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GOE 450 AIRFOIL (goe450-il)

GOE 450 AIRFOIL - Gottingen 450 airfoil


Airfoil goe450-il
Details Dat file Parser  
(goe450-il) GOE 450 AIRFOIL
Gottingen 450 airfoil
Max thickness 8.9% 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 450 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122900 0.0200300
 0.0247100 0.0280600
 0.0495700 0.0414200
 0.0744600 0.0512800
 0.0993700 0.0600400
 0.1492400 0.0727600
 0.1991400 0.0826800
 0.2990300 0.0932200
 0.3990000 0.0952700
 0.4990500 0.0911200
 0.5991500 0.0811600
 0.6993000 0.0673100
 0.7994900 0.0492500
 0.8997200 0.0267000
 0.9498500 0.0141300
 1.0000000 0.0010500

 0.0000000 0.0000000
 0.0126100 -.0103700
 0.0251200 -.0112400
 0.0501100 -.0109800
 0.0751000 -.0097200
 0.1000800 -.0078500
 0.1500500 -.0047300
 0.2000100 -.0010100
 0.2999600 0.0042300
 0.3999100 0.0083800
 0.4998700 0.0122200
 0.5998900 0.0104700
 0.6999100 0.0084100
 0.7999300 0.0067600
 0.8999700 0.0031000
 0.9499900 0.0010300
 1.0000000 -.0010500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 450 AIRFOIL (goe450-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe450-il50,000939.6 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe450-il50,000540.1 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe450-il100,000963.4 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe450-il100,000564.4 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe450-il200,000988.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe450-il200,000585.6 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe450-il500,0009120.7 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe450-il500,0005108 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe450-il1,000,0009141.4 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe450-il1,000,0005118.9 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
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