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GOE 387 AIRFOIL (goe387-il)

GOE 387 AIRFOIL - Gottingen 387 airfoil


Airfoil goe387-il
Details Dat file Parser  
(goe387-il) GOE 387 AIRFOIL
Gottingen 387 airfoil
Max thickness 14.9% at 30% chord.
Max camber 5.5% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 387 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0308800
 0.0250000 0.0452600
 0.0500000 0.0645200
 0.0750000 0.0787900
 0.1000000 0.0905500
 0.1500000 0.1065800
 0.2000000 0.1181000
 0.3000000 0.1276500
 0.4000000 0.1262000
 0.5000000 0.1167500
 0.6000000 0.0998000
 0.7000000 0.0783500
 0.8000000 0.0539000
 0.9000000 0.0279500
 0.9500000 0.0144700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0186200
 0.0250000 -.0217400
 0.0500000 -.0249700
 0.0750000 -.0272100
 0.1000000 -.0279500
 0.1500000 -.0274300
 0.2000000 -.0259000
 0.3000000 -.0208500
 0.4000000 -.0158000
 0.5000000 -.0122500
 0.6000000 -.0087000
 0.7000000 -.0061500
 0.8000000 -.0046000
 0.9000000 -.0030500
 0.9500000 -.0025200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 387 AIRFOIL (goe387-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe387-il50,00096.1 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe387-il50,000522.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe387-il100,000943.6 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe387-il100,000550.3 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe387-il200,000971.9 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe387-il200,000569.8 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe387-il500,0009101 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe387-il500,000593 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe387-il1,000,0009122.5 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe387-il1,000,0005114.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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