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GOE 456 AIRFOIL (goe456-il)

GOE 456 AIRFOIL - Gottingen 456 airfoil


Airfoil goe456-il
Details Dat file Parser  
(goe456-il) GOE 456 AIRFOIL
Gottingen 456 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 456 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 -.0048100
 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 456 AIRFOIL (goe456-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe456-il50,000942.9 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe456-il50,000542.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe456-il100,000965.1 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe456-il100,000564.6 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe456-il200,000987.5 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe456-il200,000586.3 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe456-il500,0009117.9 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe456-il500,0005115.6 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe456-il1,000,0009140.9 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe456-il1,000,0005134.3 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
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