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GOE 11K AIRFOIL (goe11k-il)

GOE 11K AIRFOIL - Gottingen 11K airfoil


Airfoil goe11k-il
Details Dat file Parser  
(goe11k-il) GOE 11K AIRFOIL
Gottingen 11K airfoil
Max thickness 7.5% at 50% chord.
Max camber 2.7% at 60% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 11K AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0250000 0.0192800
 0.0500000 0.0269500
 0.1000000 0.0372100
 0.1500000 0.0447700
 0.2000000 0.0507200
 0.3000000 0.0588300
 0.4000000 0.0625400
 0.5000000 0.0644500
 0.6000000 0.0633600
 0.7000000 0.0568700
 0.8000000 0.0449800
 0.9000000 0.0272900
 0.9500000 0.0161500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0129200
 0.0500000 -.0152500
 0.1000000 -.0160900
 0.1500000 -.0153300
 0.2000000 -.0145800
 0.3000000 -.0130700
 0.4000000 -.0115600
 0.5000000 -.0100500
 0.6000000 -.0085400
 0.7000000 -.0070300
 0.8000000 -.0055200
 0.9000000 -.0040100
 0.9500000 -.0032600
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 11K AIRFOIL (goe11k-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe11k-il50,000928.2 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe11k-il50,000531.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe11k-il100,000941.9 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe11k-il100,000549 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe11k-il200,000972.4 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe11k-il200,000572.9 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe11k-il500,0009109.5 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe11k-il500,000599.4 at α=1.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe11k-il1,000,0009122.4 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe11k-il1,000,000587.1 at α=1.25°Mach=0 Ncrit=5Xfoil predictionDetails
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