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GOE 801 (MVA 301) AIRFOIL (goe801-il)

GOE 801 (MVA 301) AIRFOIL - Gottingen 801 (MVA 301) airfoil


Airfoil goe801-il
Details Dat file Parser  
(goe801-il) GOE 801 (MVA 301) AIRFOIL
Gottingen 801 (MVA 301) airfoil
Max thickness 9.8% 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 801 (MVA 301) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0261500
 0.0250000 0.0398000
 0.0500000 0.0566000
 0.0750000 0.0689000
 0.1000000 0.0782000
 0.1500000 0.0918000
 0.2000000 0.1014000
 0.3000000 0.1096000
 0.4000000 0.1088000
 0.5000000 0.1015000
 0.6000000 0.0897000
 0.7000000 0.0734000
 0.8000000 0.0526000
 0.9000000 0.0288000
 0.9500000 0.0164000
 1.0000000 0.0040000

 0.0000000 0.0000000
 0.0125000 -.0118500
 0.0250000 -.0117000
 0.0500000 -.0094000
 0.0750000 -.0071000
 0.1000000 -.0048000
 0.1500000 -.0002000
 0.2000000 0.0044000
 0.3000000 0.0116000
 0.4000000 0.0148000
 0.5000000 0.0150000
 0.6000000 0.0147000
 0.7000000 0.0124000
 0.8000000 0.0086000
 0.9000000 0.0038000
 0.9500000 0.0019000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 801 (MVA 301) AIRFOIL (goe801-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe801-il50,000917.9 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe801-il50,000538.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe801-il100,000955.9 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe801-il100,000560.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe801-il200,000979.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe801-il200,000579.6 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe801-il500,0009110.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe801-il500,0005104.1 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe801-il1,000,0009132 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe801-il1,000,0005123 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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