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DEFIANT CANARD BL20 AIRFOIL (defcnd1-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: DEFIANT CANARD BL20 AIRFOIL (defcnd1-il)
Reynolds number: 1,000,000
Max Cl/Cd: 116.6 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-defcnd1-il-1000000-n5.txt
Download as CSV file: xf-defcnd1-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.6991   0.08681   0.08216  -0.0914   0.6765   0.0149
 -18.250  -0.7350   0.07836   0.07357  -0.0960   0.6750   0.0147
 -18.000  -0.7668   0.07077   0.06583  -0.1002   0.6712   0.0148
 -17.750  -0.7889   0.06474   0.05967  -0.1035   0.6675   0.0151
 -17.500  -0.8121   0.05885   0.05364  -0.1066   0.6641   0.0151
 -17.250  -0.8311   0.05377   0.04846  -0.1091   0.6609   0.0151
 -17.000  -0.8470   0.04931   0.04389  -0.1111   0.6568   0.0151
 -16.750  -0.8598   0.04532   0.03980  -0.1128   0.6527   0.0152
 -16.500  -0.8686   0.04188   0.03625  -0.1141   0.6482   0.0153
 -16.000  -0.8841   0.03539   0.02958  -0.1162   0.6410   0.0157
 -15.750  -0.8887   0.03255   0.02665  -0.1169   0.6373   0.0159
 -15.500  -0.8908   0.03009   0.02411  -0.1173   0.6334   0.0162
 -15.250  -0.8909   0.02803   0.02197  -0.1173   0.6288   0.0163
 -15.000  -0.8903   0.02624   0.02010  -0.1167   0.6247   0.0166
 -14.750  -0.8880   0.02475   0.01854  -0.1158   0.6209   0.0169
 -14.500  -0.8846   0.02347   0.01721  -0.1145   0.6172   0.0172
 -14.250  -0.8796   0.02242   0.01609  -0.1130   0.6134   0.0175
 -14.000  -0.8737   0.02152   0.01512  -0.1111   0.6096   0.0178
 -13.750  -0.8667   0.02074   0.01428  -0.1091   0.6057   0.0181
 -13.500  -0.8604   0.01999   0.01348  -0.1068   0.6020   0.0186
 -13.250  -0.8521   0.01933   0.01278  -0.1045   0.5990   0.0190
 -13.000  -0.8432   0.01873   0.01215  -0.1020   0.5953   0.0196
 -12.750  -0.8328   0.01822   0.01159  -0.0996   0.5915   0.0202
 -12.500  -0.8215   0.01776   0.01108  -0.0971   0.5878   0.0209
 -12.250  -0.8106   0.01731   0.01059  -0.0945   0.5843   0.0215
 -12.000  -0.7997   0.01691   0.01015  -0.0918   0.5815   0.0224
 -11.750  -0.7872   0.01656   0.00979  -0.0892   0.5789   0.0235
 -11.500  -0.7711   0.01618   0.00938  -0.0873   0.5756   0.0248
 -11.250  -0.7539   0.01579   0.00897  -0.0856   0.5719   0.0266
 -11.000  -0.7353   0.01545   0.00859  -0.0841   0.5683   0.0282
 -10.750  -0.7163   0.01511   0.00822  -0.0826   0.5645   0.0302
 -10.500  -0.6964   0.01475   0.00786  -0.0813   0.5619   0.0326
 -10.250  -0.6757   0.01441   0.00751  -0.0800   0.5594   0.0357
 -10.000  -0.6544   0.01409   0.00718  -0.0789   0.5564   0.0389
  -9.750  -0.6329   0.01376   0.00685  -0.0777   0.5531   0.0424
  -9.500  -0.6109   0.01346   0.00655  -0.0767   0.5495   0.0461
  -9.250  -0.5888   0.01316   0.00624  -0.0756   0.5458   0.0510
  -9.000  -0.5659   0.01288   0.00596  -0.0747   0.5430   0.0555
  -8.750  -0.5422   0.01261   0.00570  -0.0739   0.5408   0.0603
  -8.500  -0.5182   0.01236   0.00546  -0.0731   0.5380   0.0653
  -8.250  -0.4939   0.01213   0.00524  -0.0724   0.5350   0.0710
  -8.000  -0.4693   0.01192   0.00504  -0.0717   0.5315   0.0764
  -7.750  -0.4442   0.01174   0.00486  -0.0711   0.5280   0.0814
  -7.500  -0.4184   0.01161   0.00471  -0.0706   0.5248   0.0858
  -7.250  -0.3923   0.01144   0.00456  -0.0701   0.5227   0.0897
  -7.000  -0.3657   0.01132   0.00443  -0.0697   0.5202   0.0934
  -6.750  -0.3392   0.01119   0.00429  -0.0693   0.5172   0.0961
  -6.500  -0.3128   0.01107   0.00416  -0.0689   0.5139   0.0996
  -6.250  -0.2859   0.01099   0.00405  -0.0686   0.5105   0.1030
  -6.000  -0.2596   0.01088   0.00393  -0.0681   0.5072   0.1068
  -5.750  -0.2326   0.01077   0.00383  -0.0678   0.5051   0.1098
  -5.500  -0.2052   0.01068   0.00372  -0.0676   0.5028   0.1119
  -5.250  -0.1777   0.01060   0.00362  -0.0673   0.5000   0.1135
  -5.000  -0.1509   0.01049   0.00350  -0.0670   0.4967   0.1161
  -4.750  -0.1240   0.01040   0.00340  -0.0667   0.4935   0.1184
  -4.500  -0.0970   0.01033   0.00330  -0.0663   0.4904   0.1207
  -4.250  -0.0697   0.01027   0.00322  -0.0661   0.4878   0.1228
  -4.000  -0.0418   0.01020   0.00314  -0.0659   0.4857   0.1245
  -3.750  -0.0145   0.01011   0.00305  -0.0657   0.4829   0.1277
  -3.500   0.0127   0.01002   0.00297  -0.0654   0.4799   0.1306
  -3.250   0.0401   0.00996   0.00289  -0.0651   0.4768   0.1334
  -3.000   0.0674   0.00992   0.00283  -0.0649   0.4738   0.1361
  -2.750   0.0945   0.00988   0.00277  -0.0646   0.4706   0.1397
  -2.500   0.1220   0.00979   0.00271  -0.0644   0.4684   0.1441
  -2.250   0.1497   0.00973   0.00266  -0.0643   0.4658   0.1489
  -2.000   0.1769   0.00965   0.00260  -0.0640   0.4629   0.1565
  -1.750   0.2040   0.00958   0.00256  -0.0638   0.4600   0.1664
  -1.500   0.2305   0.00950   0.00251  -0.0634   0.4568   0.1809
  -1.250   0.2565   0.00940   0.00247  -0.0630   0.4534   0.2010
  -1.000   0.2830   0.00927   0.00243  -0.0627   0.4511   0.2273
  -0.750   0.3095   0.00914   0.00240  -0.0624   0.4488   0.2549
  -0.500   0.3360   0.00904   0.00238  -0.0620   0.4458   0.2819
  -0.250   0.3625   0.00897   0.00237  -0.0617   0.4426   0.3060
   0.000   0.3889   0.00893   0.00238  -0.0614   0.4393   0.3276
   0.250   0.4154   0.00893   0.00241  -0.0610   0.4361   0.3443
   0.500   0.4427   0.00890   0.00243  -0.0608   0.4338   0.3593
   0.750   0.4700   0.00889   0.00245  -0.0607   0.4312   0.3714
   1.000   0.4973   0.00890   0.00248  -0.0605   0.4280   0.3831
   1.250   0.5241   0.00891   0.00252  -0.0602   0.4248   0.3942
   1.500   0.5508   0.00896   0.00256  -0.0599   0.4216   0.4059
   1.750   0.5768   0.00898   0.00262  -0.0595   0.4181   0.4221
   2.000   0.6038   0.00898   0.00267  -0.0593   0.4156   0.4361
   2.250   0.6309   0.00901   0.00272  -0.0591   0.4127   0.4464
   2.500   0.6573   0.00904   0.00278  -0.0588   0.4095   0.4567
   2.750   0.6834   0.00910   0.00285  -0.0584   0.4061   0.4679
   3.000   0.7086   0.00917   0.00293  -0.0579   0.4024   0.4796
   3.250   0.7351   0.00921   0.00300  -0.0576   0.3996   0.4901
   3.500   0.7611   0.00924   0.00307  -0.0573   0.3969   0.5023
   3.750   0.7868   0.00928   0.00314  -0.0569   0.3936   0.5154
   4.000   0.8116   0.00934   0.00323  -0.0563   0.3898   0.5287
   4.250   0.8355   0.00943   0.00333  -0.0556   0.3859   0.5418
   4.500   0.8603   0.00947   0.00343  -0.0550   0.3832   0.5580
   4.750   0.8846   0.00949   0.00352  -0.0544   0.3803   0.5803
   5.000   0.9072   0.00949   0.00363  -0.0534   0.3768   0.6186
   5.250   0.9268   0.00945   0.00376  -0.0519   0.3729   0.6779
   5.500   0.9439   0.00943   0.00391  -0.0498   0.3691   0.7449
   5.750   0.9611   0.00934   0.00405  -0.0477   0.3666   0.8166
   6.000   0.9849   0.00928   0.00423  -0.0468   0.3635   0.8989
   6.250   1.0525   0.00952   0.00454  -0.0554   0.3582   0.9480
   6.500   1.1046   0.00981   0.00480  -0.0609   0.3530   0.9623
   6.750   1.1457   0.01001   0.00500  -0.0639   0.3496   0.9712
   7.000   1.1777   0.01020   0.00519  -0.0650   0.3455   0.9798
   7.250   1.2089   0.01044   0.00541  -0.0660   0.3410   0.9864
   7.500   1.2354   0.01072   0.00566  -0.0661   0.3369   0.9944
   8.000   1.3012   0.01116   0.00611  -0.0689   0.3298   1.0000
   8.250   1.3119   0.01137   0.00631  -0.0658   0.3261   1.0000
   8.500   1.3175   0.01160   0.00653  -0.0618   0.3223   1.0000
   8.750   1.3275   0.01185   0.00678  -0.0587   0.3190   1.0000
   9.000   1.3417   0.01207   0.00702  -0.0564   0.3162   1.0000
   9.250   1.3553   0.01236   0.00732  -0.0542   0.3125   1.0000
   9.500   1.3677   0.01273   0.00768  -0.0519   0.3086   1.0000
   9.750   1.3782   0.01321   0.00816  -0.0494   0.3043   1.0000
  10.000   1.3941   0.01358   0.00855  -0.0479   0.3017   1.0000
  10.250   1.4089   0.01402   0.00901  -0.0464   0.2985   1.0000
  10.500   1.4213   0.01461   0.00961  -0.0447   0.2944   1.0000
  10.750   1.4315   0.01537   0.01038  -0.0429   0.2906   1.0000
  11.000   1.4441   0.01611   0.01114  -0.0416   0.2874   1.0000
  11.250   1.4580   0.01686   0.01192  -0.0406   0.2843   1.0000
  11.500   1.4700   0.01780   0.01288  -0.0396   0.2807   1.0000
  11.750   1.4787   0.01905   0.01414  -0.0386   0.2767   1.0000
  12.000   1.4870   0.02041   0.01553  -0.0377   0.2729   1.0000
  12.250   1.4986   0.02157   0.01672  -0.0371   0.2690   1.0000
  12.500   1.5065   0.02302   0.01819  -0.0363   0.2646   1.0000
  12.750   1.5087   0.02488   0.02007  -0.0352   0.2600   1.0000
  13.000   1.5156   0.02639   0.02160  -0.0344   0.2558   1.0000
  13.250   1.5223   0.02793   0.02317  -0.0336   0.2522   1.0000
  13.500   1.5219   0.03001   0.02526  -0.0326   0.2471   1.0000
  13.750   1.5222   0.03206   0.02733  -0.0316   0.2435   1.0000
  14.000   1.5282   0.03366   0.02897  -0.0309   0.2396   1.0000
  14.250   1.5302   0.03564   0.03098  -0.0301   0.2355   1.0000
  14.500   1.5294   0.03789   0.03325  -0.0293   0.2312   1.0000
  14.750   1.5301   0.04010   0.03548  -0.0286   0.2273   1.0000
  15.000   1.5351   0.04195   0.03736  -0.0281   0.2232   1.0000
  15.250   1.5342   0.04440   0.03984  -0.0276   0.2190   1.0000
  15.500   1.5309   0.04707   0.04252  -0.0270   0.2141   1.0000
  15.750   1.5348   0.04911   0.04459  -0.0266   0.2104   1.0000
  16.000   1.5364   0.05139   0.04690  -0.0263   0.2062   1.0000
  16.250   1.5298   0.05451   0.05003  -0.0258   0.2015   1.0000
  16.500   1.5348   0.05650   0.05205  -0.0256   0.1979   1.0000
  16.750   1.5303   0.05949   0.05506  -0.0253   0.1921   1.0000
  17.000   1.5257   0.06251   0.05809  -0.0251   0.1872   1.0000
  17.250   1.5257   0.06511   0.06072  -0.0250   0.1828   1.0000
  17.500   1.5211   0.06818   0.06380  -0.0249   0.1771   1.0000
  17.750   1.5168   0.07129   0.06693  -0.0249   0.1732   1.0000
  18.000   1.5184   0.07378   0.06945  -0.0249   0.1687   1.0000
  18.250   1.5115   0.07725   0.07294  -0.0250   0.1642   1.0000
  18.500   1.5103   0.08007   0.07578  -0.0251   0.1602   1.0000
  18.750   1.5077   0.08311   0.07886  -0.0253   0.1560   1.0000
  19.000   1.4989   0.08689   0.08264  -0.0256   0.1504   1.0000
  19.250   1.4966   0.08995   0.08574  -0.0259   0.1458   1.0000
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