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GOE 447 AIRFOIL (goe447-il)

GOE 447 AIRFOIL - Gottingen 447 airfoil


Airfoil goe447-il
Details Dat file Parser  
(goe447-il) GOE 447 AIRFOIL
Gottingen 447 airfoil
Max thickness 12.7% at 29.7% chord.
Max camber 8% at 39.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 447 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0120000 0.0252400
 0.0242600 0.0376800
 0.0488600 0.0578600
 0.0735600 0.0732500
 0.0982900 0.0870400
 0.1479100 0.1061100
 0.1976300 0.1200900
 0.2972900 0.1377600
 0.3972100 0.1418300
 0.4972900 0.1374000
 0.5975800 0.1228700
 0.6980300 0.0999500
 0.7986000 0.0709300
 0.8992299 0.0390100
 0.9495800 0.0213100
 1.0000000 0.0016000

 0.0000000 0.0000000
 0.0128200 -.0162500
 0.0253800 -.0192000
 0.0503900 -.0198100
 0.0753200 -.0163200
 0.1002500 -.0129200
 0.1501400 -.0071400
 0.2000200 -.0008600
 0.2997800 0.0112100
 0.3996400 0.0184700
 0.4996000 0.0204400
 0.5996400 0.0182100
 0.6997300 0.0137800
 0.7998300 0.0088600
 0.8999299 0.0033300
 0.9499800 0.0011100
 1.0000000 -.0016000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 447 AIRFOIL (goe447-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe447-il50,00096.1 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe447-il50,000516 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe447-il100,000940 at α=12°Mach=0 Ncrit=9Xfoil predictionDetails
   goe447-il100,000549.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe447-il200,000984 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe447-il200,000584.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe447-il500,0009129.4 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe447-il500,0005116.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe447-il1,000,0009161.3 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe447-il1,000,0005126.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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