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GOE 497 AIRFOIL (goe497-il)

GOE 497 AIRFOIL - Gottingen 497 airfoil


Airfoil goe497-il
Details Dat file Parser  
(goe497-il) GOE 497 AIRFOIL
Gottingen 497 airfoil
Max thickness 12.7% at 30% chord.
Max camber 5.3% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 497 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0249600
 0.0250000 0.0364200
 0.0500000 0.0518500
 0.0750000 0.0632700
 0.1000000 0.0727000
 0.1500000 0.0875500
 0.2000000 0.0969000
 0.3000000 0.1081000
 0.4000000 0.1088000
 0.5000000 0.1040000
 0.6000000 0.0922000
 0.7000000 0.0754000
 0.8000000 0.0536000
 0.9000000 0.0283000
 0.9500000 0.0145500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0155400
 0.0250000 -.0215800
 0.0500000 -.0276500
 0.0750000 -.0307200
 0.1000000 -.0318000
 0.1500000 -.0314500
 0.2000000 -.0286000
 0.3000000 -.0189000
 0.4000000 -.0077000
 0.5000000 0.0025000
 0.6000000 0.0092000
 0.7000000 0.0124000
 0.8000000 0.0126000
 0.9000000 0.0088000
 0.9500000 0.0051500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 497 AIRFOIL (goe497-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe497-il50,000928.4 at α=11.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe497-il50,000534.8 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe497-il100,000958.6 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe497-il100,000560.5 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe497-il200,000985 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe497-il200,000582 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe497-il500,0009118 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe497-il500,0005105.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe497-il1,000,0009135.2 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe497-il1,000,0005114.2 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
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