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GOE 481A AIRFOIL (goe481a-il)

GOE 481A AIRFOIL - Gottingen 481A airfoil


Airfoil goe481a-il
Details Dat file Parser  
(goe481a-il) GOE 481A AIRFOIL
Gottingen 481A airfoil
Max thickness 15.3% at 29.4% chord.
Max camber 5.5% at 39.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 481A AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0116100 0.0284000
 0.0229300 0.0440800
 0.0469600 0.0647100
 0.0713000 0.0788500
 0.0957500 0.0905000
 0.1450000 0.1063200
 0.1944700 0.1176400
 0.2939700 0.1283200
 0.3939600 0.1285200
 0.4943000 0.1212300
 0.5948600 0.1094600
 0.6955700 0.0941900
 0.7965300 0.0739400
 0.8978500 0.0457000
 0.9487300 0.0270900
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0138600 -.0288500
 0.0267000 -.0372400
 0.0520000 -.0425600
 0.0770600 -.0438800
 0.1020300 -.0432000
 0.1517600 -.0373700
 0.2015300 -.0325300
 0.3011500 -.0243500
 0.4008500 -.0181600
 0.5006100 -.0129700
 0.6004600 -.0097800
 0.7003100 -.0065900
 0.8002300 -.0048900
 0.9001500 -.0031900
 0.9501100 -.0023400
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 481A AIRFOIL (goe481a-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe481a-il50,00096.5 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe481a-il50,000527.9 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe481a-il100,000947.3 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe481a-il100,000546.3 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe481a-il200,000963.8 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe481a-il200,000559 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe481a-il500,000980.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe481a-il500,000574.1 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe481a-il1,000,000995.8 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe481a-il1,000,000581.3 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
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