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GOE 535 AIRFOIL (goe535-il)

GOE 535 AIRFOIL - Gottingen 535 airfoil


Airfoil goe535-il
Details Dat file Parser  
(goe535-il) GOE 535 AIRFOIL
Gottingen 535 airfoil
Max thickness 16.1% at 20% chord.
Max camber 5.8% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 535 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0410200
 0.0250000 0.0555400
 0.0500000 0.0745700
 0.0750000 0.0891100
 0.1000000 0.1006500
 0.1500000 0.1162300
 0.2000000 0.1258000
 0.3000000 0.1324500
 0.4000000 0.1271000
 0.5000000 0.1152500
 0.6000000 0.0984000
 0.7000000 0.0782500
 0.8000000 0.0557000
 0.9000000 0.0298500
 0.9500000 0.0154300
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0194800
 0.0250000 -.0264600
 0.0500000 -.0329300
 0.0750000 -.0348900
 0.1000000 -.0358500
 0.1500000 -.0362800
 0.2000000 -.0347000
 0.3000000 -.0280500
 0.4000000 -.0149000
 0.5000000 -.0002500
 0.6000000 0.0119000
 0.7000000 0.0160500
 0.8000000 0.0152000
 0.9000000 0.0088500
 0.9500000 0.0029200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 535 AIRFOIL (goe535-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe535-il50,00097.2 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe535-il50,000529.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe535-il100,000943.1 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe535-il100,000550.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe535-il200,000968.1 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe535-il200,000568.5 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe535-il500,000996.6 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe535-il500,000590.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe535-il1,000,0009116.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe535-il1,000,0005110.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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