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DEFIANT CANARD BL20 AIRFOIL (defcnd1-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: DEFIANT CANARD BL20 AIRFOIL (defcnd1-il)
Reynolds number: 200,000
Max Cl/Cd: 60.1 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-defcnd1-il-200000-n5.txt
Download as CSV file: xf-defcnd1-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.5312   0.09163   0.08621  -0.0805   0.7832   0.0346
 -16.250  -0.5394   0.08574   0.08014  -0.0850   0.7654   0.0355
 -16.000  -0.5516   0.07975   0.07401  -0.0891   0.7542   0.0362
 -15.750  -0.5651   0.07377   0.06786  -0.0932   0.7452   0.0368
 -15.500  -0.5815   0.06800   0.06194  -0.0967   0.7375   0.0375
 -15.250  -0.5974   0.06281   0.05659  -0.0996   0.7301   0.0381
 -15.000  -0.6122   0.05808   0.05168  -0.1021   0.7235   0.0388
 -14.750  -0.6259   0.05367   0.04716  -0.1043   0.7171   0.0394
 -14.500  -0.6392   0.04951   0.04288  -0.1063   0.7107   0.0401
 -14.250  -0.6498   0.04580   0.03902  -0.1079   0.7052   0.0410
 -14.000  -0.6577   0.04246   0.03558  -0.1092   0.6993   0.0420
 -13.750  -0.6627   0.03955   0.03252  -0.1102   0.6936   0.0434
 -13.500  -0.6690   0.03672   0.02959  -0.1109   0.6885   0.0446
 -13.250  -0.6728   0.03434   0.02710  -0.1111   0.6840   0.0461
 -13.000  -0.6735   0.03239   0.02503  -0.1108   0.6789   0.0480
 -12.750  -0.6757   0.03058   0.02317  -0.1100   0.6738   0.0499
 -12.500  -0.6749   0.02916   0.02164  -0.1087   0.6690   0.0521
 -12.000  -0.6690   0.02690   0.01921  -0.1052   0.6600   0.0571
 -11.750  -0.6634   0.02599   0.01824  -0.1031   0.6554   0.0602
 -11.500  -0.6563   0.02521   0.01739  -0.1009   0.6511   0.0636
 -11.250  -0.6482   0.02454   0.01666  -0.0986   0.6472   0.0669
 -11.000  -0.6382   0.02402   0.01603  -0.0962   0.6436   0.0709
 -10.750  -0.6281   0.02356   0.01557  -0.0938   0.6393   0.0744
 -10.500  -0.6144   0.02317   0.01510  -0.0918   0.6349   0.0787
 -10.250  -0.5990   0.02281   0.01470  -0.0901   0.6307   0.0826
 -10.000  -0.5814   0.02247   0.01425  -0.0886   0.6270   0.0869
  -9.750  -0.5633   0.02219   0.01388  -0.0872   0.6238   0.0909
  -9.500  -0.5435   0.02188   0.01349  -0.0859   0.6202   0.0950
  -9.250  -0.5239   0.02161   0.01319  -0.0847   0.6162   0.0988
  -9.000  -0.5026   0.02136   0.01281  -0.0837   0.6121   0.1031
  -8.750  -0.4825   0.02110   0.01252  -0.0825   0.6084   0.1067
  -8.500  -0.4608   0.02090   0.01220  -0.0815   0.6050   0.1111
  -8.250  -0.4390   0.02066   0.01187  -0.0805   0.6020   0.1151
  -8.000  -0.4171   0.02041   0.01162  -0.0796   0.5985   0.1189
  -7.750  -0.3942   0.02018   0.01130  -0.0787   0.5947   0.1227
  -7.500  -0.3714   0.01988   0.01094  -0.0779   0.5911   0.1259
  -7.250  -0.3489   0.01956   0.01060  -0.0770   0.5876   0.1290
  -7.000  -0.3254   0.01932   0.01027  -0.0762   0.5846   0.1324
  -6.750  -0.3013   0.01911   0.00996  -0.0755   0.5816   0.1357
  -6.500  -0.2779   0.01880   0.00965  -0.0747   0.5783   0.1387
  -6.250  -0.2546   0.01851   0.00938  -0.0740   0.5748   0.1420
  -6.000  -0.2305   0.01828   0.00911  -0.0733   0.5714   0.1454
  -5.750  -0.2060   0.01807   0.00881  -0.0726   0.5681   0.1489
  -5.500  -0.1820   0.01781   0.00851  -0.0719   0.5652   0.1523
  -5.250  -0.1581   0.01758   0.00826  -0.0711   0.5625   0.1561
  -5.000  -0.1337   0.01738   0.00807  -0.0705   0.5592   0.1603
  -4.750  -0.1087   0.01722   0.00787  -0.0699   0.5559   0.1644
  -4.500  -0.0850   0.01697   0.00765  -0.0691   0.5525   0.1691
  -4.250  -0.0605   0.01677   0.00744  -0.0685   0.5494   0.1747
  -4.000  -0.0353   0.01661   0.00722  -0.0679   0.5465   0.1807
  -3.750  -0.0108   0.01642   0.00701  -0.0673   0.5440   0.1887
  -3.500   0.0137   0.01626   0.00691  -0.0666   0.5410   0.1986
  -3.250   0.0380   0.01608   0.00680  -0.0660   0.5377   0.2127
  -3.000   0.0622   0.01589   0.00668  -0.0653   0.5344   0.2315
  -2.750   0.0863   0.01569   0.00657  -0.0646   0.5312   0.2568
  -2.500   0.1110   0.01552   0.00647  -0.0640   0.5284   0.2867
  -2.250   0.1359   0.01540   0.00641  -0.0634   0.5259   0.3170
  -2.000   0.1610   0.01536   0.00643  -0.0628   0.5232   0.3430
  -1.750   0.1861   0.01534   0.00646  -0.0622   0.5198   0.3643
  -1.500   0.2115   0.01532   0.00648  -0.0617   0.5164   0.3826
  -1.250   0.2371   0.01529   0.00648  -0.0612   0.5132   0.3990
  -1.000   0.2630   0.01529   0.00646  -0.0607   0.5104   0.4143
  -0.750   0.2897   0.01530   0.00643  -0.0604   0.5080   0.4285
  -0.500   0.3156   0.01533   0.00646  -0.0599   0.5052   0.4417
  -0.250   0.3407   0.01537   0.00654  -0.0594   0.5018   0.4531
   0.000   0.3661   0.01540   0.00659  -0.0589   0.4983   0.4653
   0.250   0.3917   0.01541   0.00663  -0.0584   0.4953   0.4772
   0.500   0.4175   0.01542   0.00664  -0.0579   0.4925   0.4925
   0.750   0.4432   0.01542   0.00663  -0.0574   0.4899   0.5097
   1.000   0.4682   0.01543   0.00669  -0.0569   0.4871   0.5254
   1.250   0.4920   0.01545   0.00681  -0.0561   0.4836   0.5411
   1.500   0.5161   0.01547   0.00691  -0.0554   0.4803   0.5584
   2.000   0.5645   0.01543   0.00701  -0.0539   0.4743   0.5990
   2.250   0.5892   0.01539   0.00703  -0.0532   0.4716   0.6244
   2.500   0.6120   0.01539   0.00717  -0.0522   0.4687   0.6573
   2.750   0.6335   0.01537   0.00738  -0.0510   0.4654   0.7024
   3.000   0.6579   0.01534   0.00759  -0.0501   0.4619   0.7636
   3.250   0.6958   0.01538   0.00781  -0.0520   0.4584   0.8381
   3.500   0.7505   0.01554   0.00799  -0.0572   0.4551   0.8944
   3.750   0.7983   0.01575   0.00817  -0.0612   0.4520   0.9279
   4.000   0.8404   0.01601   0.00848  -0.0643   0.4478   0.9501
   4.250   0.8786   0.01624   0.00871  -0.0666   0.4438   0.9666
   4.500   0.9149   0.01644   0.00888  -0.0685   0.4404   0.9804
   4.750   0.9541   0.01663   0.00899  -0.0710   0.4373   0.9914
   5.000   0.9946   0.01687   0.00919  -0.0739   0.4339   1.0000
   5.250   1.0090   0.01710   0.00947  -0.0717   0.4302   1.0000
   5.500   1.0245   0.01732   0.00969  -0.0696   0.4267   1.0000
   5.750   1.0410   0.01752   0.00987  -0.0678   0.4236   1.0000
   6.000   1.0588   0.01770   0.01000  -0.0661   0.4206   1.0000
   6.250   1.0764   0.01791   0.01016  -0.0644   0.4176   1.0000
   6.500   1.0886   0.01822   0.01054  -0.0619   0.4139   1.0000
   6.750   1.1019   0.01851   0.01085  -0.0595   0.4103   1.0000
   7.000   1.1161   0.01878   0.01110  -0.0573   0.4069   1.0000
   7.250   1.1318   0.01902   0.01130  -0.0554   0.4039   1.0000
   7.500   1.1469   0.01928   0.01152  -0.0533   0.4008   1.0000
   7.750   1.1503   0.01968   0.01200  -0.0494   0.3971   1.0000
   8.000   1.1569   0.02008   0.01244  -0.0461   0.3935   1.0000
   8.250   1.1670   0.02047   0.01283  -0.0435   0.3902   1.0000
   8.500   1.1805   0.02082   0.01314  -0.0415   0.3870   1.0000
   8.750   1.1935   0.02124   0.01354  -0.0396   0.3838   1.0000
   9.000   1.1970   0.02199   0.01439  -0.0367   0.3797   1.0000
   9.250   1.2042   0.02271   0.01515  -0.0345   0.3758   1.0000
   9.500   1.2155   0.02333   0.01577  -0.0328   0.3723   1.0000
   9.750   1.2312   0.02381   0.01620  -0.0316   0.3691   1.0000
  10.000   1.2351   0.02491   0.01739  -0.0296   0.3651   1.0000
  10.250   1.2378   0.02618   0.01874  -0.0278   0.3606   1.0000
  10.500   1.2468   0.02719   0.01976  -0.0266   0.3568   1.0000
  10.750   1.2613   0.02788   0.02043  -0.0257   0.3536   1.0000
  11.000   1.2678   0.02916   0.02174  -0.0245   0.3498   1.0000
  11.250   1.2662   0.03105   0.02375  -0.0231   0.3449   1.0000
  11.500   1.2731   0.03239   0.02511  -0.0222   0.3407   1.0000
  11.750   1.2879   0.03313   0.02582  -0.0215   0.3374   1.0000
  12.000   1.2921   0.03475   0.02748  -0.0206   0.3336   1.0000
  12.250   1.2874   0.03713   0.02998  -0.0195   0.3287   1.0000
  12.500   1.2935   0.03864   0.03151  -0.0188   0.3245   1.0000
  12.750   1.3094   0.03932   0.03215  -0.0182   0.3213   1.0000
  13.000   1.3086   0.04150   0.03441  -0.0175   0.3171   1.0000
  13.250   1.3021   0.04427   0.03728  -0.0167   0.3123   1.0000
  13.500   1.3092   0.04581   0.03884  -0.0162   0.3083   1.0000
  13.750   1.3273   0.04633   0.03932  -0.0158   0.3053   1.0000
  14.000   1.3198   0.04938   0.04248  -0.0153   0.3007   1.0000
  14.250   1.3127   0.05248   0.04568  -0.0149   0.2959   1.0000
  14.500   1.3222   0.05392   0.04714  -0.0146   0.2923   1.0000
  14.750   1.3428   0.05419   0.04735  -0.0143   0.2895   1.0000
  15.000   1.3254   0.05855   0.05186  -0.0141   0.2842   1.0000
  15.250   1.3195   0.06176   0.05517  -0.0140   0.2797   1.0000
  15.500   1.3320   0.06292   0.05633  -0.0138   0.2765   1.0000
  15.750   1.3547   0.06293   0.05630  -0.0135   0.2741   1.0000
  16.000   1.3275   0.06869   0.06224  -0.0138   0.2684   1.0000
  16.250   1.3215   0.07209   0.06571  -0.0139   0.2637   1.0000
  16.500   1.3373   0.07290   0.06652  -0.0138   0.2610   1.0000
  16.750   1.3641   0.07235   0.06592  -0.0135   0.2586   1.0000
  17.000   1.3148   0.08113   0.07494  -0.0144   0.2513   1.0000
  17.250   1.3203   0.08323   0.07707  -0.0146   0.2474   1.0000
  17.500   1.3459   0.08278   0.07657  -0.0144   0.2447   1.0000
  17.750   1.3069   0.09060   0.08457  -0.0155   0.2379   1.0000
  18.000   1.3041   0.09385   0.08787  -0.0160   0.2331   1.0000
  18.250   1.3323   0.09298   0.08694  -0.0158   0.2303   1.0000
  18.500   1.2892   0.10168   0.09583  -0.0174   0.2234   1.0000
  18.750   1.2901   0.10450   0.09869  -0.0180   0.2187   1.0000
  19.000   1.3182   0.10355   0.09769  -0.0178   0.2160   1.0000
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