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GOE 477 AIRFOIL (goe477-il)

GOE 477 AIRFOIL - Gottingen 477 airfoil


Airfoil goe477-il
Details Dat file Parser  
(goe477-il) GOE 477 AIRFOIL
Gottingen 477 airfoil
Max thickness 10.1% at 30% chord.
Max camber 4.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 477 AIRFOIL
       13.       13.

 0.0000000 0.0000000
 0.0250000 0.0289100
 0.0500000 0.0443200
 0.1000000 0.0681500
 0.2000000 0.0898000
 0.3000000 0.0969500
 0.4000000 0.0975000
 0.5000000 0.0942500
 0.6000000 0.0849000
 0.7000000 0.0690500
 0.8000000 0.0457000
 0.9000000 0.0233500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0130900
 0.0500000 -.0151800
 0.1000000 -.0143500
 0.2000000 -.0087000
 0.3000000 -.0035500
 0.4000000 0.0001000
 0.5000000 0.0022500
 0.6000000 0.0034000
 0.7000000 0.0030500
 0.8000000 0.0022000
 0.9000000 0.0013500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 477 AIRFOIL (goe477-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe477-il50,000934.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe477-il50,000536.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe477-il100,000956.7 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe477-il100,000554.7 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe477-il200,000980.5 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe477-il200,000575 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe477-il500,0009111.3 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   goe477-il500,000587.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe477-il1,000,0009121.7 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe477-il1,000,0005104.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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