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DU 86-137/25 AIRFOIL (du861372-il)

DU 86-137/25 AIRFOIL - Delft University DU 86-137/25 Airfoil


Airfoil du861372-il
Details Dat file Parser  
(du861372-il) DU 86-137/25 AIRFOIL
Delft University DU 86-137/25 Airfoil
Max thickness 13.6% at 41.6% chord.
Max camber 0.3% at 1.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
DU 86-137/25 AIRFOIL
      24.0      17.0
 
 0.0000000 0.0000000
 0.0013248 0.0050461
 0.0044717 0.0094186
 0.0095787 0.0138426
 0.0164958 0.0183179
 0.0251730 0.0227745
 0.0476677 0.0314815
 0.0766932 0.0397133
 0.1117794 0.0472594
 0.1524067 0.0538597
 0.1980050 0.0593335
 0.2979470 0.0635972
 0.3014651 0.0664599
 0.3577769 0.0679714
 0.4159799 0.0680342
 0.4455118 0.0674958
 0.5048665 0.0652194
 0.5929860 0.0585138
 0.6500642 0.0514254
 0.7050142 0.0415553
 0.7622559 0.0296667
 0.8168343 0.0220965
 0.9074373 0.0107725
 1.0000000 0.0000000
 
 0.0000000 0.0000000
 0.0028942 -.0076934
 0.0075974 -.0116402
 0.0143074 -.0112452
 0.0451316 -.0284035
 0.0740791 -.0365126
 0.1029262 -.0441418
 0.1499337 -.0511076
 0.2453367 -.0620680
 0.2985821 -.0656890
 0.3545166 -.0678380
 0.4123400 -.0684256
 0.6177524 -.0571940
 0.7016879 -.0452816
 0.8077582 -.0247126
 0.9012113 -.0086931
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for DU 86-137/25 AIRFOIL (du861372-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   du861372-il50,000928.9 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   du861372-il50,000523.8 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   du861372-il100,000933.4 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   du861372-il100,000527.1 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   du861372-il200,000932.8 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   du861372-il200,000535.5 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   du861372-il500,000946.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   du861372-il500,000548.9 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   du861372-il1,000,000958.4 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   du861372-il1,000,000559.9 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
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