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DELFT DU84-132V3 AIRFOIL (MEASURED) (du84132v-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: DELFT DU84-132V3 AIRFOIL (MEASURED) (du84132v-il)
Reynolds number: 1,000,000
Max Cl/Cd: 82.14 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-du84132v-il-1000000-n5.txt
Download as CSV file: xf-du84132v-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: DELFT DU84-132V3 AIRFOIL (MEASURED)             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.9338   0.05824   0.05525  -0.0812   1.0000   0.0107
 -15.750  -0.9509   0.05216   0.04904  -0.0850   1.0000   0.0108
 -15.500  -0.9862   0.04419   0.04083  -0.0896   1.0000   0.0106
 -15.250  -0.9959   0.04055   0.03708  -0.0908   1.0000   0.0106
 -15.000  -0.9788   0.04015   0.03671  -0.0904   1.0000   0.0109
 -14.750  -0.9845   0.03710   0.03355  -0.0912   0.9998   0.0109
 -14.500  -0.9717   0.03498   0.03135  -0.0934   0.9989   0.0110
 -14.250  -0.9591   0.03292   0.02920  -0.0954   0.9975   0.0112
 -14.000  -0.9396   0.03175   0.02800  -0.0968   0.9959   0.0114
 -13.750  -0.9224   0.03037   0.02655  -0.0982   0.9935   0.0116
 -13.500  -0.9113   0.02875   0.02483  -0.0989   0.9905   0.0117
 -13.250  -0.8952   0.02753   0.02354  -0.0997   0.9873   0.0118
 -13.000  -0.8762   0.02640   0.02234  -0.1008   0.9843   0.0120
 -12.750  -0.8568   0.02511   0.02095  -0.1022   0.9816   0.0121
 -12.500  -0.8448   0.02395   0.01970  -0.1020   0.9759   0.0122
 -12.250  -0.8247   0.02303   0.01870  -0.1026   0.9715   0.0124
 -12.000  -0.7977   0.02217   0.01776  -0.1042   0.9689   0.0125
 -11.500  -0.7483   0.02065   0.01608  -0.1057   0.9610   0.0127
 -11.250  -0.7186   0.02004   0.01540  -0.1072   0.9576   0.0128
 -11.000  -0.6863   0.01936   0.01465  -0.1092   0.9548   0.0129
 -10.750  -0.6564   0.01849   0.01369  -0.1109   0.9507   0.0130
 -10.500  -0.6319   0.01756   0.01268  -0.1114   0.9413   0.0131
 -10.250  -0.6031   0.01669   0.01172  -0.1128   0.9332   0.0134
 -10.000  -0.5737   0.01614   0.01112  -0.1139   0.9245   0.0135
  -9.750  -0.5461   0.01564   0.01055  -0.1145   0.9163   0.0137
  -9.500  -0.5196   0.01519   0.01003  -0.1148   0.9076   0.0139
  -9.250  -0.4956   0.01470   0.00947  -0.1146   0.8979   0.0140
  -9.000  -0.4715   0.01428   0.00896  -0.1143   0.8873   0.0141
  -8.750  -0.4474   0.01395   0.00857  -0.1139   0.8759   0.0143
  -8.500  -0.4231   0.01364   0.00819  -0.1135   0.8664   0.0146
  -8.250  -0.3993   0.01325   0.00772  -0.1130   0.8585   0.0147
  -8.000  -0.3748   0.01292   0.00733  -0.1126   0.8525   0.0149
  -7.750  -0.3503   0.01258   0.00693  -0.1123   0.8461   0.0151
  -7.500  -0.3257   0.01222   0.00650  -0.1119   0.8406   0.0152
  -7.250  -0.3007   0.01186   0.00610  -0.1115   0.8340   0.0154
  -7.000  -0.2760   0.01154   0.00573  -0.1111   0.8249   0.0155
  -6.750  -0.2507   0.01124   0.00538  -0.1108   0.8151   0.0157
  -6.500  -0.2256   0.01098   0.00505  -0.1104   0.8040   0.0158
  -6.250  -0.2004   0.01074   0.00474  -0.1099   0.7928   0.0160
  -6.000  -0.1749   0.01051   0.00446  -0.1096   0.7770   0.0161
  -5.750  -0.1499   0.01034   0.00420  -0.1091   0.7641   0.0162
  -5.500  -0.1242   0.01015   0.00395  -0.1087   0.7568   0.0163
  -5.250  -0.0987   0.00988   0.00361  -0.1084   0.7500   0.0166
  -5.000  -0.0721   0.00963   0.00334  -0.1083   0.7417   0.0169
  -4.750  -0.0454   0.00943   0.00311  -0.1081   0.7314   0.0172
  -4.500  -0.0196   0.00931   0.00292  -0.1077   0.7170   0.0175
  -4.250   0.0062   0.00921   0.00275  -0.1073   0.7034   0.0178
  -4.000   0.0327   0.00910   0.00259  -0.1071   0.6884   0.0182
  -3.750   0.0581   0.00905   0.00245  -0.1066   0.6683   0.0186
  -3.500   0.0841   0.00900   0.00232  -0.1062   0.6549   0.0191
  -3.250   0.1110   0.00893   0.00221  -0.1060   0.6369   0.0196
  -3.000   0.1367   0.00892   0.00211  -0.1056   0.6188   0.0201
  -2.750   0.1634   0.00886   0.00200  -0.1054   0.6091   0.0220
  -2.500   0.1906   0.00878   0.00191  -0.1053   0.5957   0.0245
  -2.250   0.2167   0.00874   0.00186  -0.1050   0.5784   0.0400
  -2.000   0.2431   0.00874   0.00182  -0.1047   0.5650   0.0439
  -1.750   0.2702   0.00873   0.00178  -0.1045   0.5546   0.0471
  -1.500   0.2971   0.00875   0.00175  -0.1043   0.5432   0.0486
  -1.250   0.3237   0.00877   0.00172  -0.1041   0.5282   0.0512
  -1.000   0.3496   0.00882   0.00171  -0.1037   0.5101   0.0552
  -0.750   0.3755   0.00877   0.00168  -0.1034   0.4957   0.0890
  -0.500   0.4014   0.00866   0.00167  -0.1032   0.4800   0.1413
  -0.250   0.4274   0.00869   0.00167  -0.1029   0.4477   0.1633
   0.000   0.4499   0.00879   0.00173  -0.1021   0.3985   0.2257
   0.250   0.4738   0.00886   0.00181  -0.1016   0.3710   0.2787
   0.500   0.4988   0.00873   0.00187  -0.1013   0.3502   0.3718
   0.750   0.5242   0.00879   0.00194  -0.1010   0.3263   0.4107
   1.000   0.5492   0.00888   0.00201  -0.1005   0.3054   0.4454
   1.250   0.5749   0.00881   0.00208  -0.1003   0.2920   0.5153
   1.500   0.5998   0.00863   0.00218  -0.1000   0.2766   0.6313
   1.750   0.6248   0.00874   0.00237  -0.0994   0.2640   0.6890
   2.000   0.6505   0.00891   0.00252  -0.0989   0.2547   0.7049
   2.250   0.6768   0.00905   0.00264  -0.0986   0.2479   0.7155
   2.500   0.7028   0.00921   0.00277  -0.0982   0.2422   0.7222
   2.750   0.7294   0.00933   0.00289  -0.0980   0.2372   0.7293
   3.000   0.7546   0.00954   0.00303  -0.0975   0.2222   0.7351
   3.250   0.7786   0.00981   0.00321  -0.0968   0.2009   0.7391
   3.500   0.8017   0.01014   0.00342  -0.0959   0.1784   0.7427
   3.750   0.8239   0.01053   0.00367  -0.0949   0.1496   0.7479
   4.000   0.8479   0.01079   0.00387  -0.0942   0.1410   0.7505
   4.250   0.8727   0.01096   0.00404  -0.0937   0.1360   0.7528
   4.500   0.8975   0.01114   0.00422  -0.0931   0.1310   0.7550
   4.750   0.9211   0.01139   0.00444  -0.0924   0.1237   0.7569
   5.000   0.9426   0.01175   0.00470  -0.0913   0.1001   0.7589
   5.250   0.9646   0.01208   0.00495  -0.0902   0.0881   0.7607
   5.500   0.9878   0.01231   0.00517  -0.0894   0.0830   0.7625
   5.750   1.0109   0.01255   0.00538  -0.0886   0.0796   0.7643
   6.000   1.0335   0.01279   0.00562  -0.0877   0.0765   0.7659
   6.250   1.0555   0.01302   0.00584  -0.0867   0.0734   0.7677
   6.500   1.0770   0.01321   0.00605  -0.0855   0.0720   0.7694
   6.750   1.0980   0.01340   0.00626  -0.0843   0.0709   0.7707
   7.000   1.1187   0.01362   0.00650  -0.0830   0.0689   0.7720
   7.250   1.1390   0.01387   0.00676  -0.0817   0.0671   0.7733
   7.500   1.1584   0.01416   0.00705  -0.0803   0.0644   0.7746
   7.750   1.1779   0.01445   0.00734  -0.0789   0.0619   0.7758
   8.000   1.1981   0.01471   0.00762  -0.0776   0.0596   0.7769
   8.250   1.2131   0.01522   0.00803  -0.0755   0.0445   0.7780
   8.500   1.2305   0.01563   0.00840  -0.0739   0.0422   0.7791
   8.750   1.2485   0.01599   0.00877  -0.0723   0.0408   0.7802
   9.000   1.2663   0.01637   0.00916  -0.0708   0.0392   0.7812
   9.250   1.2842   0.01674   0.00955  -0.0693   0.0381   0.7821
   9.500   1.3018   0.01712   0.00996  -0.0678   0.0375   0.7830
   9.750   1.3189   0.01752   0.01040  -0.0662   0.0368   0.7841
  10.000   1.3353   0.01796   0.01088  -0.0646   0.0361   0.7851
  10.250   1.3506   0.01846   0.01143  -0.0629   0.0350   0.7862
  10.500   1.3642   0.01907   0.01206  -0.0610   0.0334   0.7873
  10.750   1.3786   0.01964   0.01267  -0.0592   0.0324   0.7885
  11.000   1.3943   0.02015   0.01323  -0.0577   0.0317   0.7898
  11.250   1.4104   0.02065   0.01377  -0.0563   0.0306   0.7911
  11.500   1.4251   0.02124   0.01440  -0.0547   0.0281   0.7922
  12.000   1.4468   0.02293   0.01607  -0.0510   0.0212   0.7945
  12.250   1.4568   0.02387   0.01702  -0.0491   0.0196   0.7956
  12.500   1.4670   0.02482   0.01801  -0.0474   0.0184   0.7966
  12.750   1.4781   0.02574   0.01898  -0.0458   0.0179   0.7975
  13.000   1.4884   0.02674   0.02003  -0.0443   0.0174   0.7985
  13.250   1.4978   0.02783   0.02118  -0.0427   0.0170   0.7997
  13.500   1.5057   0.02906   0.02247  -0.0412   0.0164   0.8008
  13.750   1.5131   0.03038   0.02384  -0.0397   0.0159   0.8019
  14.000   1.5202   0.03177   0.02530  -0.0383   0.0154   0.8031
  14.250   1.5273   0.03322   0.02681  -0.0371   0.0150   0.8042
  14.500   1.5353   0.03463   0.02829  -0.0360   0.0148   0.8053
  14.750   1.5428   0.03614   0.02987  -0.0350   0.0144   0.8064
  15.000   1.5494   0.03779   0.03160  -0.0341   0.0139   0.8076
  15.250   1.5548   0.03961   0.03349  -0.0333   0.0136   0.8087
  15.500   1.5594   0.04156   0.03550  -0.0326   0.0131   0.8097
  15.750   1.5630   0.04369   0.03770  -0.0319   0.0129   0.8107
  16.000   1.5645   0.04612   0.04019  -0.0314   0.0123   0.8117
  16.250   1.5677   0.04845   0.04260  -0.0311   0.0119   0.8126
  16.750   1.5739   0.05335   0.04766  -0.0310   0.0112   0.8147
  17.000   1.5754   0.05610   0.05050  -0.0311   0.0107   0.8158
  17.250   1.5756   0.05911   0.05359  -0.0314   0.0102   0.8169
  17.500   1.5743   0.06239   0.05695  -0.0318   0.0098   0.8179
  17.750   1.5728   0.06578   0.06043  -0.0325   0.0092   0.8190
  18.000   1.5711   0.06931   0.06404  -0.0333   0.0086   0.8200
  18.250   1.5676   0.07319   0.06800  -0.0343   0.0079   0.8210
  18.500   1.5624   0.07740   0.07229  -0.0356   0.0072   0.8221
  18.750   1.5565   0.08182   0.07680  -0.0370   0.0066   0.8231
  19.000   1.5494   0.08656   0.08164  -0.0388   0.0061   0.8240
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