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GOE 796 AIRFOIL (goe796-il)

GOE 796 AIRFOIL - Gottingen 796 airfoil


Airfoil goe796-il
Details Dat file Parser  
(goe796-il) GOE 796 AIRFOIL
Gottingen 796 airfoil
Max thickness 12% at 30% chord.
Max camber 3.6% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 796 AIRFOIL
       21.       21.

 0.0000000 0.0000000
 0.0020000 0.0075700
 0.0040000 0.0109400
 0.0060000 0.0135000
 0.0080000 0.0160700
 0.0125000 0.0206300
 0.0250000 0.0308500
 0.0500000 0.0452000
 0.0750000 0.0557500
 0.1000000 0.0642000
 0.1500000 0.0763000
 0.2000000 0.0856000
 0.3000000 0.0942000
 0.4000000 0.0961000
 0.5000000 0.0920000
 0.6000000 0.0816000
 0.7000000 0.0666000
 0.8000000 0.0490000
 0.9000000 0.0276000
 0.9500000 0.0158000
 1.0000000 0.0040000

 0.0000000 0.0000000
 0.0020000 -.0059300
 0.0040000 -.0093600
 0.0060000 -.0118000
 0.0080000 -.0135300
 0.0125000 -.0160700
 0.0250000 -.0216500
 0.0500000 -.0271000
 0.0750000 -.0298500
 0.1000000 -.0304000
 0.1500000 -.0303000
 0.2000000 -.0292000
 0.3000000 -.0258000
 0.4000000 -.0224000
 0.5000000 -.0190000
 0.6000000 -.0156000
 0.7000000 -.0122000
 0.8000000 -.0088000
 0.9000000 -.0054000
 0.9500000 -.0029000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 796 AIRFOIL (goe796-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe796-il50,000932.2 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe796-il50,000535.5 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe796-il100,000955.5 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe796-il100,000555.6 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe796-il200,000978 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe796-il200,000573.2 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe796-il500,0009105.9 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe796-il500,000590.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe796-il1,000,0009122.7 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe796-il1,000,0005105.2 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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