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DEFIANT CANARD BL110 AIRFOIL (defcnd2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: DEFIANT CANARD BL110 AIRFOIL (defcnd2-il)
Reynolds number: 1,000,000
Max Cl/Cd: 117.18 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-defcnd2-il-1000000.txt
Download as CSV file: xf-defcnd2-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.2972   0.11266   0.11108  -0.0452   0.9756   0.0133
 -11.500  -0.2785   0.10695   0.10533  -0.0523   0.9604   0.0143
 -11.250  -0.3460   0.03515   0.03303  -0.1030   0.8971   0.0121
 -11.000  -0.3776   0.02971   0.02731  -0.1060   0.8707   0.0121
 -10.750  -0.4108   0.02593   0.02328  -0.1057   0.8516   0.0121
 -10.500  -0.4355   0.02351   0.02065  -0.1033   0.8382   0.0122
 -10.250  -0.4415   0.02260   0.01958  -0.1005   0.8279   0.0120
 -10.000  -0.4608   0.02083   0.01762  -0.0956   0.8186   0.0120
  -9.750  -0.4755   0.01856   0.01512  -0.0911   0.8115   0.0121
  -9.500  -0.4728   0.01708   0.01345  -0.0884   0.8055   0.0120
  -9.250  -0.4743   0.01483   0.01092  -0.0853   0.8002   0.0120
  -9.000  -0.4707   0.01273   0.00857  -0.0827   0.7952   0.0120
  -8.750  -0.4684   0.02234   0.01769  -0.0843   0.7972   0.0120
  -8.500  -0.4584   0.01996   0.01502  -0.0820   0.7922   0.0122
  -8.250  -0.4414   0.01864   0.01356  -0.0806   0.7874   0.0125
  -8.000  -0.4217   0.01758   0.01236  -0.0794   0.7830   0.0126
  -7.750  -0.3995   0.01708   0.01181  -0.0786   0.7782   0.0130
  -7.500  -0.3773   0.01648   0.01112  -0.0777   0.7734   0.0133
  -7.250  -0.3539   0.01606   0.01064  -0.0771   0.7687   0.0138
  -7.000  -0.3314   0.01528   0.00975  -0.0762   0.7625   0.0141
  -6.750  -0.3082   0.01469   0.00904  -0.0753   0.7568   0.0145
  -6.500  -0.2846   0.01408   0.00836  -0.0745   0.7498   0.0148
  -6.250  -0.2607   0.01359   0.00777  -0.0738   0.7426   0.0151
  -6.000  -0.2361   0.01319   0.00730  -0.0732   0.7356   0.0153
  -5.750  -0.2116   0.01284   0.00687  -0.0725   0.7269   0.0156
  -5.500  -0.1922   0.01170   0.00565  -0.0710   0.7194   0.0162
  -5.250  -0.1697   0.01121   0.00510  -0.0700   0.7104   0.0166
  -5.000  -0.1457   0.01087   0.00472  -0.0693   0.6989   0.0173
  -4.750  -0.1218   0.01059   0.00437  -0.0685   0.6844   0.0180
  -4.500  -0.0977   0.01039   0.00408  -0.0677   0.6677   0.0189
  -4.250  -0.0737   0.01021   0.00381  -0.0669   0.6491   0.0195
  -4.000  -0.0497   0.01008   0.00357  -0.0661   0.6275   0.0199
  -3.500  -0.0045   0.00960   0.00286  -0.0639   0.5861   0.0224
  -3.250   0.0198   0.00951   0.00267  -0.0632   0.5683   0.0237
  -3.000   0.0446   0.00944   0.00252  -0.0626   0.5542   0.0250
  -2.750   0.0692   0.00932   0.00235  -0.0619   0.5428   0.0286
  -2.500   0.0937   0.00919   0.00222  -0.0612   0.5327   0.0391
  -2.250   0.1168   0.00889   0.00208  -0.0604   0.5243   0.0881
  -2.000   0.1402   0.00868   0.00200  -0.0596   0.5159   0.1364
  -1.750   0.1635   0.00839   0.00192  -0.0589   0.5079   0.2059
  -1.500   0.1845   0.00801   0.00184  -0.0577   0.4990   0.3093
  -1.250   0.2056   0.00760   0.00176  -0.0566   0.4900   0.4244
  -1.000   0.2241   0.00713   0.00170  -0.0548   0.4812   0.5642
  -0.750   0.2443   0.00691   0.00174  -0.0533   0.4701   0.6642
  -0.500   0.2685   0.00689   0.00175  -0.0525   0.4573   0.7027
  -0.250   0.2925   0.00691   0.00177  -0.0517   0.4423   0.7291
   0.000   0.3163   0.00696   0.00180  -0.0508   0.4253   0.7528
   0.250   0.3395   0.00702   0.00184  -0.0498   0.4097   0.7808
   0.500   0.3630   0.00706   0.00189  -0.0489   0.3976   0.8031
   0.750   0.3875   0.00711   0.00194  -0.0482   0.3903   0.8218
   1.000   0.4119   0.00716   0.00200  -0.0475   0.3845   0.8427
   1.250   0.4359   0.00719   0.00208  -0.0466   0.3799   0.8686
   1.500   0.4613   0.00721   0.00216  -0.0460   0.3767   0.8991
   1.750   0.4897   0.00728   0.00226  -0.0461   0.3732   0.9250
   2.000   0.5226   0.00740   0.00238  -0.0472   0.3704   0.9418
   2.250   0.5560   0.00755   0.00249  -0.0485   0.3673   0.9541
   2.500   0.5945   0.00769   0.00261  -0.0510   0.3651   0.9601
   2.750   0.6273   0.00780   0.00271  -0.0521   0.3634   0.9686
   3.000   0.6663   0.00793   0.00282  -0.0547   0.3612   0.9712
   3.250   0.7027   0.00807   0.00294  -0.0568   0.3590   0.9746
   3.500   0.7361   0.00823   0.00307  -0.0582   0.3566   0.9793
   3.750   0.7697   0.00840   0.00320  -0.0596   0.3541   0.9831
   4.000   0.8059   0.00858   0.00336  -0.0617   0.3515   0.9854
   4.250   0.8417   0.00870   0.00348  -0.0636   0.3499   0.9880
   4.500   0.8768   0.00881   0.00360  -0.0654   0.3486   0.9910
   4.750   0.9109   0.00893   0.00372  -0.0670   0.3468   0.9938
   5.000   0.9474   0.00903   0.00383  -0.0692   0.3449   0.9957
   5.250   0.9832   0.00916   0.00396  -0.0712   0.3428   0.9978
   5.500   1.0188   0.00931   0.00410  -0.0732   0.3404   0.9995
   5.750   1.0419   0.00946   0.00425  -0.0725   0.3380   1.0000
   6.000   1.0584   0.00965   0.00443  -0.0705   0.3354   1.0000
   6.250   1.0785   0.00971   0.00452  -0.0691   0.3342   1.0000
   6.500   1.0986   0.00978   0.00463  -0.0677   0.3324   1.0000
   6.750   1.1186   0.00987   0.00475  -0.0663   0.3303   1.0000
   7.000   1.1384   0.00998   0.00489  -0.0648   0.3279   1.0000
   7.250   1.1572   0.01013   0.00504  -0.0632   0.3246   1.0000
   7.500   1.1759   0.01027   0.00518  -0.0616   0.3186   1.0000
   7.750   1.1980   0.01031   0.00523  -0.0607   0.3115   1.0000
   8.000   1.2178   0.01043   0.00534  -0.0593   0.3028   1.0000
   8.250   1.2374   0.01056   0.00546  -0.0579   0.2917   1.0000
   8.750   1.2678   0.01103   0.00583  -0.0534   0.2690   1.0000
   9.000   1.2802   0.01131   0.00610  -0.0507   0.2613   1.0000
   9.250   1.2927   0.01165   0.00641  -0.0481   0.2546   1.0000
   9.500   1.3068   0.01197   0.00673  -0.0458   0.2480   1.0000
   9.750   1.3181   0.01244   0.00716  -0.0432   0.2389   1.0000
  10.000   1.3334   0.01281   0.00753  -0.0414   0.2303   1.0000
  10.250   1.3461   0.01331   0.00801  -0.0392   0.2222   1.0000
  10.500   1.3640   0.01363   0.00835  -0.0379   0.2140   1.0000
  10.750   1.3749   0.01428   0.00891  -0.0357   0.1906   1.0000
  11.000   1.3649   0.01603   0.01033  -0.0309   0.1424   1.0000
  11.250   1.3586   0.01775   0.01186  -0.0271   0.1095   1.0000
  11.500   1.3612   0.01911   0.01313  -0.0246   0.0917   1.0000
  11.750   1.3573   0.02096   0.01484  -0.0218   0.0677   1.0000
  12.000   1.3634   0.02227   0.01612  -0.0201   0.0579   1.0000
  12.250   1.3469   0.02526   0.01893  -0.0169   0.0289   1.0000
  12.500   1.3582   0.02634   0.02006  -0.0160   0.0282   1.0000
  12.750   1.3396   0.02981   0.02345  -0.0134   0.0099   1.0000
  13.000   1.3382   0.03208   0.02575  -0.0121   0.0068   1.0000
  13.250   1.3422   0.03398   0.02771  -0.0112   0.0061   1.0000
  13.500   1.3451   0.03607   0.02987  -0.0105   0.0057   1.0000
  13.750   1.3475   0.03829   0.03216  -0.0099   0.0055   1.0000
  14.000   1.3494   0.04064   0.03458  -0.0095   0.0053   1.0000
  14.250   1.3501   0.04322   0.03724  -0.0092   0.0052   1.0000
  14.500   1.3471   0.04630   0.04042  -0.0090   0.0050   1.0000
  14.750   1.3451   0.04935   0.04355  -0.0090   0.0048   1.0000
  15.000   1.3447   0.05230   0.04658  -0.0091   0.0048   1.0000
  15.250   1.3392   0.05590   0.05028  -0.0093   0.0047   1.0000
  15.500   1.3333   0.05957   0.05405  -0.0096   0.0046   1.0000
  15.750   1.3298   0.06301   0.05757  -0.0100   0.0046   1.0000
  16.000   1.3252   0.06664   0.06129  -0.0104   0.0044   1.0000
  16.250   1.3189   0.07051   0.06524  -0.0109   0.0045   1.0000
  16.500   1.3120   0.07451   0.06934  -0.0116   0.0043   1.0000
  16.750   1.3055   0.07855   0.07346  -0.0123   0.0045   1.0000
  17.000   1.2991   0.08262   0.07762  -0.0131   0.0043   1.0000
  17.250   1.2925   0.08674   0.08183  -0.0139   0.0042   1.0000
  17.500   1.2854   0.09100   0.08617  -0.0149   0.0042   1.0000
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