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GOE 429 AIRFOIL (goe429-il)

GOE 429 AIRFOIL - Gottingen 429 airfoil


Airfoil goe429-il
Details Dat file Parser  
(goe429-il) GOE 429 AIRFOIL
Gottingen 429 airfoil
Max thickness 11.4% at 30% chord.
Max camber 0.2% at 10% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 429 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0202000
 0.0250000 0.0271000
 0.0500000 0.0367000
 0.0750000 0.0447000
 0.1000000 0.0495000
 0.1500000 0.0547000
 0.2000000 0.0569000
 0.3000000 0.0569000
 0.4000000 0.0532000
 0.5000000 0.0468000
 0.6000000 0.0372000
 0.7000000 0.0261000
 0.8000000 0.0160000
 0.9000000 0.0069000
 0.9500000 0.0037000
 1.0000000 0.0016000

 0.0000000 0.0000000
 0.0125000 -.0165000
 0.0250000 -.0245000
 0.0500000 -.0346000
 0.0750000 -.0410000
 0.1000000 -.0457000
 0.1500000 -.0527000
 0.2000000 -.0558000
 0.3000000 -.0569000
 0.4000000 -.0527000
 0.5000000 -.0452000
 0.6000000 -.0356000
 0.7000000 -.0239000
 0.8000000 -.0144000
 0.9000000 -.0074000
 0.9500000 -.0043000
 1.0000000 -.0016000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 429 AIRFOIL (goe429-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe429-il50,000923.1 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe429-il50,000526.9 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe429-il100,000935.5 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe429-il100,000537.6 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe429-il200,000947.4 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe429-il200,000545.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe429-il500,000957.2 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe429-il500,000558.6 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe429-il1,000,000967.9 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe429-il1,000,000572.7 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
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