   0.1005
 -10.250  -0.5530   0.03224   0.02348  -0.0949   0.6806   0.1047
 -10.000  -0.5397   0.03188   0.02309  -0.0932   0.6754   0.1084
  -9.750  -0.5297   0.03123   0.02214  -0.0911   0.6707   0.1133
  -9.500  -0.5119   0.03087   0.02179  -0.0898   0.6665   0.1170
  -9.250  -0.4963   0.03041   0.02119  -0.0883   0.6622   0.1215
  -9.000  -0.4804   0.02984   0.02047  -0.0869   0.6574   0.1259
  -8.750  -0.4606   0.02943   0.02007  -0.0859   0.6530   0.1298
  -8.500  -0.4421   0.02894   0.01941  -0.0846   0.6489   0.1344
  -8.250  -0.4222   0.02840   0.01870  -0.0835   0.6454   0.1385
  -8.000  -0.4008   0.02798   0.01829  -0.0827   0.6413   0.1424
  -7.750  -0.3805   0.02754   0.01778  -0.0817   0.6365   0.1467
  -7.500  -0.3596   0.02708   0.01716  -0.0807   0.6323   0.1510
  -7.250  -0.3369   0.02663   0.01673  -0.0799   0.6286   0.1548
  -7.000  -0.3142   0.02623   0.01625  -0.0791   0.6254   0.1592
  -6.750  -0.2915   0.02587   0.01571  -0.0783   0.6221   0.1637
  -6.500  -0.2696   0.02547   0.01538  -0.0775   0.6175   0.1676
  -6.250  -0.2473   0.02514   0.01506  -0.0766   0.6132   0.1720
  -6.000  -0.2243   0.02482   0.01464  -0.0758   0.6095   0.1770
  -5.750  -0.2007   0.02447   0.01423  -0.0751   0.6064   0.1817
  -5.500  -0.1773   0.02413   0.01387  -0.0743   0.6036   0.1867
  -5.250  -0.1551   0.02392   0.01364  -0.0735   0.5998   0.1925
  -5.000  -0.1333   0.02369   0.01343  -0.0725   0.5954   0.1982
  -4.750  -0.1114   0.02342   0.01320  -0.0715   0.5915   0.2047
  -4.500  -0.0878   0.02319   0.01290  -0.0707   0.5882   0.2129
  -4.250  -0.0651   0.02290   0.01265  -0.0698   0.5854   0.2219
  -4.000  -0.0409   0.02265   0.01236  -0.0691   0.5830   0.2334
  -3.750  -0.0209   0.02256   0.01238  -0.0679   0.5786   0.2476
  -3.500  -0.0001   0.02243   0.01236  -0.0668   0.5744   0.2659
  -3.250   0.0217   0.02227   0.01230  -0.0658   0.5708   0.2892
  -3.000   0.0447   0.02214   0.01223  -0.0649   0.5678   0.3163
  -2.750   0.0693   0.02205   0.01213  -0.0642   0.5653   0.3442
  -2.500   0.0939   0.02202   0.01210  -0.0634   0.5628   0.3691
  -2.250   0.1132   0.02222   0.01241  -0.0621   0.5582   0.3902
  -2.000   0.1351   0.02234   0.01255  -0.0611   0.5541   0.4098
  -1.750   0.1589   0.02240   0.01257  -0.0603   0.5507   0.4281
  -1.500   0.1839   0.02241   0.01255  -0.0596   0.5479   0.4455
  -1.250   0.2101   0.02238   0.01247  -0.0591   0.5455   0.4615
  -1.000   0.2342   0.02247   0.01255  -0.0584   0.5426   0.4764
  -0.500   0.2746   0.02289   0.01308  -0.0560   0.5339   0.5048
  -0.250   0.2989   0.02292   0.01312  -0.0553   0.5308   0.5200
   0.000   0.3243   0.02289   0.01310  -0.0547   0.5283   0.5402
   0.250   0.3513   0.02277   0.01301  -0.0542   0.5261   0.5640
   0.500   0.3699   0.02302   0.01339  -0.0528   0.5221   0.5852
   0.750   0.3873   0.02332   0.01384  -0.0513   0.5175   0.6051
   1.000   0.4101   0.02344   0.01403  -0.0504   0.5140   0.6265
   1.250   0.4365   0.02343   0.01408  -0.0501   0.5112   0.6500
   1.500   0.4659   0.02331   0.01401  -0.0501   0.5088   0.6784
   1.750   0.4973   0.02314   0.01390  -0.0503   0.5067   0.7154
   2.000   0.5085   0.02384   0.01490  -0.0480   0.5011   0.7592
   2.250   0.5410   0.02416   0.01542  -0.0490   0.4969   0.8187
   2.500   0.5948   0.02432   0.01562  -0.0537   0.4936   0.8767
   2.750   0.6510   0.02434   0.01556  -0.0588   0.4909   0.9192
   3.000   0.7040   0.02431   0.01538  -0.0633   0.4887   0.9486
   3.250   0.7331   0.02535   0.01654  -0.0651   0.4830   0.9777
   3.500   0.7754   0.02585   0.01702  -0.0687   0.4786   0.9987
   3.750   0.7935   0.02605   0.01715  -0.0674   0.4755   1.0000
   4.000   0.8145   0.02608   0.01706  -0.0662   0.4730   1.0000
   4.250   0.8399   0.02602   0.01687  -0.0656   0.4710   1.0000
   4.500   0.8244   0.02737   0.01834  -0.0597   0.4655   1.0000
   4.750   0.8223   0.02822   0.01921  -0.0556   0.4609   1.0000
   5.000   0.8369   0.02850   0.01944  -0.0536   0.4577   1.0000
   5.250   0.8618   0.02847   0.01931  -0.0529   0.4554   1.0000
   5.500   0.8927   0.02831   0.01905  -0.0531   0.4535   1.0000
   5.750   0.8049   0.03205   0.02301  -0.0388   0.4442   1.0000
   6.000   0.8127   0.03277   0.02370  -0.0366   0.4405   1.0000
   6.250   0.8412   0.03258   0.02343  -0.0363   0.4384   1.0000
   6.500   0.8784   0.03205   0.02281  -0.0369   0.4368   1.0000
   7.000   0.7656   0.04263   0.03360  -0.0266   0.4155   1.0000
   7.250   0.8173   0.04035   0.03122  -0.0269   0.4170   1.0000
   7.500   0.8737   0.03796   0.02873  -0.0276   0.4183   1.0000
   8.000   0.8224   0.04604   0.03691  -0.0233   0.4012   1.0000
  10.000   0.8056   0.06742   0.05843  -0.0177   0.3524   1.0000
  10.500   0.7883   0.07509   0.06617  -0.0174   0.3372   1.0000
  10.750   0.8127   0.07490   0.06597  -0.0169   0.3363   1.0000
  12.250   0.7716   0.09886   0.09018  -0.0185   0.2954   1.0000
  12.750   0.8039   0.10078   0.09214  -0.0181   0.2910   1.0000
  13.750   0.8280   0.11051   0.10200  -0.0192   0.2750   1.0000
  14.000   0.8008   0.11805   0.10962  -0.0210   0.2651   1.0000
  14.250   0.8147   0.11933   0.11093  -0.0211   0.2624   1.0000
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