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GOE 481 AIRFOIL (goe481-il)

GOE 481 AIRFOIL - Gottingen 481 airfoil


Airfoil goe481-il
Details Dat file Parser  
(goe481-il) GOE 481 AIRFOIL
Gottingen 481 airfoil
Max thickness 13.4% at 9.6% chord.
Max camber 8.8% at 39.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 481 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0111400 0.0290200
 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 -.0362400
 0.0520000 -.0425600
 0.0770600 -.0438800
 0.1020300 -.0432000
 0.1498800 0.0025400
 0.1986200 0.0293400
 0.2978900 0.0450000
 0.3977600 0.0476900
 0.4978400 0.0459000
 0.5980700 0.0411100
 0.6984600 0.0328300
 0.7989600 0.0220500
 0.8995200 0.0102800
 0.9498100 0.0041400
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 481 AIRFOIL (goe481-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe481-il50,00097 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe481-il50,000528.9 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe481-il100,000943 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe481-il100,000541.1 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe481-il200,000953.4 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe481-il200,000548.9 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe481-il500,000963.4 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe481-il500,000558.3 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe481-il1,000,000970.3 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe481-il1,000,000563.8 at α=10°Mach=0 Ncrit=5Xfoil predictionDetails
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