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DEFIANT CANARD BL20 AIRFOIL (defcnd1-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: DEFIANT CANARD BL20 AIRFOIL (defcnd1-il)
Reynolds number: 500,000
Max Cl/Cd: 93.72 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-defcnd1-il-500000.txt
Download as CSV file: xf-defcnd1-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.7602   0.09119   0.08727  -0.0613   1.0000   0.0255
 -17.500  -0.7665   0.08680   0.08283  -0.0636   1.0000   0.0258
 -17.250  -0.7735   0.08232   0.07830  -0.0660   1.0000   0.0261
 -17.000  -0.7802   0.07796   0.07389  -0.0683   1.0000   0.0263
 -16.750  -0.7818   0.07268   0.06852  -0.0724   0.9485   0.0267
 -16.500  -0.7080   0.06251   0.05796  -0.0991   0.8763   0.0280
 -16.250  -0.7005   0.05758   0.05249  -0.1061   0.7768   0.0287
 -16.000  -0.7106   0.05381   0.04850  -0.1078   0.7546   0.0292
 -15.750  -0.7199   0.05020   0.04474  -0.1093   0.7417   0.0296
 -15.500  -0.7277   0.04680   0.04120  -0.1107   0.7318   0.0302
 -15.250  -0.7360   0.04348   0.03775  -0.1119   0.7237   0.0304
 -15.000  -0.7392   0.04065   0.03479  -0.1128   0.7165   0.0311
 -14.750  -0.7505   0.03720   0.03125  -0.1138   0.7099   0.0316
 -14.500  -0.7576   0.03420   0.02815  -0.1145   0.7037   0.0322
 -14.250  -0.7615   0.03159   0.02547  -0.1150   0.6979   0.0329
 -14.000  -0.7627   0.02945   0.02322  -0.1149   0.6920   0.0337
 -13.750  -0.7619   0.02772   0.02134  -0.1143   0.6861   0.0348
 -13.500  -0.7668   0.02581   0.01938  -0.1132   0.6814   0.0357
 -13.250  -0.7682   0.02434   0.01787  -0.1115   0.6766   0.0367
 -13.000  -0.7651   0.02327   0.01671  -0.1095   0.6717   0.0383
 -12.750  -0.7637   0.02225   0.01560  -0.1070   0.6670   0.0398
 -12.500  -0.7606   0.02135   0.01466  -0.1044   0.6625   0.0415
 -12.250  -0.7539   0.02060   0.01387  -0.1018   0.6583   0.0439
 -12.000  -0.7488   0.01984   0.01309  -0.0989   0.6538   0.0466
 -11.750  -0.7418   0.01920   0.01240  -0.0959   0.6495   0.0498
 -11.500  -0.7327   0.01874   0.01187  -0.0931   0.6453   0.0538
 -11.250  -0.7234   0.01826   0.01139  -0.0903   0.6417   0.0579
 -11.000  -0.7094   0.01778   0.01092  -0.0882   0.6381   0.0627
 -10.750  -0.6927   0.01736   0.01050  -0.0864   0.6341   0.0678
 -10.500  -0.6739   0.01702   0.01014  -0.0850   0.6301   0.0731
 -10.250  -0.6529   0.01679   0.00984  -0.0838   0.6259   0.0785
 -10.000  -0.6316   0.01656   0.00961  -0.0827   0.6220   0.0833
  -9.750  -0.6089   0.01634   0.00938  -0.0818   0.6188   0.0879
  -9.500  -0.5850   0.01619   0.00921  -0.0811   0.6151   0.0925
  -9.250  -0.5619   0.01599   0.00897  -0.0802   0.6115   0.0963
  -9.000  -0.5377   0.01587   0.00881  -0.0795   0.6078   0.1002
  -8.750  -0.5122   0.01584   0.00866  -0.0789   0.6038   0.1036
  -8.500  -0.4898   0.01557   0.00843  -0.0780   0.6006   0.1071
  -8.250  -0.4646   0.01546   0.00829  -0.0774   0.5973   0.1105
  -8.000  -0.4384   0.01540   0.00814  -0.0769   0.5939   0.1135
  -7.750  -0.4161   0.01506   0.00782  -0.0759   0.5906   0.1168
  -7.500  -0.3912   0.01492   0.00765  -0.0753   0.5873   0.1199
  -7.250  -0.3652   0.01491   0.00753  -0.0749   0.5834   0.1233
  -7.000  -0.3409   0.01467   0.00729  -0.0742   0.5805   0.1270
  -6.750  -0.3162   0.01446   0.00711  -0.0736   0.5774   0.1308
  -6.500  -0.2903   0.01433   0.00695  -0.0731   0.5742   0.1342
  -6.250  -0.2640   0.01424   0.00678  -0.0726   0.5711   0.1366
  -6.000  -0.2405   0.01389   0.00643  -0.0718   0.5680   0.1400
  -5.750  -0.2156   0.01373   0.00623  -0.0712   0.5645   0.1432
  -5.500  -0.1898   0.01359   0.00607  -0.0707   0.5615   0.1462
  -5.250  -0.1635   0.01345   0.00591  -0.0703   0.5586   0.1490
  -5.000  -0.1382   0.01324   0.00568  -0.0697   0.5556   0.1521
  -4.750  -0.1134   0.01300   0.00546  -0.0691   0.5526   0.1562
  -4.500  -0.0874   0.01285   0.00528  -0.0686   0.5495   0.1600
  -4.250  -0.0609   0.01277   0.00513  -0.0682   0.5463   0.1637
  -4.000  -0.0355   0.01262   0.00498  -0.0677   0.5431   0.1688
  -3.750  -0.0098   0.01244   0.00484  -0.0672   0.5405   0.1747
  -3.500   0.0166   0.01230   0.00471  -0.0667   0.5377   0.1810
  -3.250   0.0420   0.01209   0.00456  -0.0662   0.5347   0.1918
  -3.000   0.0674   0.01188   0.00440  -0.0657   0.5316   0.2079
  -2.750   0.0920   0.01162   0.00426  -0.0650   0.5287   0.2396
  -2.500   0.1165   0.01145   0.00421  -0.0645   0.5253   0.2872
  -2.250   0.1416   0.01125   0.00419  -0.0639   0.5230   0.3273
  -2.000   0.1676   0.01114   0.00418  -0.0634   0.5202   0.3556
  -1.750   0.1942   0.01108   0.00417  -0.0631   0.5170   0.3769
  -1.500   0.2211   0.01103   0.00415  -0.0627   0.5140   0.3939
  -1.250   0.2483   0.01103   0.00413  -0.0625   0.5111   0.4087
  -1.000   0.2756   0.01108   0.00415  -0.0623   0.5081   0.4231
  -0.750   0.3025   0.01110   0.00420  -0.0620   0.5053   0.4353
  -0.500   0.3297   0.01110   0.00421  -0.0617   0.5025   0.4467
  -0.250   0.3563   0.01107   0.00422  -0.0614   0.4994   0.4574
   0.000   0.3837   0.01108   0.00423  -0.0611   0.4964   0.4680
   0.250   0.4104   0.01107   0.00423  -0.0608   0.4936   0.4784
   0.500   0.4377   0.01113   0.00424  -0.0606   0.4905   0.4892
   0.750   0.4644   0.01118   0.00431  -0.0604   0.4874   0.4998
   1.000   0.4909   0.01117   0.00434  -0.0600   0.4847   0.5109
   1.250   0.5168   0.01114   0.00438  -0.0596   0.4818   0.5242
   1.500   0.5430   0.01113   0.00440  -0.0592   0.4787   0.5386
   1.750   0.5689   0.01111   0.00441  -0.0587   0.4757   0.5542
   2.000   0.5946   0.01111   0.00444  -0.0583   0.4725   0.5718
   2.250   0.6199   0.01114   0.00454  -0.0578   0.4696   0.5941
   2.500   0.6433   0.01105   0.00461  -0.0569   0.4669   0.6268
   2.750   0.6649   0.01090   0.00468  -0.0556   0.4637   0.6799
   3.000   0.6840   0.01067   0.00478  -0.0536   0.4607   0.7682
   3.250   0.7111   0.01054   0.00493  -0.0532   0.4577   0.8676
   3.500   0.7660   0.01074   0.00516  -0.0586   0.4539   0.9255
   3.750   0.8167   0.01093   0.00537  -0.0633   0.4504   0.9483
   4.000   0.8577   0.01108   0.00553  -0.0660   0.4469   0.9633
   4.250   0.9014   0.01125   0.00569  -0.0692   0.4434   0.9721
   4.500   0.9406   0.01142   0.00581  -0.0716   0.4399   0.9805
   4.750   0.9833   0.01166   0.00595  -0.0748   0.4358   0.9861
   5.000   1.0240   0.01181   0.00613  -0.0776   0.4326   0.9923
   5.250   1.0678   0.01191   0.00625  -0.0810   0.4289   0.9969
   5.500   1.1073   0.01202   0.00634  -0.0837   0.4251   1.0000
   5.750   1.1249   0.01216   0.00643  -0.0819   0.4218   1.0000
   6.000   1.1432   0.01238   0.00659  -0.0803   0.4183   1.0000
   6.250   1.1600   0.01248   0.00675  -0.0783   0.4155   1.0000
   6.500   1.1771   0.01261   0.00690  -0.0764   0.4122   1.0000
   6.750   1.1941   0.01275   0.00705  -0.0745   0.4088   1.0000
   7.000   1.2109   0.01292   0.00718  -0.0726   0.4054   1.0000
   7.250   1.2285   0.01318   0.00737  -0.0708   0.4016   1.0000
   7.500   1.2440   0.01333   0.00758  -0.0687   0.3987   1.0000
   7.750   1.2596   0.01350   0.00779  -0.0666   0.3953   1.0000
   8.000   1.2745   0.01369   0.00798  -0.0643   0.3917   1.0000
   8.250   1.2888   0.01392   0.00819  -0.0620   0.3882   1.0000
   8.500   1.3023   0.01422   0.00843  -0.0596   0.3846   1.0000
   8.750   1.3113   0.01441   0.00869  -0.0563   0.3817   1.0000
   9.000   1.3221   0.01465   0.00897  -0.0535   0.3783   1.0000
   9.250   1.3338   0.01493   0.00926  -0.0509   0.3746   1.0000
   9.500   1.3459   0.01528   0.00958  -0.0486   0.3709   1.0000
   9.750   1.3594   0.01568   0.00998  -0.0466   0.3673   1.0000
  10.000   1.3714   0.01608   0.01045  -0.0445   0.3639   1.0000
  10.250   1.3837   0.01653   0.01094  -0.0425   0.3602   1.0000
  10.500   1.3955   0.01706   0.01146  -0.0407   0.3564   1.0000
  10.750   1.4084   0.01767   0.01201  -0.0391   0.3522   1.0000
  11.000   1.4193   0.01834   0.01278  -0.0375   0.3489   1.0000
  11.250   1.4306   0.01907   0.01357  -0.0361   0.3452   1.0000
  11.500   1.4413   0.01990   0.01441  -0.0348   0.3413   1.0000
  11.750   1.4523   0.02079   0.01526  -0.0335   0.3373   1.0000
  12.000   1.4626   0.02179   0.01633  -0.0325   0.3336   1.0000
  12.250   1.4721   0.02291   0.01752  -0.0316   0.3297   1.0000
  12.500   1.4814   0.02408   0.01871  -0.0307   0.3258   1.0000
  12.750   1.4908   0.02522   0.01982  -0.0297   0.3217   1.0000
  13.000   1.4994   0.02648   0.02113  -0.0289   0.3179   1.0000
  13.250   1.5061   0.02795   0.02268  -0.0282   0.3140   1.0000
  13.500   1.5126   0.02942   0.02417  -0.0274   0.3099   1.0000
  13.750   1.5201   0.03072   0.02542  -0.0265   0.3053   1.0000
  14.000   1.5249   0.03238   0.02716  -0.0258   0.3016   1.0000
  14.250   1.5280   0.03421   0.02907  -0.0251   0.2973   1.0000
  14.500   1.5317   0.03597   0.03082  -0.0244   0.2926   1.0000
  14.750   1.5381   0.03746   0.03228  -0.0237   0.2882   1.0000
  15.000   1.5389   0.03966   0.03460  -0.0232   0.2841   1.0000
  15.250   1.5420   0.04164   0.03663  -0.0228   0.2802   1.0000
  15.500   1.5468   0.04340   0.03836  -0.0223   0.2759   1.0000
  15.750   1.5501   0.04538   0.04038  -0.0218   0.2717   1.0000
  16.000   1.5511   0.04772   0.04280  -0.0216   0.2676   1.0000
  16.250   1.5532   0.04992   0.04503  -0.0213   0.2635   1.0000
  16.500   1.5591   0.05161   0.04667  -0.0209   0.2591   1.0000
  16.750   1.5576   0.05430   0.04947  -0.0207   0.2551   1.0000
  17.000   1.5579   0.05680   0.05203  -0.0206   0.2510   1.0000
  17.250   1.5588   0.05918   0.05440  -0.0205   0.2464   1.0000
  17.500   1.5612   0.06140   0.05664  -0.0203   0.2423   1.0000
  17.750   1.5576   0.06443   0.05978  -0.0204   0.2379   1.0000
  18.000   1.5563   0.06716   0.06252  -0.0204   0.2333   1.0000
  18.250   1.5603   0.06921   0.06454  -0.0203   0.2290   1.0000
  18.500   1.5553   0.07252   0.06796  -0.0205   0.2252   1.0000
  18.750   1.5541   0.07532   0.07081  -0.0207   0.2209   1.0000
  19.000   1.5538   0.07796   0.07345  -0.0208   0.2169   1.0000
  19.250   1.5533   0.08069   0.07623  -0.0210   0.2131   1.0000
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