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GOE 693 AIRFOIL (goe693-il)

GOE 693 AIRFOIL - Gottingen 693 airfoil


Airfoil goe693-il
Details Dat file Parser  
(goe693-il) GOE 693 AIRFOIL
Gottingen 693 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 693 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0204300
 0.0250000 0.0303600
 0.0500000 0.0452300
 0.0750000 0.0555900
 0.1000000 0.0644500
 0.1500000 0.0761700
 0.2000000 0.0855000
 0.3000000 0.0943500
 0.4000000 0.0963000
 0.5000000 0.0922500
 0.6000000 0.0817000
 0.7000000 0.0666500
 0.8000000 0.0491000
 0.9000000 0.0285500
 0.9500000 0.0167800
 1.0000000 0.0050000

 0.0000000 0.0000000
 0.0125000 -.0160700
 0.0250000 -.0216400
 0.0500000 -.0272700
 0.0750000 -.0299100
 0.1000000 -.0305500
 0.1500000 -.0303300
 0.2000000 -.0291000
 0.3000000 -.0256500
 0.4000000 -.0222000
 0.5000000 -.0187500
 0.6000000 -.0153000
 0.7000000 -.0118500
 0.8000000 -.0084000
 0.9000000 -.0049500
 0.9500000 -.0027300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 693 AIRFOIL (goe693-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe693-il50,000932.3 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe693-il50,000535.6 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe693-il100,000956 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe693-il100,000555.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe693-il200,000978.2 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe693-il200,000572.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe693-il500,0009103.2 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe693-il500,000587.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe693-il1,000,0009115.5 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe693-il1,000,000597.3 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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