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GOE 5K AIRFOIL (goe05k-il)

GOE 5K AIRFOIL - Gottingen 5K airfoil


Airfoil goe05k-il
Details Dat file Parser  
(goe05k-il) GOE 5K AIRFOIL
Gottingen 5K airfoil
Max thickness 3.7% at 50% chord.
Max camber 1.5% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 5K AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0250000 0.0078100
 0.0500000 0.0116100
 0.0750000 0.0146200
 0.1000000 0.0173300
 0.1500000 0.0216400
 0.2000000 0.0249600
 0.3000000 0.0299900
 0.4000000 0.0329200
 0.5000000 0.0338500
 0.6000000 0.0329800
 0.7000000 0.0294100
 0.8000000 0.0231400
 0.9000000 0.0138700
 0.9500000 0.0080800
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0034900
 0.0500000 -.0038900
 0.0750000 -.0041800
 0.1000000 -.0042700
 0.1500000 -.0045600
 0.2000000 -.0044400
 0.3000000 -.0040100
 0.4000000 -.0035800
 0.5000000 -.0031500
 0.6000000 -.0027200
 0.7000000 -.0022900
 0.8000000 -.0018600
 0.9000000 -.0014300
 0.9500000 -.0012200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 5K AIRFOIL (goe05k-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe05k-il50,000920.5 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe05k-il50,000521.2 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe05k-il100,000925.6 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe05k-il100,000527.6 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe05k-il200,000933.4 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe05k-il200,000539.8 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe05k-il500,000971.3 at α=1.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe05k-il500,000582.4 at α=1.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe05k-il1,000,000995.1 at α=0.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe05k-il1,000,000595.1 at α=0.75°Mach=0 Ncrit=5Xfoil predictionDetails
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