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DELFT DU84-132V3 AIRFOIL (MEASURED) (du84132v-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: DELFT DU84-132V3 AIRFOIL (MEASURED) (du84132v-il)
Reynolds number: 500,000
Max Cl/Cd: 75.33 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-du84132v-il-500000-n5.txt
Download as CSV file: xf-du84132v-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.6523   0.06777   0.06469  -0.0714   1.0000   0.0162
 -13.000  -0.6890   0.05829   0.05504  -0.0777   1.0000   0.0162
 -12.750  -0.7146   0.05221   0.04880  -0.0810   1.0000   0.0161
 -12.500  -0.7311   0.04720   0.04363  -0.0842   0.9992   0.0161
 -12.250  -0.7336   0.04248   0.03868  -0.0893   0.9960   0.0161
 -12.000  -0.7323   0.03887   0.03486  -0.0926   0.9916   0.0161
 -11.750  -0.7271   0.03627   0.03207  -0.0946   0.9863   0.0162
 -11.500  -0.7172   0.03377   0.02935  -0.0971   0.9815   0.0162
 -11.250  -0.7087   0.03184   0.02723  -0.0977   0.9738   0.0162
 -11.000  -0.6900   0.02989   0.02509  -0.0992   0.9697   0.0162
 -10.750  -0.6704   0.02756   0.02254  -0.1010   0.9671   0.0164
 -10.500  -0.6564   0.02608   0.02093  -0.1003   0.9599   0.0165
 -10.250  -0.6334   0.02461   0.01935  -0.1013   0.9562   0.0168
 -10.000  -0.6056   0.02343   0.01806  -0.1028   0.9538   0.0170
  -9.750  -0.5790   0.02255   0.01713  -0.1038   0.9499   0.0173
  -9.500  -0.5561   0.02174   0.01623  -0.1038   0.9430   0.0176
  -9.250  -0.5268   0.02068   0.01505  -0.1052   0.9388   0.0177
  -9.000  -0.4999   0.01971   0.01396  -0.1058   0.9335   0.0178
  -8.750  -0.4724   0.01880   0.01295  -0.1065   0.9276   0.0179
  -8.500  -0.4414   0.01793   0.01197  -0.1078   0.9229   0.0180
  -8.250  -0.4135   0.01716   0.01112  -0.1084   0.9169   0.0181
  -8.000  -0.3855   0.01646   0.01033  -0.1090   0.9111   0.0182
  -7.750  -0.3557   0.01578   0.00956  -0.1099   0.9060   0.0184
  -7.500  -0.3306   0.01522   0.00894  -0.1098   0.8987   0.0185
  -7.250  -0.3036   0.01467   0.00831  -0.1100   0.8918   0.0187
  -7.000  -0.2776   0.01417   0.00775  -0.1100   0.8842   0.0189
  -6.750  -0.2514   0.01372   0.00723  -0.1099   0.8760   0.0191
  -6.500  -0.2252   0.01329   0.00674  -0.1098   0.8680   0.0193
  -6.250  -0.1990   0.01291   0.00628  -0.1097   0.8599   0.0195
  -6.000  -0.1727   0.01256   0.00587  -0.1096   0.8530   0.0197
  -5.750  -0.1467   0.01224   0.00550  -0.1094   0.8461   0.0199
  -5.500  -0.1199   0.01196   0.00515  -0.1093   0.8395   0.0201
  -5.250  -0.0951   0.01158   0.00474  -0.1089   0.8309   0.0204
  -5.000  -0.0691   0.01127   0.00438  -0.1087   0.8226   0.0208
  -4.750  -0.0431   0.01100   0.00408  -0.1084   0.8135   0.0213
  -4.500  -0.0166   0.01078   0.00381  -0.1082   0.8045   0.0218
  -4.250   0.0099   0.01059   0.00356  -0.1080   0.7948   0.0225
  -4.000   0.0361   0.01040   0.00334  -0.1077   0.7814   0.0235
  -3.750   0.0623   0.01026   0.00312  -0.1073   0.7683   0.0246
  -3.500   0.0886   0.01012   0.00291  -0.1070   0.7577   0.0266
  -3.250   0.1150   0.00999   0.00277  -0.1067   0.7483   0.0309
  -3.000   0.1417   0.00990   0.00268  -0.1065   0.7373   0.0427
  -2.750   0.1684   0.00983   0.00257  -0.1063   0.7239   0.0478
  -2.500   0.1947   0.00976   0.00244  -0.1059   0.7133   0.0522
  -2.250   0.2210   0.00970   0.00234  -0.1056   0.7012   0.0576
  -2.000   0.2470   0.00948   0.00222  -0.1054   0.6865   0.0911
  -1.750   0.2720   0.00925   0.00212  -0.1050   0.6709   0.1496
  -1.500   0.2975   0.00912   0.00205  -0.1047   0.6576   0.1860
  -1.000   0.3489   0.00877   0.00194  -0.1042   0.6272   0.2969
  -0.750   0.3741   0.00853   0.00192  -0.1039   0.6143   0.3857
  -0.500   0.4002   0.00834   0.00189  -0.1037   0.6015   0.4487
  -0.250   0.4260   0.00816   0.00187  -0.1035   0.5878   0.5178
   0.000   0.4505   0.00797   0.00195  -0.1029   0.5753   0.6078
   0.250   0.4747   0.00807   0.00217  -0.1020   0.5628   0.6739
   0.500   0.5000   0.00825   0.00230  -0.1014   0.5470   0.6966
   0.750   0.5250   0.00844   0.00242  -0.1007   0.5263   0.7096
   1.000   0.5493   0.00868   0.00254  -0.0999   0.5047   0.7197
   1.250   0.5745   0.00889   0.00266  -0.0993   0.4878   0.7288
   1.500   0.6006   0.00904   0.00278  -0.0989   0.4730   0.7362
   1.750   0.6246   0.00930   0.00293  -0.0981   0.4423   0.7441
   2.000   0.6477   0.00962   0.00310  -0.0971   0.4100   0.7515
   2.250   0.6695   0.01001   0.00335  -0.0959   0.3839   0.7571
   2.500   0.6934   0.01030   0.00354  -0.0951   0.3659   0.7621
   2.750   0.7180   0.01055   0.00370  -0.0945   0.3471   0.7655
   3.000   0.7420   0.01079   0.00386  -0.0938   0.3272   0.7677
   3.250   0.7652   0.01107   0.00404  -0.0930   0.3086   0.7699
   3.500   0.7890   0.01131   0.00422  -0.0922   0.2936   0.7719
   3.750   0.8135   0.01151   0.00439  -0.0916   0.2838   0.7739
   4.000   0.8377   0.01173   0.00456  -0.0910   0.2717   0.7763
   4.250   0.8618   0.01195   0.00474  -0.0903   0.2636   0.7789
   4.500   0.8857   0.01219   0.00493  -0.0896   0.2558   0.7815
   4.750   0.9095   0.01239   0.00512  -0.0890   0.2476   0.7835
   5.000   0.9323   0.01262   0.00532  -0.0881   0.2404   0.7851
   5.250   0.9566   0.01277   0.00551  -0.0874   0.2333   0.7866
   5.500   0.9793   0.01300   0.00571  -0.0866   0.2214   0.7879
   5.750   1.0006   0.01331   0.00594  -0.0855   0.2028   0.7891
   6.000   1.0196   0.01370   0.00622  -0.0840   0.1812   0.7903
   6.250   1.0341   0.01426   0.00661  -0.0818   0.1482   0.7917
   6.500   1.0516   0.01466   0.00694  -0.0800   0.1386   0.7931
   6.750   1.0710   0.01498   0.00725  -0.0786   0.1287   0.7948
   7.000   1.0901   0.01532   0.00759  -0.0771   0.1185   0.7964
   7.250   1.1054   0.01589   0.00803  -0.0752   0.0984   0.7978
   7.500   1.1231   0.01628   0.00841  -0.0735   0.0923   0.7988
   7.750   1.1407   0.01668   0.00880  -0.0719   0.0873   0.7998
   8.000   1.1593   0.01703   0.00918  -0.0705   0.0845   0.8009
   8.250   1.1779   0.01738   0.00957  -0.0691   0.0824   0.8020
   8.500   1.1955   0.01778   0.01001  -0.0676   0.0797   0.8032
   8.750   1.2121   0.01824   0.01049  -0.0659   0.0767   0.8044
   9.000   1.2282   0.01873   0.01100  -0.0642   0.0737   0.8056
   9.250   1.2460   0.01914   0.01146  -0.0629   0.0721   0.8069
   9.500   1.2632   0.01957   0.01195  -0.0614   0.0700   0.8082
   9.750   1.2796   0.02006   0.01248  -0.0599   0.0672   0.8095
  10.000   1.2947   0.02063   0.01307  -0.0583   0.0642   0.8108
  10.250   1.3093   0.02125   0.01372  -0.0567   0.0614   0.8121
  10.500   1.3251   0.02179   0.01432  -0.0552   0.0585   0.8134
  10.750   1.3390   0.02244   0.01499  -0.0536   0.0529   0.8148
  11.000   1.3501   0.02327   0.01580  -0.0518   0.0455   0.8161
  11.250   1.3611   0.02414   0.01668  -0.0500   0.0430   0.8174
  11.500   1.3718   0.02506   0.01762  -0.0482   0.0412   0.8188
  11.750   1.3822   0.02604   0.01864  -0.0465   0.0395   0.8201
  12.000   1.3923   0.02706   0.01972  -0.0449   0.0380   0.8215
  12.250   1.4029   0.02808   0.02083  -0.0434   0.0367   0.8230
  12.500   1.4116   0.02927   0.02210  -0.0419   0.0351   0.8244
  12.750   1.4178   0.03069   0.02358  -0.0403   0.0335   0.8258
  13.000   1.4237   0.03220   0.02514  -0.0388   0.0320   0.8271
  13.250   1.4355   0.03329   0.02633  -0.0378   0.0305   0.8284
  13.500   1.4446   0.03461   0.02774  -0.0367   0.0280   0.8298
  13.750   1.4517   0.03614   0.02934  -0.0356   0.0262   0.8313
  14.000   1.4583   0.03776   0.03104  -0.0347   0.0246   0.8328
  14.250   1.4634   0.03958   0.03290  -0.0338   0.0228   0.8343
  14.500   1.4674   0.04157   0.03494  -0.0330   0.0215   0.8359
  14.750   1.4713   0.04366   0.03710  -0.0323   0.0208   0.8376
  15.000   1.4734   0.04600   0.03951  -0.0318   0.0199   0.8393
  15.250   1.4742   0.04858   0.04216  -0.0314   0.0190   0.8409
  15.500   1.4755   0.05123   0.04489  -0.0312   0.0184   0.8425
  16.000   1.4782   0.05679   0.05069  -0.0314   0.0176   0.8459
  16.250   1.4780   0.05991   0.05393  -0.0317   0.0172   0.8479
  16.500   1.4769   0.06326   0.05739  -0.0323   0.0168   0.8500
  16.750   1.4748   0.06685   0.06109  -0.0330   0.0164   0.8522
  17.000   1.4712   0.07076   0.06512  -0.0340   0.0160   0.8545
  17.250   1.4667   0.07494   0.06941  -0.0353   0.0157   0.8570
  17.750   1.4533   0.08428   0.07900  -0.0385   0.0150   0.8635
  18.000   1.4503   0.08855   0.08342  -0.0401   0.0148   0.8687
  18.500   1.4427   0.09791   0.09317  -0.0444   0.0141   0.9107
  18.750   1.4355   0.10296   0.09835  -0.0467   0.0138   1.0000
  19.000   1.4287   0.10811   0.10362  -0.0491   0.0135   1.0000
  19.250   1.4213   0.11342   0.10904  -0.0516   0.0131   1.0000
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