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DEFIANT CANARD BL20 AIRFOIL (defcnd1-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: DEFIANT CANARD BL20 AIRFOIL (defcnd1-il)
Reynolds number: 200,000
Max Cl/Cd: 52.84 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-defcnd1-il-200000.txt
Download as CSV file: xf-defcnd1-il-200000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.2905   0.18046   0.17682  -0.0265   1.0000   0.0622
 -17.000  -0.3044   0.17582   0.17223  -0.0317   1.0000   0.0649
 -16.750  -0.6970   0.08241   0.07762  -0.0764   1.0000   0.0435
 -16.250  -0.6827   0.07819   0.07355  -0.0775   1.0000   0.0451
 -16.000  -0.7039   0.07189   0.06710  -0.0814   1.0000   0.0455
 -15.750  -0.7204   0.06657   0.06165  -0.0846   1.0000   0.0459
 -15.500  -0.7352   0.06170   0.05666  -0.0875   1.0000   0.0465
 -15.250  -0.7481   0.05723   0.05206  -0.0900   1.0000   0.0471
 -15.000  -0.7612   0.05289   0.04755  -0.0925   1.0000   0.0478
 -14.750  -0.7362   0.04950   0.04415  -0.0985   0.9264   0.0494
 -14.500  -0.6852   0.04480   0.03903  -0.1124   0.8529   0.0524
 -14.250  -0.6716   0.04182   0.03573  -0.1166   0.8169   0.0543
 -14.000  -0.6621   0.03997   0.03377  -0.1180   0.7967   0.0561
 -13.750  -0.6640   0.03768   0.03123  -0.1185   0.7834   0.0580
 -13.500  -0.6640   0.03576   0.02916  -0.1183   0.7722   0.0598
 -13.250  -0.6598   0.03435   0.02769  -0.1179   0.7630   0.0618
 -13.000  -0.6617   0.03266   0.02583  -0.1169   0.7543   0.0643
 -12.750  -0.6596   0.03143   0.02453  -0.1157   0.7467   0.0666
 -12.500  -0.6577   0.03034   0.02339  -0.1141   0.7395   0.0694
 -12.250  -0.6564   0.02925   0.02219  -0.1121   0.7327   0.0725
 -12.000  -0.6519   0.02861   0.02149  -0.1100   0.7269   0.0756
 -11.750  -0.6496   0.02782   0.02059  -0.1073   0.7212   0.0794
 -11.500  -0.6437   0.02742   0.02021  -0.1046   0.7151   0.0828
 -11.250  -0.6412   0.02694   0.01954  -0.1013   0.7097   0.0868
 -11.000  -0.6325   0.02690   0.01949  -0.0986   0.7047   0.0902
 -10.750  -0.6252   0.02650   0.01892  -0.0958   0.6995   0.0948
 -10.500  -0.6094   0.02640   0.01889  -0.0941   0.6943   0.0985
 -10.250  -0.5991   0.02617   0.01839  -0.0915   0.6898   0.1032
 -10.000  -0.5792   0.02599   0.01827  -0.0904   0.6856   0.1071
  -9.750  -0.5639   0.02581   0.01798  -0.0886   0.6809   0.1117
  -9.500  -0.5455   0.02539   0.01753  -0.0873   0.6759   0.1159
  -9.250  -0.5255   0.02523   0.01735  -0.0861   0.6712   0.1203
  -9.000  -0.5093   0.02508   0.01692  -0.0842   0.6674   0.1249
  -8.750  -0.4851   0.02465   0.01658  -0.0839   0.6638   0.1294
  -8.500  -0.4654   0.02446   0.01635  -0.0826   0.6594   0.1343
  -8.250  -0.4447   0.02399   0.01581  -0.0816   0.6548   0.1391
  -8.000  -0.4213   0.02372   0.01557  -0.0809   0.6505   0.1440
  -7.750  -0.3998   0.02353   0.01520  -0.0798   0.6469   0.1489
  -7.500  -0.3758   0.02301   0.01462  -0.0793   0.6436   0.1534
  -7.250  -0.3522   0.02267   0.01436  -0.0786   0.6395   0.1578
  -7.000  -0.3293   0.02242   0.01402  -0.0777   0.6353   0.1623
  -6.750  -0.3053   0.02193   0.01346  -0.0771   0.6313   0.1664
  -6.500  -0.2799   0.02150   0.01304  -0.0767   0.6278   0.1709
  -6.250  -0.2547   0.02126   0.01270  -0.0761   0.6246   0.1755
  -6.000  -0.2308   0.02114   0.01246  -0.0754   0.6211   0.1796
  -5.750  -0.2063   0.02061   0.01206  -0.0749   0.6171   0.1842
  -5.500  -0.1819   0.02035   0.01182  -0.0743   0.6132   0.1891
  -5.250  -0.1567   0.02012   0.01151  -0.0737   0.6096   0.1942
  -5.000  -0.1311   0.01972   0.01109  -0.0732   0.6064   0.1995
  -4.750  -0.1056   0.01951   0.01085  -0.0728   0.6035   0.2056
  -4.500  -0.0817   0.01940   0.01074  -0.0720   0.5999   0.2120
  -4.250  -0.0590   0.01911   0.01059  -0.0712   0.5961   0.2194
  -4.000  -0.0347   0.01894   0.01042  -0.0705   0.5923   0.2289
  -3.750  -0.0111   0.01861   0.01018  -0.0697   0.5890   0.2408
  -3.500   0.0133   0.01832   0.00993  -0.0689   0.5861   0.2582
  -3.250   0.0373   0.01810   0.00980  -0.0682   0.5834   0.2877
  -3.000   0.0574   0.01799   0.00994  -0.0669   0.5800   0.3280
  -2.750   0.0787   0.01801   0.01011  -0.0657   0.5761   0.3672
  -2.500   0.1020   0.01804   0.01022  -0.0647   0.5725   0.3965
  -2.250   0.1272   0.01806   0.01023  -0.0640   0.5692   0.4203
  -2.000   0.1536   0.01807   0.01019  -0.0635   0.5664   0.4399
  -1.750   0.1808   0.01815   0.01021  -0.0632   0.5639   0.4568
  -1.500   0.2036   0.01836   0.01045  -0.0622   0.5605   0.4717
  -1.250   0.2264   0.01849   0.01064  -0.0613   0.5564   0.4856
  -1.000   0.2512   0.01851   0.01069  -0.0606   0.5527   0.4992
  -0.750   0.2776   0.01850   0.01062  -0.0602   0.5496   0.5136
  -0.500   0.3051   0.01842   0.01055  -0.0599   0.5470   0.5270
  -0.250   0.3335   0.01844   0.01052  -0.0599   0.5447   0.5404
   0.000   0.3551   0.01864   0.01079  -0.0588   0.5410   0.5539
   0.250   0.3770   0.01871   0.01099  -0.0578   0.5368   0.5674
   0.500   0.4016   0.01870   0.01103  -0.0572   0.5332   0.5836
   0.750   0.4273   0.01863   0.01101  -0.0566   0.5304   0.6038
   1.000   0.4544   0.01853   0.01095  -0.0562   0.5279   0.6268
   1.250   0.4827   0.01848   0.01094  -0.0561   0.5255   0.6522
   1.500   0.4998   0.01865   0.01135  -0.0543   0.5215   0.6814
   1.750   0.5193   0.01869   0.01164  -0.0527   0.5174   0.7210
   2.000   0.5443   0.01860   0.01180  -0.0518   0.5141   0.7821
   2.250   0.5914   0.01853   0.01191  -0.0549   0.5111   0.8658
   2.500   0.6605   0.01858   0.01187  -0.0624   0.5081   0.9178
   2.750   0.7115   0.01899   0.01227  -0.0670   0.5043   0.9480
   3.000   0.7601   0.01944   0.01275  -0.0713   0.4995   0.9674
   3.250   0.8139   0.01959   0.01284  -0.0765   0.4955   0.9820
   3.500   0.8707   0.01953   0.01266  -0.0821   0.4922   0.9929
   3.750   0.9258   0.01946   0.01243  -0.0875   0.4894   1.0000
   4.000   0.9368   0.01985   0.01285  -0.0850   0.4861   1.0000
   4.250   0.9449   0.02025   0.01332  -0.0820   0.4819   1.0000
   4.500   0.9604   0.02043   0.01348  -0.0800   0.4783   1.0000
   4.750   0.9811   0.02048   0.01347  -0.0788   0.4753   1.0000
   5.000   1.0065   0.02048   0.01337  -0.0783   0.4728   1.0000
   5.250   1.0320   0.02067   0.01344  -0.0779   0.4702   1.0000
   5.500   1.0339   0.02128   0.01420  -0.0738   0.4658   1.0000
   5.750   1.0466   0.02161   0.01457  -0.0714   0.4618   1.0000
   6.000   1.0671   0.02171   0.01462  -0.0702   0.4585   1.0000
   6.250   1.0940   0.02170   0.01453  -0.0699   0.4558   1.0000
   6.500   1.1256   0.02175   0.01445  -0.0705   0.4532   1.0000
   6.750   1.1255   0.02245   0.01531  -0.0662   0.4489   1.0000
   7.000   1.1342   0.02289   0.01580  -0.0632   0.4447   1.0000
   7.250   1.1539   0.02304   0.01594  -0.0619   0.4413   1.0000
   7.500   1.1823   0.02303   0.01585  -0.0620   0.4385   1.0000
   7.750   1.2175   0.02304   0.01572  -0.0631   0.4359   1.0000
   8.000   1.2102   0.02390   0.01676  -0.0579   0.4315   1.0000
   8.250   1.2138   0.02445   0.01738  -0.0542   0.4272   1.0000
   8.500   1.2333   0.02460   0.01752  -0.0530   0.4238   1.0000
   8.750   1.2651   0.02454   0.01737  -0.0535   0.4210   1.0000
   9.000   1.3002   0.02462   0.01736  -0.0548   0.4181   1.0000
   9.250   1.2726   0.02579   0.01873  -0.0466   0.4135   1.0000
   9.500   1.2668   0.02648   0.01948  -0.0418   0.4094   1.0000
   9.750   1.2897   0.02656   0.01954  -0.0411   0.4061   1.0000
  10.000   1.3302   0.02638   0.01926  -0.0430   0.4034   1.0000
  10.250   1.3401   0.02699   0.01990  -0.0407   0.3999   1.0000
  10.500   1.3004   0.02904   0.02215  -0.0329   0.3950   1.0000
  10.750   1.3072   0.02979   0.02292  -0.0309   0.3909   1.0000
  11.000   1.3432   0.02943   0.02249  -0.0316   0.3880   1.0000
  11.250   1.3945   0.02880   0.02174  -0.0342   0.3853   1.0000
  11.500   1.3222   0.03310   0.02635  -0.0257   0.3792   1.0000
  11.750   1.3147   0.03504   0.02836  -0.0236   0.3744   1.0000
  12.000   1.3544   0.03420   0.02745  -0.0242   0.3718   1.0000
  12.250   1.4062   0.03292   0.02607  -0.0257   0.3695   1.0000
  12.500   1.2719   0.04381   0.03735  -0.0186   0.3587   1.0000
  12.750   1.3098   0.04272   0.03623  -0.0187   0.3566   1.0000
  13.000   1.3603   0.04078   0.03422  -0.0192   0.3550   1.0000
  13.250   1.4174   0.03862   0.03197  -0.0203   0.3532   1.0000
  13.500   1.2552   0.05400   0.04772  -0.0155   0.3394   1.0000
  13.750   1.3083   0.05128   0.04496  -0.0156   0.3388   1.0000
  14.000   1.3652   0.04842   0.04204  -0.0159   0.3379   1.0000
  14.250   1.4267   0.04549   0.03903  -0.0166   0.3367   1.0000
  14.500   1.2571   0.06345   0.05732  -0.0138   0.3217   1.0000
  14.750   1.3120   0.06016   0.05401  -0.0137   0.3215   1.0000
  15.000   1.3694   0.05689   0.05069  -0.0137   0.3210   1.0000
  15.250   1.4322   0.05341   0.04715  -0.0139   0.3201   1.0000
  15.500   1.2576   0.07383   0.06786  -0.0131   0.3043   1.0000
  15.750   1.3120   0.07023   0.06425  -0.0127   0.3043   1.0000
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