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GOE 178 AIRFOIL (goe178-il)

GOE 178 AIRFOIL - Gottingen 178 airfoil


Airfoil goe178-il
Details Dat file Parser  
(goe178-il) GOE 178 AIRFOIL
Gottingen 178 airfoil
Max thickness 8.5% 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 178 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0161900
 0.0250000 0.0253700
 0.0500000 0.0377500
 0.0750000 0.0491200
 0.1000000 0.0585000
 0.1500000 0.0722500
 0.2000000 0.0800000
 0.3000000 0.0865000
 0.4000000 0.0820000
 0.5000000 0.0735000
 0.6000000 0.0630000
 0.7000000 0.0505000
 0.8000000 0.0360000
 0.9000000 0.0205000
 0.9500000 0.0112500
 1.0000000 0.0030000

 0.0000000 0.0000000
 0.0125000 -.0108100
 0.0250000 -.0126300
 0.0500000 -.0142500
 0.0750000 -.0128800
 0.1000000 -.0110000
 0.1500000 -.0077500
 0.2000000 -.0040000
 0.3000000 0.0015000
 0.4000000 0.0060000
 0.5000000 0.0085000
 0.6000000 0.0090000
 0.7000000 0.0085000
 0.8000000 0.0070000
 0.9000000 0.0045000
 0.9500000 0.0022500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 178 AIRFOIL (goe178-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe178-il50,000937.8 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe178-il50,000538.9 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe178-il100,000958.1 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe178-il100,000558.6 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe178-il200,000978.1 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe178-il200,000576.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe178-il500,0009104.5 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe178-il500,000598.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe178-il1,000,0009123 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe178-il1,000,0005110.5 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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