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DEFIANT CANARD BL20 AIRFOIL (defcnd1-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: DEFIANT CANARD BL20 AIRFOIL (defcnd1-il)
Reynolds number: 500,000
Max Cl/Cd: 92.44 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-defcnd1-il-500000-n5.txt
Download as CSV file: xf-defcnd1-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: DEFIANT CANARD BL20 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.6243   0.08592   0.08076  -0.0893   0.7025   0.0206
 -17.250  -0.6439   0.07968   0.07440  -0.0927   0.6981   0.0208
 -17.000  -0.6647   0.07346   0.06805  -0.0960   0.6936   0.0207
 -16.750  -0.6855   0.06744   0.06189  -0.0992   0.6892   0.0209
 -16.500  -0.7029   0.06213   0.05645  -0.1020   0.6845   0.0210
 -16.250  -0.7241   0.05665   0.05086  -0.1048   0.6810   0.0213
 -16.000  -0.7420   0.05183   0.04593  -0.1070   0.6764   0.0215
 -15.750  -0.7560   0.04765   0.04164  -0.1088   0.6717   0.0217
 -15.500  -0.7681   0.04381   0.03769  -0.1103   0.6669   0.0221
 -15.250  -0.7767   0.04043   0.03419  -0.1115   0.6629   0.0221
 -15.000  -0.7830   0.03732   0.03100  -0.1125   0.6588   0.0227
 -14.750  -0.7862   0.03459   0.02818  -0.1132   0.6544   0.0231
 -14.500  -0.7887   0.03208   0.02556  -0.1136   0.6499   0.0236
 -14.250  -0.7893   0.02996   0.02332  -0.1136   0.6455   0.0240
 -14.000  -0.7904   0.02799   0.02127  -0.1132   0.6417   0.0245
 -13.750  -0.7905   0.02632   0.01953  -0.1123   0.6373   0.0252
 -13.500  -0.7887   0.02497   0.01811  -0.1109   0.6329   0.0259
 -13.250  -0.7849   0.02387   0.01693  -0.1092   0.6288   0.0266
 -13.000  -0.7799   0.02294   0.01591  -0.1072   0.6250   0.0276
 -12.750  -0.7750   0.02205   0.01497  -0.1050   0.6216   0.0286
 -12.500  -0.7677   0.02130   0.01417  -0.1027   0.6180   0.0297
 -12.000  -0.7510   0.02000   0.01278  -0.0977   0.6101   0.0328
 -11.750  -0.7410   0.01946   0.01219  -0.0952   0.6062   0.0346
 -11.500  -0.7320   0.01896   0.01164  -0.0923   0.6027   0.0369
 -11.250  -0.7203   0.01855   0.01120  -0.0898   0.5998   0.0393
 -11.000  -0.7064   0.01808   0.01072  -0.0877   0.5966   0.0424
 -10.750  -0.6902   0.01764   0.01026  -0.0859   0.5931   0.0456
 -10.500  -0.6727   0.01724   0.00982  -0.0843   0.5895   0.0493
 -10.000  -0.6352   0.01649   0.00901  -0.0814   0.5823   0.0577
  -9.750  -0.6149   0.01612   0.00865  -0.0802   0.5793   0.0623
  -9.500  -0.5937   0.01579   0.00833  -0.0791   0.5762   0.0672
  -9.250  -0.5716   0.01551   0.00803  -0.0781   0.5729   0.0722
  -9.000  -0.5488   0.01525   0.00776  -0.0771   0.5696   0.0773
  -8.750  -0.5257   0.01503   0.00752  -0.0763   0.5662   0.0818
  -8.500  -0.5017   0.01485   0.00728  -0.0755   0.5629   0.0863
  -8.250  -0.4773   0.01464   0.00708  -0.0748   0.5599   0.0904
  -8.000  -0.4521   0.01448   0.00688  -0.0742   0.5568   0.0941
  -7.750  -0.4276   0.01428   0.00668  -0.0736   0.5537   0.0973
  -7.500  -0.4024   0.01413   0.00649  -0.0730   0.5506   0.1007
  -7.250  -0.3768   0.01401   0.00631  -0.0724   0.5474   0.1040
  -7.000  -0.3521   0.01386   0.00615  -0.0718   0.5442   0.1081
  -6.750  -0.3257   0.01374   0.00601  -0.0714   0.5413   0.1120
  -6.500  -0.2999   0.01358   0.00583  -0.0709   0.5384   0.1148
  -6.250  -0.2746   0.01340   0.00565  -0.0704   0.5354   0.1175
  -6.000  -0.2489   0.01326   0.00548  -0.0698   0.5325   0.1201
  -5.750  -0.2228   0.01315   0.00531  -0.0694   0.5294   0.1226
  -5.500  -0.1966   0.01307   0.00516  -0.0689   0.5262   0.1246
  -5.250  -0.1712   0.01289   0.00498  -0.0684   0.5234   0.1272
  -5.000  -0.1452   0.01273   0.00483  -0.0679   0.5207   0.1300
  -4.750  -0.1189   0.01260   0.00469  -0.0675   0.5179   0.1328
  -4.500  -0.0923   0.01250   0.00455  -0.0671   0.5149   0.1355
  -4.250  -0.0660   0.01239   0.00442  -0.0667   0.5119   0.1383
  -4.000  -0.0403   0.01227   0.00427  -0.0662   0.5088   0.1418
  -3.750  -0.0141   0.01217   0.00415  -0.0658   0.5059   0.1454
  -3.500   0.0129   0.01207   0.00406  -0.0655   0.5034   0.1492
  -3.250   0.0394   0.01195   0.00395  -0.0651   0.5008   0.1540
  -3.000   0.0659   0.01184   0.00385  -0.0648   0.4978   0.1598
  -2.750   0.0923   0.01174   0.00376  -0.0644   0.4947   0.1671
  -2.500   0.1183   0.01164   0.00366  -0.0640   0.4916   0.1782
  -2.250   0.1440   0.01153   0.00358  -0.0635   0.4888   0.1936
  -2.000   0.1701   0.01137   0.00351  -0.0631   0.4864   0.2148
  -1.750   0.1959   0.01120   0.00345  -0.0627   0.4837   0.2428
  -1.500   0.2216   0.01105   0.00341  -0.0622   0.4806   0.2717
  -1.250   0.2474   0.01094   0.00338  -0.0618   0.4775   0.3001
  -1.000   0.2734   0.01087   0.00337  -0.0614   0.4746   0.3250
  -0.750   0.2994   0.01084   0.00337  -0.0610   0.4718   0.3456
  -0.500   0.3260   0.01082   0.00338  -0.0606   0.4692   0.3626
  -0.250   0.3529   0.01079   0.00340  -0.0604   0.4663   0.3774
   0.000   0.3798   0.01078   0.00342  -0.0601   0.4632   0.3899
   0.250   0.4065   0.01079   0.00344  -0.0598   0.4603   0.4027
   0.500   0.4328   0.01080   0.00347  -0.0594   0.4573   0.4144
   0.750   0.4591   0.01085   0.00350  -0.0590   0.4541   0.4256
   1.000   0.4854   0.01086   0.00354  -0.0587   0.4514   0.4369
   1.250   0.5121   0.01087   0.00360  -0.0584   0.4487   0.4504
   1.500   0.5383   0.01088   0.00365  -0.0580   0.4457   0.4648
   1.750   0.5642   0.01091   0.00371  -0.0576   0.4424   0.4767
   2.000   0.5898   0.01096   0.00376  -0.0571   0.4391   0.4886
   2.250   0.6148   0.01101   0.00382  -0.0566   0.4361   0.5003
   2.750   0.6662   0.01105   0.00396  -0.0557   0.4305   0.5274
   3.000   0.6910   0.01106   0.00404  -0.0551   0.4271   0.5439
   3.250   0.7153   0.01109   0.00411  -0.0544   0.4238   0.5606
   3.500   0.7386   0.01112   0.00420  -0.0536   0.4208   0.5815
   3.750   0.7610   0.01114   0.00430  -0.0526   0.4178   0.6110
   4.000   0.7832   0.01108   0.00442  -0.0515   0.4149   0.6549
   4.250   0.8031   0.01099   0.00454  -0.0499   0.4117   0.7174
   4.500   0.8215   0.01087   0.00469  -0.0479   0.4085   0.7963
   4.750   0.8504   0.01086   0.00491  -0.0481   0.4051   0.8781
   5.000   0.9083   0.01111   0.00520  -0.0545   0.4009   0.9288
   5.250   0.9637   0.01133   0.00544  -0.0603   0.3970   0.9505
   5.500   1.0040   0.01153   0.00563  -0.0631   0.3931   0.9641
   5.750   1.0394   0.01174   0.00583  -0.0649   0.3892   0.9739
   6.000   1.0711   0.01199   0.00604  -0.0660   0.3854   0.9832
   6.250   1.1040   0.01219   0.00625  -0.0673   0.3820   0.9909
   6.500   1.1372   0.01241   0.00647  -0.0687   0.3783   0.9973
   6.750   1.1684   0.01264   0.00670  -0.0698   0.3744   1.0000
   7.000   1.1818   0.01286   0.00690  -0.0672   0.3709   1.0000
   7.250   1.1949   0.01309   0.00711  -0.0647   0.3675   1.0000
   7.500   1.2088   0.01328   0.00732  -0.0622   0.3643   1.0000
   7.750   1.2189   0.01347   0.00753  -0.0590   0.3610   1.0000
   8.000   1.2283   0.01372   0.00777  -0.0558   0.3574   1.0000
   8.250   1.2372   0.01404   0.00807  -0.0527   0.3538   1.0000
   8.500   1.2493   0.01436   0.00840  -0.0503   0.3506   1.0000
   8.750   1.2635   0.01467   0.00874  -0.0483   0.3472   1.0000
   9.000   1.2766   0.01505   0.00914  -0.0462   0.3437   1.0000
   9.250   1.2879   0.01554   0.00963  -0.0440   0.3400   1.0000
   9.500   1.2971   0.01616   0.01023  -0.0418   0.3362   1.0000
   9.750   1.3117   0.01665   0.01078  -0.0403   0.3330   1.0000
  10.000   1.3245   0.01728   0.01143  -0.0389   0.3291   1.0000
  10.250   1.3357   0.01804   0.01221  -0.0373   0.3253   1.0000
  10.500   1.3443   0.01902   0.01319  -0.0358   0.3215   1.0000
  10.750   1.3559   0.01993   0.01414  -0.0347   0.3178   1.0000
  11.000   1.3679   0.02089   0.01514  -0.0338   0.3139   1.0000
  11.250   1.3780   0.02204   0.01631  -0.0329   0.3101   1.0000
  11.500   1.3854   0.02339   0.01767  -0.0319   0.3063   1.0000
  11.750   1.3945   0.02466   0.01897  -0.0311   0.3029   1.0000
  12.000   1.4049   0.02588   0.02023  -0.0304   0.2990   1.0000
  12.250   1.4126   0.02729   0.02167  -0.0296   0.2952   1.0000
  12.500   1.4172   0.02892   0.02332  -0.0287   0.2911   1.0000
  12.750   1.4230   0.03048   0.02489  -0.0278   0.2877   1.0000
  13.000   1.4313   0.03189   0.02636  -0.0272   0.2842   1.0000
  13.250   1.4371   0.03349   0.02800  -0.0265   0.2802   1.0000
  13.500   1.4396   0.03537   0.02990  -0.0257   0.2763   1.0000
  13.750   1.4430   0.03723   0.03176  -0.0249   0.2724   1.0000
  14.000   1.4499   0.03886   0.03346  -0.0244   0.2690   1.0000
  14.250   1.4553   0.04064   0.03527  -0.0239   0.2652   1.0000
  14.500   1.4528   0.04315   0.03778  -0.0233   0.2598   1.0000
  14.750   1.4573   0.04510   0.03977  -0.0229   0.2554   1.0000
  15.000   1.4608   0.04717   0.04189  -0.0225   0.2513   1.0000
  15.250   1.4633   0.04934   0.04408  -0.0222   0.2472   1.0000
  15.500   1.4626   0.05185   0.04660  -0.0218   0.2428   1.0000
  15.750   1.4689   0.05373   0.04853  -0.0216   0.2393   1.0000
  16.000   1.4695   0.05619   0.05103  -0.0214   0.2348   1.0000
  16.250   1.4707   0.05857   0.05343  -0.0212   0.2311   1.0000
  16.500   1.4713   0.06108   0.05598  -0.0211   0.2268   1.0000
  16.750   1.4726   0.06356   0.05850  -0.0210   0.2220   1.0000
  17.000   1.4720   0.06622   0.06118  -0.0209   0.2179   1.0000
  17.250   1.4705   0.06902   0.06400  -0.0209   0.2136   1.0000
  17.500   1.4730   0.07142   0.06646  -0.0209   0.2092   1.0000
  17.750   1.4686   0.07461   0.06968  -0.0210   0.2043   1.0000
  18.000   1.4671   0.07746   0.07254  -0.0211   0.1999   1.0000
  18.250   1.4660   0.08035   0.07548  -0.0214   0.1952   1.0000
  18.500   1.4616   0.08360   0.07875  -0.0216   0.1900   1.0000
  18.750   1.4592   0.08667   0.08185  -0.0219   0.1859   1.0000
  19.000   1.4593   0.08945   0.08468  -0.0222   0.1818   1.0000
  19.250   1.4555   0.09270   0.08796  -0.0226   0.1772   1.0000
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