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DELFT DU84-132V3 AIRFOIL (MEASURED) (du84132v-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: DELFT DU84-132V3 AIRFOIL (MEASURED) (du84132v-il)
Reynolds number: 100,000
Max Cl/Cd: 52.5 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-du84132v-il-100000-n5.txt
Download as CSV file: xf-du84132v-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.4206   0.09515   0.08975  -0.0541   1.0000   0.0406
 -10.500  -0.4241   0.09189   0.08654  -0.0542   1.0000   0.0403
 -10.250  -0.4327   0.08772   0.08243  -0.0548   1.0000   0.0400
 -10.000  -0.4457   0.08283   0.07761  -0.0558   1.0000   0.0395
  -9.750  -0.4718   0.07551   0.07034  -0.0588   1.0000   0.0389
  -9.500  -0.5102   0.06929   0.06413  -0.0607   1.0000   0.0384
  -9.250  -0.5500   0.06569   0.06052  -0.0589   1.0000   0.0381
  -9.000  -0.5853   0.06239   0.05715  -0.0574   0.9984   0.0379
  -8.750  -0.5890   0.05572   0.05008  -0.0636   0.9891   0.0374
  -8.500  -0.5820   0.05030   0.04420  -0.0677   0.9816   0.0371
  -8.250  -0.5713   0.04625   0.03972  -0.0697   0.9741   0.0369
  -8.000  -0.5515   0.04262   0.03563  -0.0721   0.9686   0.0368
  -7.750  -0.5327   0.03974   0.03236  -0.0731   0.9622   0.0369
  -7.500  -0.5084   0.03720   0.02941  -0.0745   0.9565   0.0370
  -7.250  -0.4773   0.03489   0.02673  -0.0767   0.9526   0.0373
  -7.000  -0.4550   0.03321   0.02476  -0.0767   0.9447   0.0379
  -6.750  -0.4236   0.03155   0.02278  -0.0782   0.9397   0.0390
  -6.500  -0.3925   0.03007   0.02097  -0.0794   0.9349   0.0400
  -6.250  -0.3660   0.02884   0.01949  -0.0794   0.9279   0.0406
  -6.000  -0.3329   0.02747   0.01806  -0.0808   0.9238   0.0413
  -5.750  -0.3025   0.02634   0.01689  -0.0816   0.9189   0.0420
  -5.500  -0.2763   0.02540   0.01591  -0.0816   0.9121   0.0429
  -5.250  -0.2435   0.02444   0.01491  -0.0828   0.9083   0.0441
  -5.000  -0.2083   0.02351   0.01391  -0.0843   0.9055   0.0458
  -4.750  -0.1880   0.02292   0.01325  -0.0831   0.8969   0.0474
  -4.500  -0.1565   0.02204   0.01237  -0.0842   0.8926   0.0497
  -4.250  -0.1209   0.02125   0.01153  -0.0860   0.8897   0.0544
  -4.000  -0.0990   0.02066   0.01097  -0.0853   0.8813   0.0606
  -3.750  -0.0666   0.01993   0.01029  -0.0864   0.8767   0.0734
  -3.500  -0.0314   0.01904   0.00963  -0.0882   0.8734   0.1085
  -3.250  -0.0096   0.01831   0.00939  -0.0876   0.8653   0.2015
  -3.000   0.0205   0.01747   0.00911  -0.0886   0.8603   0.3227
  -2.750   0.0523   0.01662   0.00892  -0.0896   0.8569   0.4705
  -2.500   0.0687   0.01651   0.00927  -0.0867   0.8478   0.5671
  -2.250   0.0945   0.01674   0.00974  -0.0847   0.8428   0.6381
  -2.000   0.1186   0.01701   0.00995  -0.0834   0.8346   0.6861
  -1.750   0.1490   0.01719   0.01000  -0.0833   0.8279   0.7169
  -1.500   0.1750   0.01735   0.01006  -0.0825   0.8195   0.7352
  -1.250   0.2035   0.01746   0.01007  -0.0818   0.8121   0.7533
  -1.000   0.2264   0.01760   0.01015  -0.0801   0.8027   0.7707
  -0.750   0.2559   0.01757   0.01003  -0.0796   0.7954   0.7868
  -0.500   0.2756   0.01761   0.01001  -0.0775   0.7843   0.8012
  -0.250   0.3003   0.01751   0.00985  -0.0762   0.7753   0.8152
   0.000   0.3285   0.01732   0.00957  -0.0756   0.7666   0.8275
   0.250   0.3539   0.01712   0.00930  -0.0745   0.7563   0.8361
   0.500   0.3835   0.01698   0.00906  -0.0746   0.7455   0.8433
   0.750   0.4090   0.01684   0.00887  -0.0739   0.7343   0.8482
   1.000   0.4365   0.01673   0.00869  -0.0736   0.7240   0.8537
   1.250   0.4634   0.01668   0.00858  -0.0734   0.7143   0.8599
   1.500   0.4891   0.01659   0.00845  -0.0727   0.7050   0.8654
   1.750   0.5170   0.01653   0.00834  -0.0725   0.6959   0.8726
   2.000   0.5371   0.01649   0.00831  -0.0708   0.6843   0.8799
   2.250   0.5613   0.01647   0.00827  -0.0700   0.6737   0.8873
   2.500   0.5881   0.01643   0.00820  -0.0697   0.6638   0.8924
   2.750   0.6173   0.01640   0.00811  -0.0698   0.6538   0.8963
   3.000   0.6408   0.01645   0.00818  -0.0691   0.6411   0.9010
   3.250   0.6664   0.01650   0.00822  -0.0687   0.6289   0.9053
   3.500   0.6932   0.01653   0.00823  -0.0685   0.6169   0.9084
   3.750   0.7200   0.01660   0.00829  -0.0683   0.6042   0.9111
   4.000   0.7452   0.01670   0.00839  -0.0679   0.5902   0.9145
   4.250   0.7714   0.01680   0.00846  -0.0677   0.5761   0.9179
   4.500   0.7977   0.01691   0.00853  -0.0674   0.5608   0.9209
   4.750   0.8225   0.01706   0.00867  -0.0669   0.5442   0.9238
   5.000   0.8461   0.01724   0.00884  -0.0663   0.5262   0.9273
   5.250   0.8697   0.01744   0.00901  -0.0656   0.5074   0.9311
   5.750   0.9151   0.01792   0.00950  -0.0642   0.4655   0.9419
   6.000   0.9387   0.01820   0.00977  -0.0637   0.4438   0.9488
   6.250   0.9644   0.01853   0.01006  -0.0637   0.4258   0.9578
   6.500   0.9896   0.01885   0.01039  -0.0637   0.4082   0.9944
   6.750   1.0106   0.01931   0.01077  -0.0629   0.3931   1.0000
   7.000   1.0315   0.01981   0.01121  -0.0621   0.3780   1.0000
   7.250   1.0514   0.02034   0.01170  -0.0612   0.3623   1.0000
   7.500   1.0701   0.02087   0.01224  -0.0601   0.3466   1.0000
   7.750   1.0888   0.02141   0.01279  -0.0590   0.3323   1.0000
   8.000   1.1064   0.02199   0.01336  -0.0578   0.3182   1.0000
   8.250   1.1230   0.02262   0.01396  -0.0564   0.3045   1.0000
   8.500   1.1395   0.02326   0.01464  -0.0551   0.2904   1.0000
   8.750   1.1559   0.02391   0.01536  -0.0538   0.2764   1.0000
   9.000   1.1707   0.02464   0.01610  -0.0523   0.2628   1.0000
   9.250   1.1846   0.02544   0.01691  -0.0508   0.2494   1.0000
   9.500   1.1983   0.02626   0.01781  -0.0493   0.2347   1.0000
   9.750   1.2109   0.02713   0.01876  -0.0478   0.2158   1.0000
  10.000   1.2196   0.02822   0.01980  -0.0459   0.1967   1.0000
  10.250   1.2266   0.02947   0.02099  -0.0440   0.1796   1.0000
  10.500   1.2348   0.03076   0.02227  -0.0423   0.1633   1.0000
  10.750   1.2398   0.03229   0.02375  -0.0405   0.1519   1.0000
  11.000   1.2445   0.03393   0.02536  -0.0388   0.1430   1.0000
  11.250   1.2487   0.03567   0.02709  -0.0372   0.1352   1.0000
  11.500   1.2545   0.03737   0.02887  -0.0359   0.1270   1.0000
  11.750   1.2613   0.03905   0.03065  -0.0348   0.1190   1.0000
  12.000   1.2654   0.04097   0.03261  -0.0337   0.1118   1.0000
  12.250   1.2709   0.04284   0.03459  -0.0328   0.1053   1.0000
  12.500   1.2724   0.04510   0.03686  -0.0319   0.1004   1.0000
  12.750   1.2753   0.04734   0.03918  -0.0311   0.0958   1.0000
  13.000   1.2772   0.04974   0.04169  -0.0306   0.0912   1.0000
  13.250   1.2759   0.05251   0.04447  -0.0301   0.0874   1.0000
  13.500   1.2776   0.05511   0.04717  -0.0297   0.0835   1.0000
  13.750   1.2796   0.05777   0.04998  -0.0295   0.0795   1.0000
  14.000   1.2795   0.06070   0.05302  -0.0295   0.0761   1.0000
  14.250   1.2786   0.06376   0.05606  -0.0295   0.0732   1.0000
  14.500   1.2813   0.06663   0.05918  -0.0297   0.0698   1.0000
  14.750   1.2821   0.06976   0.06247  -0.0300   0.0666   1.0000
  15.000   1.2814   0.07312   0.06592  -0.0306   0.0640   1.0000
  15.250   1.2803   0.07655   0.06938  -0.0313   0.0617   1.0000
  15.500   1.2801   0.08014   0.07322  -0.0321   0.0588   1.0000
  15.750   1.2784   0.08393   0.07717  -0.0331   0.0563   1.0000
  16.000   1.2759   0.08789   0.08124  -0.0344   0.0543   1.0000
  16.250   1.2731   0.09192   0.08534  -0.0359   0.0527   1.0000
  16.500   1.2712   0.09602   0.08963  -0.0372   0.0509   1.0000
  16.750   1.2684   0.10030   0.09409  -0.0388   0.0493   1.0000
  17.000   1.2647   0.10480   0.09873  -0.0407   0.0479   1.0000
  17.250   1.2612   0.10929   0.10333  -0.0427   0.0466   1.0000
  17.500   1.2587   0.11363   0.10774  -0.0448   0.0455   1.0000
  17.750   1.2558   0.11807   0.11224  -0.0470   0.0444   1.0000
  18.000   1.2470   0.12391   0.11831  -0.0500   0.0434   1.0000
  18.250   1.2373   0.13002   0.12462  -0.0534   0.0424   1.0000
  18.500   1.2267   0.13643   0.13120  -0.0572   0.0416   1.0000
  18.750   1.2157   0.14308   0.13801  -0.0613   0.0408   1.0000
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