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GOE 775 AIRFOIL (goe775-il)

GOE 775 AIRFOIL - Gottingen 775 airfoil


Airfoil goe775-il
Details Dat file Parser  
(goe775-il) GOE 775 AIRFOIL
Gottingen 775 airfoil
Max thickness 21% at 30% chord.
Max camber 0% at 1.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 775 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0332300
 0.0250000 0.0458500
 0.0500000 0.0623100
 0.0750000 0.0736600
 0.1000000 0.0820200
 0.1500000 0.0938300
 0.2000000 0.1007400
 0.3000000 0.1056600
 0.4000000 0.1023800
 0.5000000 0.0938000
 0.6000000 0.0811200
 0.7000000 0.0657400
 0.8000000 0.0483600
 0.9000000 0.0272800
 0.9500000 0.0162900
 1.0000000 0.0044000

 0.0000000 0.0000000
 0.0125000 -.0331700
 0.0250000 -.0457500
 0.0500000 -.0620900
 0.0750000 -.0733300
 0.1000000 -.0815800
 0.1500000 -.0931700
 0.2000000 -.0998600
 0.3000000 -.1043400
 0.4000000 -.1006200
 0.5000000 -.0916000
 0.6000000 -.0784800
 0.7000000 -.0626600
 0.8000000 -.0448400
 0.9000000 -.0233200
 0.9500000 -.0121100
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 775 AIRFOIL (goe775-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe775-il50,000918.9 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe775-il50,000525.1 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe775-il100,000936.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe775-il100,000535.8 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe775-il200,000948.4 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe775-il200,000543.4 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe775-il500,000960.3 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe775-il500,000556.6 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe775-il1,000,000974.6 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe775-il1,000,000569.8 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
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