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GOE 654 AIRFOIL (goe654-il)

GOE 654 AIRFOIL - Gottingen 654 airfoil


Airfoil goe654-il
Details Dat file Parser  
(goe654-il) GOE 654 AIRFOIL
Gottingen 654 airfoil
Max thickness 14.5% at 30% chord.
Max camber 5.2% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 654 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0263800
 0.0250000 0.0412500
 0.0500000 0.0635000
 0.0750000 0.0797500
 0.1000000 0.0915000
 0.1500000 0.1080000
 0.2000000 0.1180000
 0.3000000 0.1240000
 0.4000000 0.1200000
 0.5000000 0.1070000
 0.6000000 0.0905000
 0.7000000 0.0705000
 0.8000000 0.0485000
 0.9000000 0.0255000
 0.9500000 0.0135000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0151300
 0.0250000 -.0182500
 0.0500000 -.0215000
 0.0750000 -.0232500
 0.1000000 -.0240000
 0.1500000 -.0245000
 0.2000000 -.0235000
 0.3000000 -.0210000
 0.4000000 -.0160000
 0.5000000 -.0110000
 0.6000000 -.0065000
 0.7000000 -.0035000
 0.8000000 -.0015000
 0.9000000 -.0005000
 0.9500000 0.0000000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 654 AIRFOIL (goe654-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe654-il50,000910 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe654-il50,000528.4 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe654-il100,000941 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe654-il100,000550 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe654-il200,000967.3 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe654-il200,000567.8 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe654-il500,000994.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe654-il500,000592.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe654-il1,000,0009118.6 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe654-il1,000,0005115.3 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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