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GOE 595 AIRFOIL (goe595-il)

GOE 595 AIRFOIL - Gottingen 595 airfoil


Airfoil goe595-il
Details Dat file Parser  
(goe595-il) GOE 595 AIRFOIL
Gottingen 595 airfoil
Max thickness 9.6% at 30% chord.
Max camber 3% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 595 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0168500
 0.0250000 0.0242000
 0.0500000 0.0354000
 0.0750000 0.0451000
 0.1000000 0.0528000
 0.1500000 0.0637000
 0.2000000 0.0701000
 0.3000000 0.0774000
 0.4000000 0.0772000
 0.5000000 0.0735000
 0.6000000 0.0663000
 0.7000000 0.0551000
 0.8000000 0.0404000
 0.9000000 0.0217000
 0.9500000 0.0116000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0081500
 0.0250000 -.0108000
 0.0500000 -.0151000
 0.0750000 -.0169000
 0.1000000 -.0182000
 0.1500000 -.0193000
 0.2000000 -.0194000
 0.3000000 -.0181000
 0.4000000 -.0168000
 0.5000000 -.0140000
 0.6000000 -.0112000
 0.7000000 -.0084000
 0.8000000 -.0056000
 0.9000000 -.0028000
 0.9500000 -.0014000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 595 AIRFOIL (goe595-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe595-il50,000936.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe595-il50,000538.1 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe595-il100,000955.1 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe595-il100,000554.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe595-il200,000974.6 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe595-il200,000568.8 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe595-il500,000997.7 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe595-il500,000586.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe595-il1,000,0009110.6 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe595-il1,000,0005100.1 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
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