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GOE 432 AIRFOIL (goe432-il)

GOE 432 AIRFOIL - Gottingen 432 airfoil


Airfoil goe432-il
Details Dat file Parser  
(goe432-il) GOE 432 AIRFOIL
Gottingen 432 airfoil
Max thickness 7.7% at 20% chord.
Max camber 4.3% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 432 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0211100
 0.0250000 0.0307200
 0.0500000 0.0444500
 0.0750000 0.0536700
 0.1000000 0.0609000
 0.1500000 0.0693500
 0.2000000 0.0758000
 0.3000000 0.0802000
 0.4000000 0.0776000
 0.5000000 0.0710000
 0.6000000 0.0629000
 0.7000000 0.0518000
 0.8000000 0.0382000
 0.9000000 0.0216000
 0.9500000 0.0110500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0068900
 0.0250000 -.0087700
 0.0500000 -.0085500
 0.0750000 -.0078300
 0.1000000 -.0066000
 0.1500000 -.0041500
 0.2000000 -.0012000
 0.3000000 0.0052000
 0.4000000 0.0091000
 0.5000000 0.0110000
 0.6000000 0.0109000
 0.7000000 0.0088000
 0.8000000 0.0062000
 0.9000000 0.0023000
 0.9500000 0.0010500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 432 AIRFOIL (goe432-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe432-il50,000935.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe432-il50,000540.4 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe432-il100,000953.3 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe432-il100,000556.9 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe432-il200,000972.5 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe432-il200,000572 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe432-il500,000994.8 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe432-il500,000588.3 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe432-il1,000,0009108 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe432-il1,000,0005107.6 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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