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GOE 498 AIRFOIL (goe498-il)

GOE 498 AIRFOIL - Gottingen 498 airfoil


Airfoil goe498-il
Details Dat file Parser  
(goe498-il) GOE 498 AIRFOIL
Gottingen 498 airfoil
Max thickness 15.9% at 29.4% chord.
Max camber 5.5% at 49.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 498 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0106900 0.0365300
 0.0225900 0.0486200
 0.0467400 0.0658100
 0.0710900 0.0790200
 0.0955300 0.0902300
 0.1448000 0.1051700
 0.1942300 0.1166100
 0.2936900 0.1275400
 0.3936700 0.1279900
 0.4940600 0.1199600
 0.5947800 0.1054400
 0.6957700 0.0854400
 0.7969300 0.0619500
 0.8983700 0.0329700
 0.9491300 0.0174800
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0134100 -.0183400
 0.0262700 -.0257000
 0.0516600 -.0334400
 0.0768400 -.0372000
 0.1019800 -.0399500
 0.1520300 -.0409700
 0.2019600 -.0395000
 0.3015400 -.0310700
 0.4010000 -.0201500
 0.5004600 -.0092300
 0.5999700 0.0007000
 0.6996700 0.0066300
 0.7995800 0.0085800
 0.8996800 0.0065300
 0.9498000 0.0041100
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 498 AIRFOIL (goe498-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe498-il50,00097.3 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe498-il50,000524.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe498-il100,000949.7 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe498-il100,000553.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe498-il200,000975.9 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe498-il200,000573.5 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe498-il500,0009105.8 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe498-il500,000591.5 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe498-il1,000,0009123.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe498-il1,000,0005102.3 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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