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GOE 704 AIRFOIL (goe704-il)

GOE 704 AIRFOIL - Gottingen 704 airfoil


Airfoil goe704-il
Details Dat file Parser  
(goe704-il) GOE 704 AIRFOIL
Gottingen 704 airfoil
Max thickness 12.9% at 29.9% chord.
Max camber 2.1% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 704 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0121600 0.0197100
 0.0244800 0.0299200
 0.0492300 0.0448500
 0.0740600 0.0547800
 0.0989100 0.0632100
 0.1487200 0.0740700
 0.1986100 0.0804300
 0.2985200 0.0856500
 0.3985400 0.0848700
 0.4986400 0.0791000
 0.5988300 0.0678300
 0.6991000 0.0520600
 0.7993900 0.0352900
 0.8996800 0.0185200
 0.9498200 0.0103800
 1.0000000 0.0027500

 0.0000000 0.0000000
 0.0127700 -.0157800
 0.0254000 -.0230600
 0.0505500 -.0321300
 0.0756500 -.0377000
 0.1007000 -.0407600
 0.1507500 -.0434000
 0.2007700 -.0445400
 0.3007600 -.0438100
 0.4007300 -.0420900
 0.5007000 -.0403600
 0.6006700 -.0386400
 0.7006300 -.0364100
 0.8005300 -.0306900
 0.9003299 -.0189700
 0.9501899 -.0111100
 1.0000000 -.0027500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 704 AIRFOIL (goe704-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe704-il50,000926 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe704-il50,000531.6 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe704-il100,000944.9 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe704-il100,000544.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe704-il200,000957.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe704-il200,000557.5 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe704-il500,000978.5 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe704-il500,000572.7 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe704-il1,000,000990.1 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe704-il1,000,000583 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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