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GOE 692 AIRFOIL (goe692-il)

GOE 692 AIRFOIL - Gottingen 692 airfoil


Airfoil goe692-il
Details Dat file Parser  
(goe692-il) GOE 692 AIRFOIL
Gottingen 692 airfoil
Max thickness 16.1% at 30% chord.
Max camber 5% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 692 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0280900
 0.0250000 0.0416900
 0.0500000 0.0613700
 0.0750000 0.0760600
 0.1000000 0.0867500
 0.1500000 0.1031300
 0.2000000 0.1145000
 0.3000000 0.1277500
 0.4000000 0.1305000
 0.5000000 0.1247500
 0.6000000 0.1110000
 0.7000000 0.0917500
 0.8000000 0.0665000
 0.9000000 0.0382500
 0.9500000 0.0226300
 1.0000000 0.0050000

 0.0000000 0.0000000
 0.0125000 -.0204100
 0.0250000 -.0273100
 0.0500000 -.0346300
 0.0750000 -.0379400
 0.1000000 -.0397500
 0.1500000 -.0398700
 0.2000000 -.0380000
 0.3000000 -.0332500
 0.4000000 -.0285000
 0.5000000 -.0237500
 0.6000000 -.0190000
 0.7000000 -.0142500
 0.8000000 -.0095000
 0.9000000 -.0047500
 0.9500000 -.0023700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 692 AIRFOIL (goe692-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe692-il50,00097.3 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe692-il50,000519 at α=10.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe692-il100,000948.1 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe692-il100,000549.6 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe692-il200,000976.1 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe692-il200,000573.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe692-il500,0009109 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe692-il500,000599.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe692-il1,000,0009132.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe692-il1,000,0005114.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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