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GOE 400 AIRFOIL (goe400-il)

GOE 400 AIRFOIL - Gottingen 400 airfoil


Airfoil goe400-il
Details Dat file Parser  
(goe400-il) GOE 400 AIRFOIL
Gottingen 400 airfoil
Max thickness 6.1% at 20% chord.
Max camber 4.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 400 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0171700
 0.0250000 0.0256400
 0.0500000 0.0381800
 0.0750000 0.0465100
 0.1000000 0.0538500
 0.1500000 0.0645200
 0.2000000 0.0714000
 0.3000000 0.0770500
 0.4000000 0.0751000
 0.5000000 0.0675500
 0.6000000 0.0560000
 0.7000000 0.0427500
 0.8000000 0.0293000
 0.9000000 0.0151500
 0.9500000 0.0078300
 1.0000000 0.0008000

 0.0000000 0.0000000
 0.0125000 -.0108300
 0.0250000 -.0126600
 0.0500000 -.0123200
 0.0750000 -.0098900
 0.1000000 -.0046500
 0.1500000 0.0035200
 0.2000000 0.0102000
 0.3000000 0.0190500
 0.4000000 0.0227000
 0.5000000 0.0224500
 0.6000000 0.0194000
 0.7000000 0.0139500
 0.8000000 0.0083000
 0.9000000 0.0036500
 0.9500000 0.0015300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 400 AIRFOIL (goe400-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe400-il50,000937.4 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe400-il50,000541.9 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe400-il100,000959.1 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe400-il100,000561.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe400-il200,000981 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe400-il200,000579.9 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe400-il500,0009109.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe400-il500,000588.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe400-il1,000,0009126 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe400-il1,000,0005101.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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