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DEFIANT CANARD BL110 AIRFOIL (defcnd2-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: DEFIANT CANARD BL110 AIRFOIL (defcnd2-il)
Reynolds number: 500,000
Max Cl/Cd: 89.6 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-defcnd2-il-500000.txt
Download as CSV file: xf-defcnd2-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.2057   0.12265   0.12061  -0.0454   1.0000   0.0209
 -12.500  -0.3128   0.12423   0.12195  -0.0431   1.0000   0.0203
 -12.250  -0.3062   0.12171   0.11945  -0.0433   1.0000   0.0206
 -12.000  -0.3012   0.11885   0.11661  -0.0439   1.0000   0.0208
 -11.750  -0.2959   0.11617   0.11395  -0.0443   1.0000   0.0211
 -11.500  -0.2923   0.11321   0.11101  -0.0450   1.0000   0.0216
 -11.250  -0.2903   0.10998   0.10780  -0.0459   1.0000   0.0219
 -11.000  -0.1809   0.08762   0.08555  -0.0689   0.9556   0.0257
 -10.750  -0.1612   0.08428   0.08218  -0.0721   0.9453   0.0263
 -10.500  -0.1445   0.08030   0.07816  -0.0760   0.9340   0.0270
 -10.250  -0.1348   0.07545   0.07326  -0.0800   0.9209   0.0277
 -10.000  -0.2773   0.07984   0.07775  -0.0710   0.9593   0.0259
  -9.750  -0.2516   0.07636   0.07423  -0.0769   0.9500   0.0266
  -9.500  -0.2298   0.07026   0.06809  -0.0866   0.9375   0.0272
  -9.250  -0.2244   0.05947   0.05716  -0.1032   0.9129   0.0278
  -9.000  -0.2465   0.05326   0.05072  -0.1075   0.8853   0.0278
  -8.750  -0.2693   0.04997   0.04724  -0.1049   0.8681   0.0279
  -8.500  -0.2823   0.04718   0.04427  -0.1022   0.8566   0.0286
  -8.250  -0.2867   0.03365   0.03037  -0.0921   0.8327   0.0315
  -8.000  -0.2926   0.03089   0.02738  -0.0893   0.8256   0.0316
  -7.000  -0.3039   0.02347   0.01820  -0.0824   0.8131   0.0230
  -6.750  -0.2917   0.01964   0.01371  -0.0794   0.8072   0.0213
  -6.250  -0.2467   0.01733   0.01106  -0.0774   0.7952   0.0216
  -6.000  -0.2231   0.01645   0.01006  -0.0766   0.7893   0.0220
  -5.750  -0.1991   0.01568   0.00919  -0.0759   0.7832   0.0225
  -5.500  -0.1753   0.01497   0.00839  -0.0751   0.7766   0.0231
  -5.250  -0.1511   0.01439   0.00770  -0.0743   0.7707   0.0238
  -5.000  -0.1269   0.01394   0.00719  -0.0735   0.7628   0.0248
  -4.750  -0.1032   0.01345   0.00659  -0.0726   0.7548   0.0253
  -4.500  -0.0832   0.01254   0.00564  -0.0711   0.7455   0.0263
  -4.250  -0.0605   0.01208   0.00514  -0.0700   0.7365   0.0274
  -4.000  -0.0371   0.01172   0.00473  -0.0691   0.7267   0.0288
  -3.750  -0.0133   0.01139   0.00436  -0.0682   0.7161   0.0303
  -3.500   0.0105   0.01109   0.00398  -0.0673   0.7054   0.0325
  -3.250   0.0340   0.01077   0.00363  -0.0664   0.6933   0.0361
  -3.000   0.0580   0.01053   0.00332  -0.0655   0.6796   0.0416
  -2.750   0.0797   0.01011   0.00302  -0.0643   0.6646   0.0768
  -2.500   0.1003   0.00967   0.00282  -0.0630   0.6484   0.1519
  -2.250   0.1206   0.00927   0.00265  -0.0617   0.6317   0.2393
  -2.000   0.1392   0.00878   0.00251  -0.0601   0.6155   0.3584
  -1.750   0.1530   0.00809   0.00238  -0.0576   0.6008   0.5350
  -1.500   0.1693   0.00779   0.00242  -0.0551   0.5865   0.6632
  -1.250   0.1910   0.00777   0.00243  -0.0537   0.5730   0.7128
  -1.000   0.2129   0.00777   0.00246  -0.0523   0.5602   0.7530
  -0.750   0.2364   0.00780   0.00247  -0.0512   0.5485   0.7796
  -0.500   0.2599   0.00782   0.00251  -0.0501   0.5384   0.8078
  -0.250   0.2834   0.00787   0.00256  -0.0490   0.5292   0.8341
   0.000   0.3080   0.00792   0.00260  -0.0482   0.5195   0.8563
   0.250   0.3333   0.00799   0.00265  -0.0475   0.5104   0.8763
   0.500   0.3598   0.00809   0.00273  -0.0471   0.5003   0.8962
   0.750   0.3886   0.00819   0.00283  -0.0471   0.4896   0.9199
   1.000   0.4206   0.00836   0.00295  -0.0478   0.4783   0.9388
   1.250   0.4579   0.00856   0.00306  -0.0498   0.4663   0.9479
   1.500   0.4927   0.00874   0.00315  -0.0514   0.4543   0.9559
   1.750   0.5317   0.00892   0.00325  -0.0539   0.4419   0.9604
   2.000   0.5663   0.00910   0.00335  -0.0555   0.4324   0.9672
   2.250   0.6047   0.00930   0.00345  -0.0580   0.4241   0.9706
   2.500   0.6439   0.00945   0.00355  -0.0606   0.4168   0.9740
   2.750   0.6795   0.00965   0.00367  -0.0625   0.4105   0.9793
   3.000   0.7164   0.00980   0.00378  -0.0647   0.4054   0.9835
   3.250   0.7554   0.00995   0.00388  -0.0674   0.4007   0.9867
   3.500   0.7923   0.01013   0.00400  -0.0696   0.3965   0.9909
   3.750   0.8296   0.01028   0.00413  -0.0720   0.3931   0.9946
   4.000   0.8687   0.01040   0.00424  -0.0747   0.3896   0.9978
   4.250   0.9025   0.01053   0.00436  -0.0764   0.3862   1.0000
   4.500   0.9185   0.01066   0.00446  -0.0743   0.3836   1.0000
   4.750   0.9349   0.01084   0.00459  -0.0723   0.3807   1.0000
   5.000   0.9534   0.01094   0.00472  -0.0707   0.3784   1.0000
   5.250   0.9721   0.01106   0.00487  -0.0691   0.3758   1.0000
   5.500   0.9907   0.01121   0.00502  -0.0674   0.3729   1.0000
   5.750   1.0093   0.01140   0.00520  -0.0658   0.3700   1.0000
   6.000   1.0281   0.01164   0.00540  -0.0643   0.3671   1.0000
   6.250   1.0479   0.01183   0.00562  -0.0629   0.3646   1.0000
   6.500   1.0679   0.01198   0.00581  -0.0615   0.3619   1.0000
   6.750   1.0877   0.01215   0.00601  -0.0601   0.3589   1.0000
   7.000   1.1074   0.01236   0.00623  -0.0588   0.3559   1.0000
   7.250   1.1273   0.01264   0.00650  -0.0575   0.3527   1.0000
   7.500   1.1479   0.01290   0.00677  -0.0563   0.3495   1.0000
   7.750   1.1672   0.01306   0.00701  -0.0549   0.3464   1.0000
   8.000   1.1864   0.01326   0.00725  -0.0534   0.3428   1.0000
   8.250   1.2044   0.01352   0.00751  -0.0518   0.3381   1.0000
   8.500   1.2215   0.01377   0.00779  -0.0501   0.3330   1.0000
   8.750   1.2328   0.01385   0.00794  -0.0470   0.3266   1.0000
   9.000   1.2461   0.01412   0.00818  -0.0446   0.3213   1.0000
   9.250   1.2604   0.01423   0.00839  -0.0422   0.3153   1.0000
   9.500   1.2766   0.01442   0.00863  -0.0404   0.3100   1.0000
   9.750   1.2921   0.01465   0.00890  -0.0385   0.3039   1.0000
  10.000   1.3093   0.01483   0.00915  -0.0370   0.2956   1.0000
  10.250   1.3257   0.01510   0.00945  -0.0354   0.2877   1.0000
  10.500   1.3396   0.01547   0.00983  -0.0335   0.2769   1.0000
  10.750   1.3502   0.01604   0.01035  -0.0313   0.2657   1.0000
  11.000   1.3593   0.01678   0.01104  -0.0291   0.2539   1.0000
  11.250   1.3706   0.01748   0.01176  -0.0272   0.2445   1.0000
  11.500   1.3797   0.01834   0.01260  -0.0252   0.2373   1.0000
  11.750   1.3919   0.01909   0.01339  -0.0237   0.2271   1.0000
  12.000   1.4026   0.01995   0.01428  -0.0221   0.2147   1.0000
  12.250   1.3968   0.02188   0.01594  -0.0192   0.1651   1.0000
  12.500   1.3908   0.02397   0.01790  -0.0166   0.1420   1.0000
  12.750   1.3789   0.02662   0.02043  -0.0138   0.1169   1.0000
  13.000   1.3695   0.02927   0.02299  -0.0116   0.0959   1.0000
  13.250   1.3623   0.03188   0.02554  -0.0099   0.0809   1.0000
  13.500   1.3527   0.03487   0.02848  -0.0085   0.0651   1.0000
  13.750   1.3439   0.03799   0.03157  -0.0074   0.0523   1.0000
  14.000   1.3312   0.04171   0.03526  -0.0066   0.0394   1.0000
  14.250   1.3189   0.04563   0.03917  -0.0062   0.0295   1.0000
  14.500   1.2980   0.05074   0.04427  -0.0061   0.0184   1.0000
  14.750   1.2910   0.05445   0.04804  -0.0062   0.0155   1.0000
  15.000   1.2824   0.05842   0.05208  -0.0065   0.0132   1.0000
  15.250   1.2713   0.06278   0.05652  -0.0069   0.0114   1.0000
  15.500   1.2625   0.06692   0.06076  -0.0074   0.0101   1.0000
  15.750   1.2581   0.07055   0.06449  -0.0079   0.0100   1.0000
  16.000   1.2509   0.07461   0.06864  -0.0085   0.0095   1.0000
  16.250   1.2443   0.07867   0.07279  -0.0092   0.0093   1.0000
  16.500   1.2342   0.08323   0.07744  -0.0101   0.0088   1.0000
  16.750   1.2275   0.08742   0.08172  -0.0110   0.0087   1.0000
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