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GOE 673 AIRFOIL (goe673-il)

GOE 673 AIRFOIL - Gottingen 673 airfoil


Airfoil goe673-il
Details Dat file Parser  
(goe673-il) GOE 673 AIRFOIL
Gottingen 673 airfoil
Max thickness 10.8% at 29.7% chord.
Max camber 2.8% at 49.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 673 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0119700 0.0129800
 0.0241900 0.0199800
 0.0487500 0.0309700
 0.0733800 0.0399700
 0.0980600 0.0479700
 0.1475500 0.0604800
 0.1972100 0.0689900
 0.2968200 0.0785200
 0.3967400 0.0805700
 0.4968800 0.0771200
 0.5972000 0.0691900
 0.6976600 0.0577600
 0.7982900 0.0423300
 0.8990500 0.0234100
 0.9494800 0.0129500
 1.0000000 0.0020000

 0.0000000 0.0000000
 0.0128400 -.0084800
 0.0255100 -.0124700
 0.0507500 -.0184400
 0.0759100 -.0224300
 0.1010300 -.0254100
 0.1511500 -.0283800
 0.2012100 -.0298500
 0.3011900 -.0293000
 0.4010600 -.0262600
 0.5008800 -.0217100
 0.6007000 -.0171700
 0.7004700 -.0116300
 0.8002900 -.0070900
 0.9001600 -.0040400
 0.9501000 -.0025200
 1.0000000 -.0020000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 673 AIRFOIL (goe673-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe673-il50,000938.1 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe673-il50,000537.5 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe673-il100,000956 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe673-il100,000555.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe673-il200,000975 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe673-il200,000573.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe673-il500,0009100.6 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe673-il500,000594.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe673-il1,000,0009118.4 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe673-il1,000,0005109.5 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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