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GOE 389 AIRFOIL (goe389-il)

GOE 389 AIRFOIL - Gottingen 389 airfoil


Airfoil goe389-il
Details Dat file Parser  
(goe389-il) GOE 389 AIRFOIL
Gottingen 389 airfoil
Max thickness 10.3% at 29.8% chord.
Max camber 4% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 389 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0121500 0.0171400
 0.0244400 0.0279900
 0.0491500 0.0421900
 0.0739300 0.0532900
 0.0987700 0.0611900
 0.1485000 0.0743900
 0.1983200 0.0833000
 0.2981700 0.0906100
 0.3982200 0.0884200
 0.4983900 0.0821700
 0.5985400 0.0723600
 0.6988400 0.0574800
 0.7991600 0.0415000
 0.8995500 0.0223300
 0.9497400 0.0127400
 1.0000000 0.0010500

 0.0000000 0.0000000
 0.0127500 -.0124400
 0.0253100 -.0153900
 0.0503600 -.0179900
 0.0753700 -.0185800
 0.1003900 -.0191800
 0.1503700 -.0186700
 0.2003500 -.0171600
 0.3002500 -.0125500
 0.4001800 -.0089400
 0.5001200 -.0058200
 0.6000600 -.0028100
 0.7000400 -.0017900
 0.8000300 -.0013800
 0.9000200 -.0009600
 0.9500200 -.0009600
 1.0000000 -.0010500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 389 AIRFOIL (goe389-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe389-il50,000932.7 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe389-il50,000537.6 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe389-il100,000955 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe389-il100,000556.2 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe389-il200,000975.1 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe389-il200,000573.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe389-il500,0009101.4 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe389-il500,000594.6 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe389-il1,000,0009119.7 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe389-il1,000,0005108.1 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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