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Dayton-Wright 6 (daytonwright6-il)

Dayton-Wright 6 - Dayton-Wright 6 airfoil


Airfoil daytonwright6-il
Details Dat file Parser  
(daytonwright6-il) Dayton-Wright 6
Dayton-Wright 6 airfoil
Max thickness 13.6% at 30% chord.
Max camber 4.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
Dayton-Wright 6
1.0000     0.0057
0.9500     0.0230
0.9000     0.0377
0.8000     0.0637
0.7000     0.0882
0.6000     0.1075
0.5000     0.1230
0.4000     0.1350
0.3000     0.1397
0.2000     0.1340
0.1500     0.1245
0.1000     0.1088
0.0750     0.0978
0.0500     0.0838
0.0250     0.0647
0.0125     0.0522
0.0000     0.0308
0.0125     0.0127
0.0250     0.0083
0.0500     0.0033
0.0750     0.0013
0.1000     0.0005
0.1500     0.0007
0.2000     0.0017
0.3000     0.0037
0.4000     0.0045
0.5000     0.0030
0.6000     0.0015
0.7000     0.0003
0.8000     0.0003
0.9000     0.0012
0.9500     0.0020
1.0000     0.0057
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Selig format dat file

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Polars for Dayton-Wright 6 (daytonwright6-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   daytonwright6-il50,000911 at α=1°Mach=0 Ncrit=9Xfoil predictionDetails
   daytonwright6-il50,000531.1 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   daytonwright6-il100,000945.6 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   daytonwright6-il100,000549.7 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   daytonwright6-il200,000966.8 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   daytonwright6-il200,000566.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   daytonwright6-il500,000992.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   daytonwright6-il500,000589.6 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   daytonwright6-il1,000,0009115.8 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   daytonwright6-il1,000,0005111.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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