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GOE 735 AIRFOIL (goe735-il)

GOE 735 AIRFOIL - Gottingen 735 airfoil


Airfoil goe735-il
Details Dat file Parser  
(goe735-il) GOE 735 AIRFOIL
Gottingen 735 airfoil
Max thickness 20.1% at 30% chord.
Max camber 4.4% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 735 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0357200
 0.0250000 0.0524400
 0.0500000 0.0763700
 0.0750000 0.0938100
 0.1000000 0.1077500
 0.1500000 0.1271200
 0.2000000 0.1387000
 0.3000000 0.1442500
 0.4000000 0.1345000
 0.5000000 0.1162500
 0.6000000 0.0930000
 0.7000000 0.0657500
 0.8000000 0.0388000
 0.9000000 0.0157500
 0.9500000 0.0064200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0212800
 0.0250000 -.0305600
 0.0500000 -.0419300
 0.0750000 -.0481900
 0.1000000 -.0517500
 0.1500000 -.0553700
 0.2000000 -.0570000
 0.3000000 -.0567500
 0.4000000 -.0540000
 0.5000000 -.0502500
 0.6000000 -.0445000
 0.7000000 -.0375500
 0.8000000 -.0282000
 0.9000000 -.0162500
 0.9500000 -.0088700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 735 AIRFOIL (goe735-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe735-il50,00092.9 at α=13°Mach=0 Ncrit=9Xfoil predictionDetails
   goe735-il50,000516.4 at α=0.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe735-il100,000923.4 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe735-il100,000535.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe735-il200,000949.6 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe735-il200,000555.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe735-il500,000982.2 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe735-il500,000578.9 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe735-il1,000,0009105 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe735-il1,000,000597.3 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
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