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GOE 547 AIRFOIL (goe547-il)

GOE 547 AIRFOIL - Gottingen 547 airfoil


Airfoil goe547-il
Details Dat file Parser  
(goe547-il) GOE 547 AIRFOIL
Gottingen 547 airfoil
Max thickness 10.5% at 29.7% chord.
Max camber 4% at 49.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 547 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0120200 0.0163500
 0.0242600 0.0252200
 0.0489000 0.0374400
 0.0736100 0.0471700
 0.0984000 0.0544000
 0.1480300 0.0668700
 0.1977800 0.0753300
 0.2974700 0.0857800
 0.3973400 0.0902200
 0.4974000 0.0881700
 0.5976500 0.0796300
 0.6980400 0.0665900
 0.7985700 0.0485600
 0.8992000 0.0270300
 0.9495600 0.0150100
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0129200 -.0141200
 0.0255200 -.0177500
 0.0506300 -.0215100
 0.0756700 -.0227700
 0.1007100 -.0240300
 0.1507400 -.0250500
 0.2007000 -.0235800
 0.3005600 -.0191300
 0.4004000 -.0136900
 0.5002300 -.0077400
 0.6000800 -.0028000
 0.7000000 0.0001500
 0.7999800 0.0006000
 0.8999800 0.0005500
 0.9499800 0.0005200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 547 AIRFOIL (goe547-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe547-il50,000936.9 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe547-il50,000535.2 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe547-il100,000960.4 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe547-il100,000559.5 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe547-il200,000986.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe547-il200,000582.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe547-il500,0009120.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe547-il500,0005105.8 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe547-il1,000,0009143.4 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe547-il1,000,0005104.7 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
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