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GOE 377 AIRFOIL (goe377-il)

GOE 377 AIRFOIL - Gottingen 377 airfoil


Airfoil goe377-il
Details Dat file Parser  
(goe377-il) GOE 377 AIRFOIL
Gottingen 377 airfoil
Max thickness 6.5% at 30% chord.
Max camber 3.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 377 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0145700
 0.0250000 0.0226500
 0.0500000 0.0338000
 0.0750000 0.0429500
 0.1000000 0.0496000
 0.1500000 0.0594000
 0.2000000 0.0652000
 0.3000000 0.0703000
 0.4000000 0.0704000
 0.5000000 0.0660000
 0.6000000 0.0586000
 0.7000000 0.0482000
 0.8000000 0.0348000
 0.9000000 0.0184000
 0.9500000 0.0097000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0064200
 0.0250000 -.0073500
 0.0500000 -.0062000
 0.0750000 -.0045500
 0.1000000 -.0029000
 0.1500000 -.0001000
 0.2000000 0.0027000
 0.3000000 0.0058000
 0.4000000 0.0074000
 0.5000000 0.0060000
 0.6000000 0.0036000
 0.7000000 0.0022000
 0.8000000 0.0003000
 0.9000000 -.0011000
 0.9500000 -.0013000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 377 AIRFOIL (goe377-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe377-il50,000937.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe377-il50,000541 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe377-il100,000957.3 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe377-il100,000558.1 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe377-il200,000977.9 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe377-il200,000573.9 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe377-il500,0009101.5 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe377-il500,000591.7 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe377-il1,000,0009115.8 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe377-il1,000,0005105.2 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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