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DRAGONFLY CANARD (drgnfly-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: DRAGONFLY CANARD (drgnfly-il)
Reynolds number: 500,000
Max Cl/Cd: 87.85 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-drgnfly-il-500000.txt
Download as CSV file: xf-drgnfly-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: DRAGONFLY CANARD                                
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.000   0.0609   0.09207   0.08764  -0.1179   0.6118   0.0309
 -10.750   0.0620   0.08882   0.08441  -0.1193   0.6108   0.0321
 -10.500   0.0355   0.08107   0.07674  -0.1249   0.6104   0.0337
 -10.250   0.0247   0.07560   0.07131  -0.1267   0.6095   0.0340
 -10.000   0.0306   0.07347   0.06920  -0.1268   0.6084   0.0343
  -9.750   0.0380   0.07171   0.06745  -0.1269   0.6071   0.0347
  -9.500   0.0406   0.06920   0.06495  -0.1277   0.6059   0.0350
  -9.250   0.0407   0.06635   0.06212  -0.1287   0.6048   0.0354
  -9.000   0.0340   0.06247   0.05826  -0.1308   0.6037   0.0358
  -8.750  -0.0030   0.05493   0.05073  -0.1363   0.6030   0.0358
  -8.500  -0.0278   0.05156   0.04730  -0.1347   0.6020   0.0361
  -8.250  -0.0466   0.04911   0.04477  -0.1318   0.6011   0.0366
  -8.000  -0.0577   0.04629   0.04182  -0.1296   0.6000   0.0374
  -7.750  -0.1004   0.02837   0.02358  -0.1178   0.5980   0.0407
  -7.500  -0.0833   0.02657   0.02185  -0.1176   0.5970   0.0412
  -7.250  -0.0698   0.02512   0.02040  -0.1167   0.5958   0.0418
  -7.000  -0.0568   0.02367   0.01890  -0.1157   0.5946   0.0425
  -6.750  -0.0456   0.02200   0.01713  -0.1143   0.5934   0.0437
  -6.500  -0.0520   0.01924   0.01374  -0.1097   0.5923   0.0482
  -6.250  -0.0512   0.02500   0.01831  -0.1096   0.5929   0.0333
  -6.000  -0.0324   0.02322   0.01633  -0.1083   0.5917   0.0330
  -5.750  -0.0106   0.02247   0.01538  -0.1073   0.5905   0.0334
  -5.500   0.0119   0.02195   0.01465  -0.1064   0.5893   0.0337
  -5.250   0.0355   0.02065   0.01319  -0.1059   0.5880   0.0338
  -5.000   0.0603   0.01940   0.01180  -0.1055   0.5869   0.0340
  -4.750   0.0858   0.01831   0.01062  -0.1053   0.5858   0.0343
  -4.500   0.1112   0.01761   0.00987  -0.1051   0.5847   0.0349
  -4.250   0.1360   0.01720   0.00944  -0.1048   0.5834   0.0356
  -4.000   0.1605   0.01679   0.00904  -0.1043   0.5825   0.0364
  -3.750   0.1851   0.01647   0.00872  -0.1038   0.5814   0.0374
  -3.500   0.2094   0.01615   0.00840  -0.1033   0.5803   0.0384
  -3.250   0.2336   0.01585   0.00808  -0.1027   0.5791   0.0391
  -3.000   0.2578   0.01560   0.00781  -0.1022   0.5779   0.0397
  -2.750   0.2813   0.01528   0.00747  -0.1015   0.5767   0.0405
  -2.500   0.3039   0.01490   0.00709  -0.1006   0.5755   0.0421
  -2.250   0.3286   0.01468   0.00687  -0.1002   0.5742   0.0437
  -2.000   0.3541   0.01452   0.00668  -0.0999   0.5731   0.0458
  -1.750   0.3801   0.01440   0.00651  -0.0996   0.5720   0.0476
  -1.500   0.4051   0.01420   0.00630  -0.0993   0.5711   0.0515
  -1.250   0.4314   0.01413   0.00620  -0.0991   0.5701   0.0568
  -1.000   0.4553   0.01396   0.00617  -0.0986   0.5690   0.0962
  -0.750   0.4690   0.01314   0.00621  -0.0966   0.5680   0.3425
  -0.500   0.4824   0.01255   0.00629  -0.0941   0.5670   0.5458
  -0.250   0.5006   0.01234   0.00640  -0.0923   0.5660   0.6371
   0.000   0.5189   0.01218   0.00651  -0.0905   0.5647   0.7156
   0.250   0.5391   0.01201   0.00662  -0.0889   0.5633   0.7946
   0.500   0.6142   0.01196   0.00685  -0.0990   0.5620   0.9083
   0.750   0.6814   0.01227   0.00714  -0.1071   0.5608   0.9544
   1.000   0.7321   0.01255   0.00737  -0.1119   0.5597   0.9697
   1.250   0.7789   0.01270   0.00745  -0.1161   0.5587   0.9753
   1.500   0.8160   0.01283   0.00753  -0.1184   0.5577   0.9819
   1.750   0.8595   0.01289   0.00752  -0.1221   0.5567   0.9849
   2.000   0.9011   0.01297   0.00753  -0.1253   0.5558   0.9888
   2.250   0.9406   0.01309   0.00759  -0.1282   0.5547   0.9929
   2.500   0.9816   0.01332   0.00776  -0.1315   0.5534   0.9960
   2.750   1.0216   0.01340   0.00787  -0.1347   0.5525   0.9995
   3.000   1.0432   0.01354   0.00804  -0.1340   0.5513   1.0000
   3.250   1.0615   0.01371   0.00823  -0.1327   0.5500   1.0000
   3.500   1.0805   0.01386   0.00841  -0.1314   0.5485   1.0000
   3.750   1.1003   0.01403   0.00858  -0.1303   0.5472   1.0000
   4.000   1.1208   0.01419   0.00875  -0.1293   0.5460   1.0000
   4.250   1.1420   0.01432   0.00889  -0.1284   0.5448   1.0000
   4.500   1.1644   0.01441   0.00898  -0.1278   0.5436   1.0000
   4.750   1.1879   0.01449   0.00905  -0.1273   0.5425   1.0000
   5.000   1.2119   0.01460   0.00913  -0.1269   0.5415   1.0000
   5.250   1.2365   0.01473   0.00925  -0.1267   0.5405   1.0000
   5.500   1.2617   0.01492   0.00942  -0.1266   0.5394   1.0000
   5.750   1.2815   0.01523   0.00976  -0.1256   0.5380   1.0000
   6.000   1.2969   0.01550   0.01011  -0.1237   0.5366   1.0000
   6.250   1.3122   0.01580   0.01048  -0.1218   0.5351   1.0000
   6.500   1.3288   0.01606   0.01079  -0.1202   0.5334   1.0000
   6.750   1.3470   0.01626   0.01103  -0.1188   0.5318   1.0000
   7.000   1.3667   0.01643   0.01123  -0.1177   0.5304   1.0000
   7.250   1.3881   0.01656   0.01139  -0.1169   0.5291   1.0000
   7.500   1.4119   0.01663   0.01147  -0.1166   0.5279   1.0000
   7.750   1.4376   0.01670   0.01155  -0.1166   0.5268   1.0000
   8.000   1.4649   0.01678   0.01162  -0.1170   0.5256   1.0000
   8.250   1.4925   0.01699   0.01183  -0.1175   0.5244   1.0000
   8.500   1.5007   0.01742   0.01236  -0.1144   0.5227   1.0000
   8.750   1.5033   0.01789   0.01295  -0.1103   0.5204   1.0000
   9.000   1.5109   0.01825   0.01339  -0.1072   0.5182   1.0000
   9.250   1.5232   0.01853   0.01372  -0.1049   0.5164   1.0000
   9.500   1.5402   0.01866   0.01389  -0.1034   0.5147   1.0000
   9.750   1.5638   0.01867   0.01393  -0.1031   0.5133   1.0000
  10.000   1.5933   0.01864   0.01392  -0.1038   0.5120   1.0000
  10.250   1.6276   0.01863   0.01391  -0.1055   0.5107   1.0000
  10.500   1.6349   0.01905   0.01440  -0.1024   0.5087   1.0000
  10.750   1.5916   0.02029   0.01579  -0.0912   0.5049   1.0000
  11.000   1.5883   0.02109   0.01667  -0.0873   0.5019   1.0000
  11.250   1.6108   0.02111   0.01673  -0.0870   0.4998   1.0000
  11.500   1.6534   0.02029   0.01590  -0.0892   0.4977   1.0000
  11.750   1.6492   0.02099   0.01666  -0.0854   0.4926   1.0000
  12.000   1.6344   0.02240   0.01815  -0.0810   0.4862   1.0000
  12.250   1.6424   0.02285   0.01857  -0.0794   0.4782   1.0000
  12.500   1.6323   0.02473   0.02047  -0.0766   0.4684   1.0000
  12.750   1.5964   0.02894   0.02479  -0.0723   0.4593   1.0000
  13.000   1.5924   0.03093   0.02677  -0.0704   0.4498   1.0000
  13.250   1.5761   0.03402   0.02992  -0.0678   0.4408   1.0000
  13.500   1.5560   0.03761   0.03356  -0.0651   0.4311   1.0000
  13.750   1.5698   0.03840   0.03432  -0.0645   0.4238   1.0000
  14.000   1.5509   0.04210   0.03808  -0.0622   0.4127   1.0000
  14.250   1.5473   0.04455   0.04057  -0.0607   0.4047   1.0000
  14.500   1.5471   0.04665   0.04265  -0.0595   0.3935   1.0000
  14.750   1.5382   0.04958   0.04554  -0.0578   0.3787   1.0000
  15.000   1.5347   0.05208   0.04803  -0.0565   0.3676   1.0000
  15.250   1.5283   0.05490   0.05083  -0.0551   0.3539   1.0000
  15.500   1.5208   0.05788   0.05379  -0.0538   0.3404   1.0000
  15.750   1.5091   0.06126   0.05707  -0.0523   0.3225   1.0000
  16.000   1.4925   0.06525   0.06098  -0.0507   0.3013   1.0000
  16.250   1.4818   0.06873   0.06441  -0.0495   0.2854   1.0000
  16.500   1.4607   0.07331   0.06886  -0.0480   0.2623   1.0000
  16.750   1.4457   0.07742   0.07289  -0.0468   0.2430   1.0000
  17.000   1.4240   0.08232   0.07765  -0.0456   0.2202   1.0000
  17.250   1.4099   0.08646   0.08171  -0.0448   0.1998   1.0000
  17.500   1.3908   0.09129   0.08641  -0.0439   0.1778   1.0000
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