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GOE 398 AIRFOIL (goe398-il)

GOE 398 AIRFOIL - Gottingen 398 airfoil


Airfoil goe398-il
Details Dat file Parser  
(goe398-il) GOE 398 AIRFOIL
Gottingen 398 airfoil
Max thickness 13.9% at 30% chord.
Max camber 4.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 398 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0343500
 0.0250000 0.0457000
 0.0500000 0.0619000
 0.0750000 0.0751000
 0.1000000 0.0858000
 0.1500000 0.1002000
 0.2000000 0.1091000
 0.3000000 0.1169000
 0.4000000 0.1147000
 0.5000000 0.1070000
 0.6000000 0.0928000
 0.7000000 0.0741000
 0.8000000 0.0519000
 0.9000000 0.0277000
 0.9500000 0.0146000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0121500
 0.0250000 -.0168000
 0.0500000 -.0216000
 0.0750000 -.0239000
 0.1000000 -.0252000
 0.1500000 -.0258000
 0.2000000 -.0244000
 0.3000000 -.0216000
 0.4000000 -.0176700
 0.5000000 -.0135000
 0.6000000 -.0097000
 0.7000000 -.0069000
 0.8000000 -.0051000
 0.9000000 -.0033000
 0.9500000 -.0029000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 398 AIRFOIL (goe398-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe398-il50,000910.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe398-il50,000531 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe398-il100,000950.1 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe398-il100,000551.5 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe398-il200,000971.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe398-il200,000568.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe398-il500,000996.5 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe398-il500,000592.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe398-il1,000,0009120.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe398-il1,000,0005112.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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