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DEFIANT CANARD BL20 AIRFOIL (defcnd1-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: DEFIANT CANARD BL20 AIRFOIL (defcnd1-il)
Reynolds number: 1,000,000
Max Cl/Cd: 124.87 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-defcnd1-il-1000000.txt
Download as CSV file: xf-defcnd1-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.7574   0.11293   0.10986  -0.0467   1.0000   0.0180
 -18.750  -0.7665   0.10782   0.10469  -0.0494   1.0000   0.0181
 -18.500  -0.7740   0.10135   0.09816  -0.0540   0.9549   0.0183
 -18.250  -0.7576   0.08993   0.08651  -0.0715   0.9154   0.0186
 -18.000  -0.7368   0.07699   0.07314  -0.0932   0.8582   0.0190
 -17.750  -0.7489   0.06985   0.06546  -0.1003   0.7626   0.0195
 -17.500  -0.7706   0.06377   0.05918  -0.1038   0.7437   0.0195
 -17.250  -0.7904   0.05824   0.05349  -0.1068   0.7316   0.0196
 -17.000  -0.8100   0.05309   0.04818  -0.1095   0.7220   0.0196
 -16.750  -0.8263   0.04858   0.04355  -0.1116   0.7140   0.0198
 -16.500  -0.8393   0.04458   0.03942  -0.1133   0.7060   0.0199
 -16.250  -0.8484   0.04107   0.03582  -0.1146   0.7000   0.0202
 -16.000  -0.8565   0.03776   0.03239  -0.1158   0.6935   0.0204
 -15.750  -0.8611   0.03489   0.02940  -0.1166   0.6866   0.0207
 -15.500  -0.8629   0.03229   0.02671  -0.1173   0.6816   0.0209
 -15.250  -0.8657   0.02976   0.02409  -0.1177   0.6760   0.0211
 -15.000  -0.8735   0.02714   0.02137  -0.1176   0.6707   0.0216
 -14.750  -0.8757   0.02529   0.01942  -0.1168   0.6644   0.0220
 -14.500  -0.8760   0.02372   0.01780  -0.1155   0.6606   0.0224
 -14.250  -0.8734   0.02251   0.01653  -0.1139   0.6560   0.0229
 -14.000  -0.8690   0.02153   0.01548  -0.1120   0.6513   0.0233
 -13.750  -0.8626   0.02075   0.01461  -0.1099   0.6462   0.0239
 -13.500  -0.8583   0.01991   0.01371  -0.1074   0.6420   0.0246
 -13.250  -0.8527   0.01914   0.01292  -0.1048   0.6384   0.0253
 -13.000  -0.8453   0.01850   0.01223  -0.1021   0.6341   0.0263
 -12.750  -0.8353   0.01799   0.01166  -0.0996   0.6298   0.0272
 -12.500  -0.8272   0.01744   0.01106  -0.0967   0.6252   0.0284
 -12.250  -0.8180   0.01694   0.01054  -0.0938   0.6218   0.0297
 -12.000  -0.8069   0.01655   0.01012  -0.0910   0.6188   0.0314
 -11.750  -0.7953   0.01610   0.00966  -0.0884   0.6152   0.0336
 -11.500  -0.7799   0.01565   0.00919  -0.0864   0.6114   0.0366
 -11.250  -0.7634   0.01524   0.00876  -0.0846   0.6072   0.0402
 -11.000  -0.7456   0.01487   0.00836  -0.0829   0.6026   0.0440
 -10.750  -0.7263   0.01447   0.00797  -0.0815   0.6001   0.0485
 -10.500  -0.7064   0.01408   0.00760  -0.0802   0.5972   0.0531
 -10.250  -0.6858   0.01372   0.00725  -0.0789   0.5938   0.0580
 -10.000  -0.6645   0.01340   0.00693  -0.0777   0.5902   0.0629
  -9.750  -0.6426   0.01312   0.00664  -0.0766   0.5862   0.0680
  -9.500  -0.6197   0.01289   0.00640  -0.0757   0.5822   0.0730
  -9.250  -0.5953   0.01266   0.00618  -0.0750   0.5797   0.0785
  -9.000  -0.5709   0.01243   0.00598  -0.0743   0.5767   0.0837
  -8.750  -0.5456   0.01226   0.00581  -0.0737   0.5736   0.0879
  -8.500  -0.5202   0.01212   0.00565  -0.0731   0.5702   0.0920
  -8.250  -0.4943   0.01202   0.00550  -0.0726   0.5664   0.0952
  -8.000  -0.4690   0.01188   0.00536  -0.0720   0.5626   0.0988
  -7.750  -0.4420   0.01177   0.00524  -0.0717   0.5602   0.1019
  -7.500  -0.4152   0.01165   0.00510  -0.0713   0.5574   0.1044
  -7.250  -0.3895   0.01148   0.00494  -0.0708   0.5544   0.1076
  -7.000  -0.3628   0.01139   0.00483  -0.0704   0.5512   0.1104
  -6.750  -0.3359   0.01133   0.00472  -0.0701   0.5477   0.1125
  -6.500  -0.3096   0.01125   0.00459  -0.0696   0.5437   0.1149
  -6.250  -0.2833   0.01107   0.00444  -0.0692   0.5415   0.1186
  -6.000  -0.2558   0.01098   0.00436  -0.0690   0.5390   0.1218
  -5.750  -0.2281   0.01091   0.00427  -0.0688   0.5362   0.1240
  -5.500  -0.2016   0.01079   0.00411  -0.0684   0.5332   0.1262
  -5.250  -0.1759   0.01063   0.00393  -0.0678   0.5299   0.1293
  -5.000  -0.1496   0.01056   0.00383  -0.0674   0.5258   0.1320
  -4.750  -0.1222   0.01045   0.00372  -0.0671   0.5235   0.1343
  -4.500  -0.0945   0.01037   0.00362  -0.0669   0.5212   0.1363
  -4.250  -0.0675   0.01024   0.00349  -0.0666   0.5186   0.1391
  -4.000  -0.0408   0.01010   0.00336  -0.0663   0.5157   0.1430
  -3.750  -0.0139   0.01001   0.00325  -0.0659   0.5125   0.1466
  -3.500   0.0132   0.00998   0.00318  -0.0656   0.5090   0.1497
  -3.250   0.0398   0.00989   0.00308  -0.0653   0.5059   0.1551
  -3.000   0.0672   0.00976   0.00300  -0.0650   0.5039   0.1615
  -2.750   0.0943   0.00963   0.00291  -0.0648   0.5013   0.1707
  -2.500   0.1210   0.00948   0.00281  -0.0644   0.4984   0.1857
  -2.000   0.1714   0.00907   0.00264  -0.0634   0.4924   0.2548
  -1.750   0.1964   0.00894   0.00261  -0.0628   0.4885   0.2939
  -1.500   0.2233   0.00880   0.00259  -0.0625   0.4866   0.3234
  -1.250   0.2507   0.00871   0.00257  -0.0623   0.4841   0.3459
  -1.000   0.2782   0.00866   0.00256  -0.0621   0.4814   0.3641
  -0.750   0.3054   0.00862   0.00256  -0.0619   0.4786   0.3804
  -0.500   0.3325   0.00861   0.00256  -0.0616   0.4754   0.3939
  -0.250   0.3595   0.00866   0.00259  -0.0613   0.4716   0.4058
   0.000   0.3869   0.00864   0.00262  -0.0611   0.4692   0.4186
   0.250   0.4150   0.00864   0.00263  -0.0611   0.4669   0.4284
   0.500   0.4426   0.00862   0.00265  -0.0609   0.4642   0.4391
   0.750   0.4704   0.00864   0.00267  -0.0608   0.4612   0.4475
   1.000   0.4970   0.00865   0.00269  -0.0605   0.4580   0.4578
   1.250   0.5236   0.00872   0.00274  -0.0602   0.4544   0.4669
   1.500   0.5506   0.00874   0.00279  -0.0599   0.4517   0.4774
   1.750   0.5783   0.00874   0.00282  -0.0598   0.4493   0.4896
   2.000   0.6052   0.00872   0.00286  -0.0596   0.4464   0.5028
   2.250   0.6322   0.00876   0.00290  -0.0594   0.4434   0.5135
   2.500   0.6579   0.00878   0.00295  -0.0589   0.4402   0.5265
   2.750   0.6829   0.00884   0.00302  -0.0584   0.4364   0.5409
   3.000   0.7091   0.00883   0.00308  -0.0580   0.4339   0.5593
   3.250   0.7347   0.00878   0.00313  -0.0575   0.4313   0.5848
   3.500   0.7586   0.00870   0.00320  -0.0567   0.4285   0.6288
   3.750   0.7788   0.00855   0.00328  -0.0552   0.4254   0.7071
   4.000   0.7956   0.00839   0.00339  -0.0529   0.4220   0.8019
   4.250   0.8175   0.00833   0.00357  -0.0515   0.4182   0.8893
   4.500   0.8712   0.00841   0.00377  -0.0569   0.4155   0.9395
   4.750   0.9250   0.00856   0.00393  -0.0624   0.4118   0.9565
   5.000   0.9674   0.00873   0.00407  -0.0655   0.4078   0.9668
   5.250   1.0009   0.00895   0.00424  -0.0668   0.4037   0.9762
   5.500   1.0377   0.00912   0.00441  -0.0688   0.4003   0.9813
   5.750   1.0766   0.00925   0.00453  -0.0712   0.3972   0.9857
   6.000   1.1126   0.00941   0.00468  -0.0730   0.3933   0.9904
   6.250   1.1489   0.00960   0.00484  -0.0750   0.3893   0.9937
   6.500   1.1859   0.00983   0.00503  -0.0772   0.3847   0.9967
   6.750   1.2257   0.00993   0.00515  -0.0799   0.3817   0.9989
   7.000   1.2574   0.01007   0.00529  -0.0809   0.3779   1.0000
   7.250   1.2738   0.01022   0.00543  -0.0789   0.3743   1.0000
   7.500   1.2880   0.01043   0.00561  -0.0764   0.3705   1.0000
   7.750   1.3038   0.01060   0.00579  -0.0743   0.3673   1.0000
   8.000   1.3218   0.01072   0.00593  -0.0725   0.3643   1.0000
   8.250   1.3378   0.01089   0.00610  -0.0704   0.3607   1.0000
   8.500   1.3509   0.01111   0.00631  -0.0678   0.3570   1.0000
   8.750   1.3555   0.01136   0.00654  -0.0635   0.3531   1.0000
   9.000   1.3687   0.01153   0.00674  -0.0609   0.3503   1.0000
   9.250   1.3836   0.01172   0.00694  -0.0587   0.3469   1.0000
   9.500   1.3971   0.01197   0.00721  -0.0564   0.3432   1.0000
   9.750   1.4082   0.01234   0.00756  -0.0538   0.3392   1.0000
  10.000   1.4201   0.01274   0.00797  -0.0515   0.3354   1.0000
  10.250   1.4380   0.01302   0.00828  -0.0502   0.3325   1.0000
  10.500   1.4530   0.01341   0.00868  -0.0486   0.3286   1.0000
  10.750   1.4651   0.01395   0.00923  -0.0467   0.3247   1.0000
  11.000   1.4733   0.01471   0.00998  -0.0445   0.3203   1.0000
  11.250   1.4907   0.01517   0.01048  -0.0436   0.3175   1.0000
  11.500   1.5052   0.01579   0.01113  -0.0424   0.3139   1.0000
  11.750   1.5161   0.01666   0.01202  -0.0411   0.3098   1.0000
  12.000   1.5223   0.01792   0.01327  -0.0396   0.3052   1.0000
  12.250   1.5367   0.01877   0.01417  -0.0390   0.3016   1.0000
  12.500   1.5485   0.01986   0.01529  -0.0383   0.2972   1.0000
  12.750   1.5553   0.02133   0.01677  -0.0373   0.2929   1.0000
  13.000   1.5596   0.02300   0.01844  -0.0363   0.2880   1.0000
  13.250   1.5716   0.02412   0.01962  -0.0358   0.2847   1.0000
  13.500   1.5781   0.02565   0.02117  -0.0350   0.2804   1.0000
  13.750   1.5786   0.02761   0.02314  -0.0339   0.2761   1.0000
  14.000   1.5831   0.02928   0.02484  -0.0330   0.2719   1.0000
  14.250   1.5900   0.03080   0.02641  -0.0323   0.2682   1.0000
  14.500   1.5922   0.03268   0.02830  -0.0314   0.2642   1.0000
  14.750   1.5865   0.03521   0.03083  -0.0303   0.2590   1.0000
  15.000   1.5935   0.03683   0.03251  -0.0298   0.2558   1.0000
  15.250   1.5996   0.03851   0.03422  -0.0293   0.2522   1.0000
  15.500   1.5972   0.04098   0.03671  -0.0286   0.2477   1.0000
  15.750   1.5947   0.04348   0.03921  -0.0279   0.2434   1.0000
  16.000   1.6019   0.04520   0.04099  -0.0276   0.2401   1.0000
  16.250   1.6046   0.04729   0.04310  -0.0272   0.2356   1.0000
  16.500   1.5981   0.05030   0.04612  -0.0266   0.2310   1.0000
  16.750   1.6017   0.05238   0.04823  -0.0263   0.2266   1.0000
  17.000   1.6028   0.05474   0.05064  -0.0261   0.2226   1.0000
  17.250   1.5999   0.05746   0.05335  -0.0257   0.2181   1.0000
  17.500   1.5964   0.06034   0.05627  -0.0255   0.2141   1.0000
  17.750   1.6018   0.06231   0.05828  -0.0254   0.2107   1.0000
  18.000   1.6004   0.06501   0.06101  -0.0253   0.2067   1.0000
  18.250   1.5926   0.06837   0.06437  -0.0252   0.2018   1.0000
  18.500   1.5964   0.07057   0.06663  -0.0252   0.1986   1.0000
  18.750   1.5959   0.07327   0.06936  -0.0252   0.1947   1.0000
  19.000   1.5913   0.07638   0.07248  -0.0253   0.1902   1.0000
  19.250   1.5867   0.07955   0.07569  -0.0254   0.1863   1.0000
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