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GOE 499 AIRFOIL (goe499-il)

GOE 499 AIRFOIL - Gottingen 499 airfoil


Airfoil goe499-il
Details Dat file Parser  
(goe499-il) GOE 499 AIRFOIL
Gottingen 499 airfoil
Max thickness 6.8% at 30% chord.
Max camber 5.9% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 499 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0121600
 0.0250000 0.0193100
 0.0500000 0.0311200
 0.0750000 0.0404400
 0.1000000 0.0477500
 0.1500000 0.0613700
 0.2000000 0.0710000
 0.3000000 0.0837500
 0.4000000 0.0870000
 0.5000000 0.0852500
 0.6000000 0.0795000
 0.7000000 0.0677500
 0.8000000 0.0495000
 0.9000000 0.0267500
 0.9500000 0.0138800
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0103400
 0.0250000 -.0116900
 0.0500000 -.0118800
 0.0750000 -.0110600
 0.1000000 -.0087500
 0.1500000 -.0031300
 0.2000000 0.0035000
 0.3000000 0.0157500
 0.4000000 0.0245000
 0.5000000 0.0317500
 0.6000000 0.0355000
 0.7000000 0.0342500
 0.8000000 0.0275000
 0.9000000 0.0157500
 0.9500000 0.0083700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 499 AIRFOIL (goe499-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe499-il50,000938.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe499-il50,000544.9 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe499-il100,000971.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe499-il100,000569.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe499-il200,0009102.2 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe499-il200,000599.1 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe499-il500,0009149.4 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe499-il500,0005118.3 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe499-il1,000,0009157.8 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe499-il1,000,0005111.9 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
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