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DEFIANT CANARD BL110 AIRFOIL (defcnd2-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: DEFIANT CANARD BL110 AIRFOIL (defcnd2-il)
Reynolds number: 500,000
Max Cl/Cd: 89.64 at α=8.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-defcnd2-il-500000-n5.txt
Download as CSV file: xf-defcnd2-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.4786   0.04029   0.03723  -0.1079   0.9040   0.0097
 -11.000  -0.4942   0.03674   0.03332  -0.1079   0.8733   0.0098
 -10.750  -0.5079   0.03454   0.03086  -0.1048   0.8535   0.0099
 -10.500  -0.5194   0.03270   0.02877  -0.1007   0.8390   0.0099
 -10.250  -0.5307   0.03064   0.02643  -0.0962   0.8279   0.0101
 -10.000  -0.5266   0.02925   0.02482  -0.0936   0.8186   0.0102
  -9.750  -0.5195   0.02788   0.02323  -0.0912   0.8113   0.0104
  -9.500  -0.5132   0.02615   0.02121  -0.0886   0.8036   0.0107
  -9.250  -0.5024   0.02470   0.01950  -0.0865   0.7968   0.0109
  -9.000  -0.4894   0.02333   0.01786  -0.0846   0.7897   0.0112
  -8.750  -0.4742   0.02205   0.01633  -0.0829   0.7845   0.0114
  -8.500  -0.4566   0.02095   0.01502  -0.0815   0.7795   0.0116
  -8.250  -0.4371   0.02010   0.01397  -0.0803   0.7742   0.0118
  -8.000  -0.4167   0.01930   0.01299  -0.0791   0.7691   0.0119
  -7.750  -0.3978   0.01812   0.01168  -0.0779   0.7636   0.0122
  -7.500  -0.3766   0.01739   0.01086  -0.0770   0.7580   0.0125
  -7.250  -0.3543   0.01682   0.01022  -0.0761   0.7530   0.0128
  -7.000  -0.3316   0.01625   0.00958  -0.0753   0.7473   0.0131
  -6.750  -0.3087   0.01574   0.00898  -0.0745   0.7415   0.0134
  -6.500  -0.2856   0.01522   0.00838  -0.0737   0.7346   0.0138
  -6.250  -0.2625   0.01474   0.00781  -0.0729   0.7269   0.0142
  -6.000  -0.2387   0.01432   0.00732  -0.0722   0.7191   0.0147
  -5.750  -0.2148   0.01399   0.00690  -0.0714   0.7100   0.0153
  -5.500  -0.1918   0.01353   0.00636  -0.0705   0.6994   0.0157
  -5.250  -0.1698   0.01301   0.00578  -0.0695   0.6882   0.0163
  -5.000  -0.1468   0.01266   0.00535  -0.0686   0.6741   0.0169
  -4.750  -0.1242   0.01240   0.00498  -0.0675   0.6529   0.0174
  -4.500  -0.1018   0.01219   0.00462  -0.0665   0.6285   0.0181
  -4.250  -0.0793   0.01203   0.00432  -0.0654   0.6040   0.0188
  -4.000  -0.0564   0.01190   0.00405  -0.0644   0.5810   0.0196
  -3.750  -0.0335   0.01174   0.00378  -0.0635   0.5629   0.0207
  -3.500  -0.0099   0.01159   0.00354  -0.0627   0.5497   0.0224
  -3.250   0.0146   0.01146   0.00334  -0.0620   0.5399   0.0240
  -2.750   0.0638   0.01120   0.00300  -0.0607   0.5235   0.0312
  -2.500   0.0876   0.01102   0.00286  -0.0600   0.5161   0.0504
  -2.250   0.1119   0.01082   0.00274  -0.0594   0.5090   0.0777
  -2.000   0.1359   0.01065   0.00264  -0.0587   0.5015   0.1085
  -1.750   0.1598   0.01043   0.00254  -0.0580   0.4946   0.1541
  -1.250   0.2049   0.00987   0.00238  -0.0563   0.4774   0.2961
  -1.000   0.2233   0.00936   0.00229  -0.0548   0.4671   0.4345
  -0.750   0.2413   0.00894   0.00225  -0.0529   0.4556   0.5606
  -0.500   0.2601   0.00871   0.00231  -0.0510   0.4441   0.6704
  -0.250   0.2825   0.00867   0.00233  -0.0499   0.4319   0.7137
   0.000   0.3058   0.00869   0.00236  -0.0489   0.4190   0.7421
   0.250   0.3294   0.00874   0.00239  -0.0480   0.4072   0.7660
   0.500   0.3528   0.00878   0.00244  -0.0470   0.3971   0.7898
   0.750   0.3759   0.00879   0.00251  -0.0459   0.3900   0.8237
   1.000   0.3999   0.00883   0.00260  -0.0450   0.3840   0.8578
   1.250   0.4263   0.00890   0.00268  -0.0447   0.3794   0.8804
   1.500   0.4547   0.00899   0.00276  -0.0448   0.3757   0.8964
   1.750   0.4844   0.00910   0.00286  -0.0453   0.3717   0.9106
   2.000   0.5155   0.00925   0.00296  -0.0461   0.3679   0.9236
   2.250   0.5497   0.00940   0.00308  -0.0476   0.3649   0.9339
   2.500   0.5848   0.00953   0.00319  -0.0493   0.3626   0.9425
   2.750   0.6194   0.00967   0.00330  -0.0509   0.3603   0.9507
   3.000   0.6545   0.00982   0.00343  -0.0527   0.3580   0.9570
   3.250   0.6895   0.00999   0.00356  -0.0545   0.3553   0.9625
   3.500   0.7213   0.01017   0.00371  -0.0556   0.3525   0.9692
   3.750   0.7558   0.01035   0.00386  -0.0573   0.3503   0.9735
   4.000   0.7879   0.01048   0.00400  -0.0584   0.3487   0.9793
   4.250   0.8203   0.01062   0.00414  -0.0596   0.3468   0.9839
   4.500   0.8540   0.01077   0.00429  -0.0611   0.3449   0.9879
   4.750   0.8863   0.01093   0.00446  -0.0624   0.3427   0.9923
   5.000   0.9193   0.01111   0.00463  -0.0638   0.3405   0.9962
   5.250   0.9528   0.01131   0.00481  -0.0654   0.3383   0.9993
   5.500   0.9752   0.01150   0.00500  -0.0647   0.3360   1.0000
   5.750   0.9943   0.01162   0.00515  -0.0631   0.3342   1.0000
   6.000   1.0140   0.01174   0.00529  -0.0617   0.3324   1.0000
   6.250   1.0336   0.01187   0.00546  -0.0602   0.3304   1.0000
   6.500   1.0530   0.01201   0.00564  -0.0587   0.3282   1.0000
   6.750   1.0721   0.01217   0.00582  -0.0572   0.3260   1.0000
   7.000   1.0908   0.01236   0.00602  -0.0556   0.3237   1.0000
   7.250   1.1089   0.01257   0.00624  -0.0540   0.3215   1.0000
   7.500   1.1281   0.01275   0.00646  -0.0525   0.3194   1.0000
   7.750   1.1478   0.01289   0.00666  -0.0511   0.3169   1.0000
   8.000   1.1655   0.01304   0.00687  -0.0494   0.3141   1.0000
   8.250   1.1817   0.01320   0.00707  -0.0473   0.3097   1.0000
   8.500   1.1974   0.01338   0.00728  -0.0452   0.3040   1.0000
   8.750   1.2137   0.01354   0.00745  -0.0433   0.2914   1.0000
   9.000   1.2286   0.01380   0.00768  -0.0413   0.2783   1.0000
   9.250   1.2386   0.01427   0.00805  -0.0385   0.2623   1.0000
   9.500   1.2514   0.01473   0.00850  -0.0364   0.2545   1.0000
   9.750   1.2642   0.01524   0.00899  -0.0343   0.2466   1.0000
  10.000   1.2748   0.01587   0.00960  -0.0320   0.2384   1.0000
  10.250   1.2903   0.01633   0.01010  -0.0305   0.2327   1.0000
  10.500   1.3019   0.01700   0.01077  -0.0286   0.2246   1.0000
  10.750   1.3161   0.01758   0.01138  -0.0271   0.2146   1.0000
  11.000   1.3245   0.01849   0.01221  -0.0251   0.1863   1.0000
  11.250   1.3116   0.02073   0.01411  -0.0210   0.1390   1.0000
  11.500   1.3114   0.02236   0.01567  -0.0186   0.1193   1.0000
  11.750   1.3067   0.02439   0.01759  -0.0160   0.0967   1.0000
  12.000   1.3122   0.02582   0.01902  -0.0145   0.0880   1.0000
  12.250   1.3089   0.02795   0.02109  -0.0126   0.0712   1.0000
  12.500   1.3134   0.02959   0.02275  -0.0114   0.0646   1.0000
  12.750   1.3071   0.03216   0.02527  -0.0097   0.0495   1.0000
  13.000   1.3006   0.03491   0.02799  -0.0084   0.0375   1.0000
  13.250   1.2930   0.03793   0.03100  -0.0074   0.0270   1.0000
  13.500   1.2848   0.04122   0.03430  -0.0067   0.0191   1.0000
  13.750   1.2790   0.04445   0.03757  -0.0063   0.0138   1.0000
  14.000   1.2740   0.04774   0.04091  -0.0062   0.0099   1.0000
  14.250   1.2700   0.05102   0.04426  -0.0062   0.0080   1.0000
  14.500   1.2634   0.05473   0.04804  -0.0064   0.0063   1.0000
  14.750   1.2621   0.05782   0.05122  -0.0066   0.0061   1.0000
  15.000   1.2591   0.06117   0.05466  -0.0069   0.0058   1.0000
  15.250   1.2546   0.06478   0.05835  -0.0073   0.0054   1.0000
  15.500   1.2464   0.06886   0.06254  -0.0078   0.0049   1.0000
  15.750   1.2436   0.07231   0.06607  -0.0083   0.0049   1.0000
  16.000   1.2385   0.07613   0.06998  -0.0090   0.0047   1.0000
  16.250   1.2343   0.07989   0.07383  -0.0097   0.0047   1.0000
  16.500   1.2302   0.08364   0.07767  -0.0104   0.0045   1.0000
  16.750   1.2262   0.08744   0.08156  -0.0112   0.0045   1.0000
  17.000   1.2227   0.09120   0.08541  -0.0120   0.0044   1.0000
  17.250   1.2191   0.09500   0.08929  -0.0129   0.0043   1.0000
  17.500   1.2151   0.09887   0.09325  -0.0139   0.0042   1.0000
  17.750   1.2109   0.10279   0.09726  -0.0149   0.0041   1.0000
  18.000   1.2089   0.10639   0.10094  -0.0159   0.0041   1.0000
  18.250   1.2038   0.11052   0.10515  -0.0171   0.0040   1.0000
  18.500   1.2007   0.11436   0.10907  -0.0183   0.0039   1.0000
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