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AH-6-40-7 AIRFOIL (ah6407-il)

AH-6-40-7 AIRFOIL - Althaus AH 6-407 airfoil


Airfoil ah6407-il
Details Dat file Parser  
(ah6407-il) AH-6-40-7 AIRFOIL
Althaus AH 6-407 airfoil
Max thickness 6.9% at 20% chord.
Max camber 5.5% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
AH-6-40-7 AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0124200 0.0180600
 0.0248800 0.0271100
 0.0498200 0.0402200
 0.0747700 0.0503400
 0.0997400 0.0584500
 0.1496800 0.0706700
 0.1996500 0.0779000
 0.2996200 0.0843500
 0.3996200 0.0848000
 0.4996300 0.0812500
 0.5996700 0.0737000
 0.6997200 0.0621500
 0.7997900 0.0466000
 0.8998800 0.0270500
 1.0000000 0.0035000

 0.0000000 0.0000000
 0.0125300 -.0069400
 0.0250400 -.0078900
 0.0500300 -.0067700
 0.0750200 -.0051600
 0.1000100 -.0025500
 0.1499900 0.0031700
 0.1999600 0.0094000
 0.2999100 0.0193500
 0.3998800 0.0258000
 0.4998700 0.0282500
 0.5998700 0.0287000
 0.6998900 0.0251500
 0.7999200 0.0186000
 0.8999600 0.0090500
 1.0000000 -.0035000
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Lednicer format dat file
Selig format dat file

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Polars for AH-6-40-7 AIRFOIL (ah6407-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ah6407-il50,000941.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah6407-il50,000546.9 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ah6407-il100,000967.1 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ah6407-il100,000567.1 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ah6407-il200,000991.5 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   ah6407-il200,000585.6 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ah6407-il500,0009119.7 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ah6407-il500,0005104 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ah6407-il1,000,0009131.3 at α=1.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah6407-il1,000,0005121.8 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
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