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GOE 433 AIRFOIL (goe433-il)

GOE 433 AIRFOIL - Gottingen 433 airfoil


Airfoil goe433-il
Details Dat file Parser  
(goe433-il) GOE 433 AIRFOIL
Gottingen 433 airfoil
Max thickness 17.4% at 29.2% chord.
Max camber 4.8% at 49.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 433 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0105700 0.0292000
 0.0220900 0.0439700
 0.0459400 0.0611500
 0.0699500 0.0761400
 0.0942000 0.0874500
 0.1431200 0.1036000
 0.1923400 0.1154700
 0.2915400 0.1274600
 0.3915600 0.1271000
 0.4921600 0.1181800
 0.5932800 0.1011900
 0.6946200 0.0810200
 0.7963099 0.0555700
 0.8980700 0.0290300
 0.9490300 0.0146200
 1.0000000 0.0008000

 0.0000000 0.0000000
 0.0141200 -.0243600
 0.0272700 -.0341900
 0.0529800 -.0448800
 0.0783400 -.0502000
 0.1035500 -.0533200
 0.1536400 -.0548000
 0.2035700 -.0536800
 0.3030400 -.0457800
 0.4023000 -.0345900
 0.5013200 -.0199100
 0.6004600 -.0069300
 0.6998800 0.0018700
 0.7995099 0.0073900
 0.8995301 0.0070300
 0.9497800 0.0033700
 1.0000000 -.0008000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 433 AIRFOIL (goe433-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe433-il50,00095.7 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe433-il50,000522.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe433-il100,000948.2 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe433-il100,000553.1 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe433-il200,000975.9 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe433-il200,000571.9 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe433-il500,0009102.7 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe433-il500,000589 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe433-il1,000,0009115.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe433-il1,000,0005100.3 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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