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GOE 379 AIRFOIL (goe379-il)

GOE 379 AIRFOIL - Gottingen 379 airfoil


Airfoil goe379-il
Details Dat file Parser  
(goe379-il) GOE 379 AIRFOIL
Gottingen 379 airfoil
Max thickness 6.5% at 30% chord.
Max camber 5.2% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 379 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124500 0.0150400
 0.0249200 0.0240900
 0.0498700 0.0381700
 0.0748300 0.0487600
 0.0998000 0.0578500
 0.1497500 0.0700200
 0.1997300 0.0782000
 0.2997000 0.0845500
 0.3997100 0.0834000
 0.4997300 0.0767500
 0.5997700 0.0666000
 0.6998100 0.0529500
 0.7998700 0.0368000
 0.8999299 0.0191500
 0.9499700 0.0098200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125100 -.0039600
 0.0250200 -.0044100
 0.0500100 -.0018200
 0.0749900 0.0017600
 0.0999800 0.0053500
 0.1499600 0.0110200
 0.1999400 0.0157000
 0.2999300 0.0200500
 0.3999300 0.0214000
 0.4999300 0.0192500
 0.5999500 0.0151000
 0.6999600 0.0104500
 0.7999800 0.0048000
 0.9000000 0.0001500
 0.9500000 -.0011700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 379 AIRFOIL (goe379-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe379-il50,000939.6 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe379-il50,000541 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe379-il100,000958.2 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe379-il100,000560.3 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe379-il200,000977.7 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe379-il200,000579.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe379-il500,0009106 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe379-il500,0005103.8 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe379-il1,000,0009126.3 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe379-il1,000,0005121.5 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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