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GOE 495 AIRFOIL (goe495-il)

GOE 495 AIRFOIL - Gottingen 495 airfoil


Airfoil goe495-il
Details Dat file Parser  
(goe495-il) GOE 495 AIRFOIL
Gottingen 495 airfoil
Max thickness 6.9% at 30% chord.
Max camber 5% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 495 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0166400
 0.0250000 0.0237900
 0.0500000 0.0345700
 0.0750000 0.0428600
 0.1000000 0.0496500
 0.1500000 0.0597200
 0.2000000 0.0678000
 0.3000000 0.0774500
 0.4000000 0.0806000
 0.5000000 0.0777500
 0.6000000 0.0704000
 0.7000000 0.0585500
 0.8000000 0.0422000
 0.9000000 0.0233500
 0.9500000 0.0124200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0078600
 0.0250000 -.0097100
 0.0500000 -.0109200
 0.0750000 -.0106400
 0.1000000 -.0093500
 0.1500000 -.0052700
 0.2000000 -.0007000
 0.3000000 0.0084500
 0.4000000 0.0166000
 0.5000000 0.0222500
 0.6000000 0.0249000
 0.7000000 0.0240500
 0.8000000 0.0192000
 0.9000000 0.0108500
 0.9500000 0.0059200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 495 AIRFOIL (goe495-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe495-il50,000944.8 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe495-il50,000545.2 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe495-il100,000969.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe495-il100,000569.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe495-il200,000995.8 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe495-il200,000593.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe495-il500,0009132.8 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe495-il500,0005122.7 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe495-il1,000,0009158.9 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   goe495-il1,000,0005126.9 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
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