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GOE 449 AIRFOIL (goe449-il)

GOE 449 AIRFOIL - Gottingen 449 airfoil


Airfoil goe449-il
Details Dat file Parser  
(goe449-il) GOE 449 AIRFOIL
Gottingen 449 airfoil
Max thickness 17% at 30% chord.
Max camber 5.4% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 449 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0312000
 0.0250000 0.0454000
 0.0500000 0.0653000
 0.0750000 0.0802000
 0.1000000 0.0916000
 0.1500000 0.1094000
 0.2000000 0.1217000
 0.3000000 0.1358000
 0.4000000 0.1384000
 0.5000000 0.1310000
 0.6000000 0.1171000
 0.7000000 0.0952000
 0.8000000 0.0673000
 0.9000000 0.0354000
 0.9500000 0.0182000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0178000
 0.0250000 -.0241000
 0.0500000 -.0307000
 0.0750000 -.0338000
 0.1000000 -.0354000
 0.1500000 -.0366000
 0.2000000 -.0363000
 0.3000000 -.0337000
 0.4000000 -.0306000
 0.5000000 -.0260000
 0.6000000 -.0224000
 0.7000000 -.0168000
 0.8000000 -.0112000
 0.9000000 -.0046000
 0.9500000 -.0013000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 449 AIRFOIL (goe449-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe449-il50,00094.2 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   goe449-il50,000512.1 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe449-il100,000934.7 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe449-il100,000543.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe449-il200,000970.4 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe449-il200,000565.6 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe449-il500,000997.5 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe449-il500,000587.7 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe449-il1,000,0009117.9 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe449-il1,000,0005107.8 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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