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GOE 430 AIRFOIL (goe430-il)

GOE 430 AIRFOIL - Gottingen 430 airfoil


Airfoil goe430-il
Details Dat file Parser  
(goe430-il) GOE 430 AIRFOIL
Gottingen 430 airfoil
Max thickness 13.4% at 29.5% chord.
Max camber 4.8% at 49.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 430 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0116000 0.0205100
 0.0236100 0.0318300
 0.0478500 0.0491000
 0.0723500 0.0604700
 0.0969300 0.0701500
 0.1463100 0.0842100
 0.1959100 0.0933800
 0.2953400 0.1064400
 0.3952900 0.1075100
 0.4955200 0.1022000
 0.5960200 0.0909100
 0.6967000 0.0753200
 0.7976200 0.0543400
 0.8945000 0.0299500
 0.9493200 0.0155800
 1.0000000 0.0011000

 0.0000000 0.0000000
 0.0133800 -.0200100
 0.0262100 -.0275500
 0.0514900 -.0340400
 0.0766500 -.0377400
 0.1017200 -.0393400
 0.1516800 -.0382600
 0.2015800 -.0360700
 0.3011700 -.0268100
 0.4007300 -.0165500
 0.5002300 -.0051900
 0.5998000 0.0045700
 0.6994600 0.0122400
 0.7994200 0.0133100
 0.8996000 0.0091000
 0.9497899 0.0048000
 1.0000000 -.0011000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 430 AIRFOIL (goe430-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe430-il50,000930.7 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe430-il50,000536.5 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe430-il100,000959.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe430-il100,000560.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe430-il200,000983.8 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe430-il200,000579.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe430-il500,0009111.4 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe430-il500,000596.6 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe430-il1,000,0009125.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe430-il1,000,0005104.8 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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