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GOE 458 AIRFOIL (goe458-il)

GOE 458 AIRFOIL - Gottingen 458 airfoil


Airfoil goe458-il
Details Dat file Parser  
(goe458-il) GOE 458 AIRFOIL
Gottingen 458 airfoil
Max thickness 7.2% at 29.9% chord.
Max camber 5.2% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 458 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124100 0.0125900
 0.0248400 0.0206900
 0.0497400 0.0343700
 0.0746600 0.0450600
 0.0996000 0.0537500
 0.1495100 0.0656200
 0.1994500 0.0735000
 0.2993700 0.0837500
 0.3993500 0.0870000
 0.4993800 0.0827500
 0.5994500 0.0735000
 0.6995400 0.0607500
 0.7996700 0.0435000
 0.8998300 0.0232500
 0.9499100 0.0121200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125300 -.0045100
 0.0250400 -.0063100
 0.0500600 -.0076200
 0.0750600 -.0079400
 0.1000500 -.0067500
 0.1499900 -.0019300
 0.1999800 0.0030000
 0.2999100 0.0117500
 0.3998700 0.0170000
 0.4998600 0.0187500
 0.5998600 0.0185000
 0.6998700 0.0167500
 0.7999099 0.0125000
 0.8999600 0.0057500
 0.9499800 0.0031200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 458 AIRFOIL (goe458-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe458-il50,000942.8 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe458-il50,000542.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe458-il100,000965.1 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe458-il100,000564.6 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe458-il200,000987.5 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe458-il200,000586.9 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe458-il500,0009117.8 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe458-il500,0005115.3 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe458-il1,000,0009140.9 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe458-il1,000,0005136.3 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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