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DEFIANT CANARD BL110 AIRFOIL (defcnd2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: DEFIANT CANARD BL110 AIRFOIL (defcnd2-il)
Reynolds number: 1,000,000
Max Cl/Cd: 114.96 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-defcnd2-il-1000000-n5.txt
Download as CSV file: xf-defcnd2-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: DEFIANT CANARD BL110 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
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.3732   0.16367   0.16193  -0.0242   1.0000   0.0053
 -15.250  -0.3679   0.16005   0.15831  -0.0256   1.0000   0.0054
 -13.750  -0.8019   0.03954   0.03694  -0.0880   0.9758   0.0071
 -13.500  -0.7762   0.03422   0.03134  -0.0992   0.9537   0.0071
 -13.250  -0.7336   0.03135   0.02824  -0.1084   0.9322   0.0073
 -13.000  -0.7076   0.02982   0.02644  -0.1119   0.8880   0.0073
 -12.750  -0.7273   0.02744   0.02371  -0.1079   0.8539   0.0073
 -12.500  -0.7251   0.02654   0.02266  -0.1051   0.8363   0.0074
 -12.250  -0.7252   0.02546   0.02141  -0.1018   0.8243   0.0075
 -12.000  -0.7244   0.02444   0.02024  -0.0982   0.8143   0.0075
 -11.750  -0.7199   0.02364   0.01931  -0.0949   0.8060   0.0076
 -11.500  -0.7115   0.02281   0.01835  -0.0923   0.7994   0.0077
 -11.250  -0.7008   0.02188   0.01727  -0.0900   0.7927   0.0077
 -11.000  -0.6868   0.02113   0.01640  -0.0882   0.7871   0.0079
 -10.750  -0.6714   0.02037   0.01551  -0.0865   0.7818   0.0080
 -10.500  -0.6550   0.01964   0.01466  -0.0849   0.7763   0.0081
 -10.250  -0.6382   0.01889   0.01378  -0.0834   0.7716   0.0083
 -10.000  -0.6197   0.01821   0.01299  -0.0821   0.7671   0.0084
  -9.750  -0.5997   0.01765   0.01233  -0.0809   0.7616   0.0086
  -9.500  -0.5798   0.01710   0.01166  -0.0797   0.7552   0.0087
  -9.250  -0.5585   0.01658   0.01104  -0.0788   0.7492   0.0088
  -9.000  -0.5364   0.01616   0.01054  -0.0779   0.7434   0.0089
  -8.750  -0.5171   0.01540   0.00967  -0.0766   0.7386   0.0092
  -8.500  -0.4958   0.01481   0.00901  -0.0756   0.7333   0.0094
  -8.250  -0.4729   0.01442   0.00857  -0.0748   0.7273   0.0096
  -8.000  -0.4498   0.01401   0.00810  -0.0741   0.7213   0.0097
  -7.750  -0.4261   0.01367   0.00770  -0.0734   0.7138   0.0099
  -7.500  -0.4025   0.01332   0.00728  -0.0726   0.7060   0.0101
  -7.250  -0.3789   0.01300   0.00689  -0.0719   0.6962   0.0104
  -7.000  -0.3554   0.01268   0.00649  -0.0711   0.6821   0.0106
  -6.750  -0.3321   0.01241   0.00612  -0.0703   0.6650   0.0109
  -6.500  -0.3099   0.01221   0.00575  -0.0692   0.6343   0.0111
  -6.250  -0.2875   0.01204   0.00543  -0.0682   0.6028   0.0114
  -6.000  -0.2648   0.01191   0.00515  -0.0672   0.5725   0.0116
  -5.750  -0.2414   0.01181   0.00491  -0.0664   0.5480   0.0118
  -5.500  -0.2180   0.01151   0.00453  -0.0656   0.5368   0.0123
  -5.250  -0.1940   0.01126   0.00422  -0.0649   0.5282   0.0127
  -5.000  -0.1688   0.01110   0.00402  -0.0644   0.5203   0.0133
  -4.750  -0.1438   0.01094   0.00381  -0.0639   0.5120   0.0138
  -4.500  -0.1186   0.01079   0.00361  -0.0633   0.5035   0.0143
  -4.250  -0.0932   0.01064   0.00341  -0.0629   0.4962   0.0148
  -4.000  -0.0676   0.01051   0.00322  -0.0624   0.4885   0.0152
  -3.750  -0.0420   0.01039   0.00306  -0.0620   0.4804   0.0156
  -3.500  -0.0170   0.01022   0.00283  -0.0614   0.4713   0.0166
  -3.250   0.0085   0.01011   0.00268  -0.0609   0.4617   0.0176
  -3.000   0.0340   0.01003   0.00255  -0.0605   0.4499   0.0187
  -2.750   0.0593   0.01000   0.00244  -0.0600   0.4337   0.0197
  -2.500   0.0836   0.01000   0.00233  -0.0593   0.4101   0.0218
  -2.250   0.1078   0.01000   0.00226  -0.0586   0.3890   0.0262
  -2.000   0.1318   0.00991   0.00219  -0.0580   0.3775   0.0459
  -1.750   0.1564   0.00981   0.00212  -0.0574   0.3698   0.0683
  -1.250   0.2059   0.00956   0.00203  -0.0563   0.3605   0.1315
  -1.000   0.2308   0.00943   0.00199  -0.0558   0.3577   0.1699
  -0.750   0.2546   0.00922   0.00196  -0.0551   0.3550   0.2325
  -0.250   0.2995   0.00864   0.00190  -0.0533   0.3507   0.4153
   0.000   0.3195   0.00820   0.00187  -0.0519   0.3494   0.5487
   0.250   0.3396   0.00790   0.00192  -0.0504   0.3482   0.6656
   0.500   0.3644   0.00786   0.00195  -0.0498   0.3468   0.6987
   0.750   0.3902   0.00787   0.00199  -0.0494   0.3454   0.7181
   1.000   0.4154   0.00786   0.00203  -0.0488   0.3441   0.7381
   1.250   0.4400   0.00785   0.00208  -0.0481   0.3427   0.7647
   1.500   0.4636   0.00782   0.00214  -0.0472   0.3413   0.7966
   1.750   0.4873   0.00781   0.00221  -0.0464   0.3393   0.8247
   2.000   0.5119   0.00784   0.00228  -0.0457   0.3377   0.8458
   2.250   0.5370   0.00788   0.00235  -0.0451   0.3361   0.8635
   2.500   0.5628   0.00791   0.00243  -0.0447   0.3350   0.8806
   2.750   0.5898   0.00794   0.00250  -0.0446   0.3343   0.8983
   3.000   0.6187   0.00798   0.00259  -0.0449   0.3333   0.9154
   3.250   0.6506   0.00806   0.00269  -0.0459   0.3322   0.9307
   3.500   0.6854   0.00816   0.00280  -0.0475   0.3306   0.9429
   3.750   0.7205   0.00827   0.00291  -0.0493   0.3284   0.9531
   4.000   0.7581   0.00841   0.00304  -0.0517   0.3262   0.9589
   4.250   0.7933   0.00854   0.00316  -0.0535   0.3241   0.9655
   4.500   0.8282   0.00869   0.00329  -0.0553   0.3222   0.9701
   4.750   0.8628   0.00884   0.00344  -0.0570   0.3203   0.9738
   5.000   0.8946   0.00894   0.00355  -0.0581   0.3191   0.9787
   5.250   0.9252   0.00904   0.00367  -0.0589   0.3176   0.9831
   5.500   0.9583   0.00915   0.00379  -0.0603   0.3156   0.9862
   5.750   0.9900   0.00927   0.00392  -0.0614   0.3131   0.9898
   6.000   1.0203   0.00940   0.00406  -0.0622   0.3103   0.9931
   6.250   1.0515   0.00955   0.00421  -0.0632   0.3073   0.9961
   6.500   1.0837   0.00968   0.00436  -0.0645   0.3045   0.9983
   6.750   1.1162   0.00980   0.00450  -0.0658   0.3006   0.9997
   7.000   1.1389   0.00992   0.00463  -0.0650   0.2952   1.0000
   7.250   1.1576   0.01007   0.00476  -0.0634   0.2857   1.0000
   7.500   1.1703   0.01045   0.00498  -0.0607   0.2626   1.0000
   7.750   1.1831   0.01082   0.00527  -0.0581   0.2502   1.0000
   8.000   1.1959   0.01119   0.00559  -0.0555   0.2400   1.0000
   8.250   1.2099   0.01143   0.00583  -0.0530   0.2348   1.0000
   8.500   1.2244   0.01163   0.00605  -0.0506   0.2312   1.0000
   8.750   1.2380   0.01191   0.00632  -0.0481   0.2266   1.0000
   9.000   1.2527   0.01220   0.00661  -0.0459   0.2223   1.0000
   9.250   1.2710   0.01240   0.00686  -0.0444   0.2193   1.0000
   9.500   1.2867   0.01272   0.00718  -0.0426   0.2116   1.0000
   9.750   1.2987   0.01323   0.00760  -0.0403   0.1911   1.0000
  10.000   1.2826   0.01506   0.00902  -0.0340   0.1295   1.0000
  10.250   1.2823   0.01631   0.01012  -0.0304   0.1012   1.0000
  10.500   1.2864   0.01745   0.01116  -0.0277   0.0816   1.0000
  10.750   1.2897   0.01872   0.01233  -0.0252   0.0622   1.0000
  11.000   1.2973   0.01981   0.01338  -0.0233   0.0513   1.0000
  11.250   1.2981   0.02140   0.01489  -0.0210   0.0346   1.0000
  11.500   1.3002   0.02300   0.01644  -0.0190   0.0232   1.0000
  11.750   1.3012   0.02477   0.01819  -0.0171   0.0134   1.0000
  12.000   1.3077   0.02621   0.01965  -0.0158   0.0093   1.0000
  12.250   1.3064   0.02831   0.02177  -0.0142   0.0042   1.0000
  12.500   1.3167   0.02956   0.02307  -0.0134   0.0044   1.0000
  12.750   1.3211   0.03132   0.02489  -0.0124   0.0037   1.0000
  13.000   1.3257   0.03315   0.02678  -0.0116   0.0034   1.0000
  13.250   1.3312   0.03496   0.02865  -0.0109   0.0032   1.0000
  13.500   1.3355   0.03695   0.03070  -0.0103   0.0031   1.0000
  13.750   1.3394   0.03905   0.03288  -0.0098   0.0030   1.0000
  14.000   1.3423   0.04134   0.03523  -0.0095   0.0030   1.0000
  14.250   1.3448   0.04374   0.03771  -0.0092   0.0030   1.0000
  14.500   1.3450   0.04647   0.04052  -0.0091   0.0029   1.0000
  14.750   1.3463   0.04914   0.04327  -0.0091   0.0029   1.0000
  15.000   1.3457   0.05211   0.04631  -0.0092   0.0029   1.0000
  15.250   1.3437   0.05529   0.04957  -0.0094   0.0028   1.0000
  15.500   1.3392   0.05877   0.05315  -0.0097   0.0027   1.0000
  15.750   1.3375   0.06196   0.05641  -0.0100   0.0027   1.0000
  16.000   1.3330   0.06555   0.06008  -0.0104   0.0026   1.0000
  16.250   1.3286   0.06916   0.06377  -0.0109   0.0027   1.0000
  16.500   1.3224   0.07303   0.06772  -0.0115   0.0025   1.0000
  16.750   1.3180   0.07675   0.07153  -0.0121   0.0026   1.0000
  17.000   1.3125   0.08066   0.07552  -0.0128   0.0025   1.0000
  17.250   1.3065   0.08464   0.07957  -0.0136   0.0024   1.0000
  17.500   1.3004   0.08870   0.08371  -0.0145   0.0024   1.0000
  17.750   1.2929   0.09302   0.08813  -0.0155   0.0023   1.0000
  18.000   1.2898   0.09673   0.09191  -0.0164   0.0023   1.0000
  18.250   1.2829   0.10097   0.09623  -0.0175   0.0023   1.0000
  18.500   1.2758   0.10531   0.10064  -0.0186   0.0023   1.0000
  18.750   1.2700   0.10946   0.10487  -0.0198   0.0023   1.0000
  19.000   1.2655   0.11346   0.10894  -0.0210   0.0022   1.0000
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