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GOE 289 (MVA 289) AIRFOIL (goe289-il)

GOE 289 (MVA 289) AIRFOIL - Gottingen 289 (MVA 289) airfoil


Airfoil goe289-il
Details Dat file Parser  
(goe289-il) GOE 289 (MVA 289) AIRFOIL
Gottingen 289 (MVA 289) airfoil
Max thickness 16.8% at 30% chord.
Max camber 6.1% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 289 (MVA 289) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0260100
 0.0250000 0.0390100
 0.0500000 0.0605200
 0.0750000 0.0770400
 0.1000000 0.0915500
 0.1500000 0.1140800
 0.2000000 0.1291000
 0.3000000 0.1416500
 0.4000000 0.1402000
 0.5000000 0.1292500
 0.6000000 0.1118000
 0.7000000 0.0888500
 0.8000000 0.0629000
 0.9000000 0.0329500
 0.9500000 0.0174700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0194900
 0.0250000 -.0244900
 0.0500000 -.0304700
 0.0750000 -.0334600
 0.1000000 -.0344500
 0.1500000 -.0339200
 0.2000000 -.0324000
 0.3000000 -.0263500
 0.4000000 -.0178000
 0.5000000 -.0117500
 0.6000000 -.0067000
 0.7000000 -.0026500
 0.8000000 -.0006000
 0.9000000 -.0000500
 0.9500000 -.0005200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 289 (MVA 289) AIRFOIL (goe289-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe289-il50,00094.3 at α=11.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe289-il50,000520.7 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe289-il100,000938.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe289-il100,000546.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe289-il200,000965.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe289-il200,000564.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe289-il500,000992.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe289-il500,000587.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe289-il1,000,0009115.9 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe289-il1,000,0005109.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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