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GOE 417A (GEW. PLATTE) AIRFOIL (goe417a-il)

GOE 417A (GEW. PLATTE) AIRFOIL - Gottingen 417A (GEW. PLATTE) airfoil


Airfoil goe417a-il
Details Dat file Parser  
(goe417a-il) GOE 417A (GEW. PLATTE) AIRFOIL
Gottingen 417A (GEW. PLATTE) airfoil
Max thickness 3.2% at 2.5% chord.
Max camber 5.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 417A (GEW. PLATTE) AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0125000 0.0155000
 0.0250000 0.0220000
 0.0500000 0.0325000
 0.0750000 0.0415000
 0.1000000 0.0485000
 0.1500000 0.0570000
 0.2000000 0.0630000
 0.3000000 0.0715000
 0.4000000 0.0735000
 0.5000000 0.0700000
 0.6000000 0.0640000
 0.7000000 0.0545000
 0.8000000 0.0425000
 0.9000000 0.0240000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0140000
 0.0250000 -.0100000
 0.0500000 0.0010000
 0.0750000 0.0105000
 0.1000000 0.0185000
 0.1500000 0.0275000
 0.2000000 0.0340000
 0.3000000 0.0425000
 0.4000000 0.0445000
 0.5000000 0.0410000
 0.6000000 0.0350000
 0.7000000 0.0255000
 0.8000000 0.0135000
 0.9000000 -.0015000
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for GOE 417A (GEW. PLATTE) AIRFOIL (goe417a-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe417a-il50,000946.5 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe417a-il50,000545.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe417a-il100,000965.5 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe417a-il100,000556.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe417a-il200,000971.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe417a-il200,000561.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe417a-il500,000975.9 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe417a-il500,000568.1 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe417a-il1,000,000986.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe417a-il1,000,0005116.9 at α=1.25°Mach=0 Ncrit=5Xfoil predictionDetails
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