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GOE 746 AIRFOIL (goe746-il)

GOE 746 AIRFOIL - Gottingen 746 airfoil


Airfoil goe746-il
Details Dat file Parser  
(goe746-il) GOE 746 AIRFOIL
Gottingen 746 airfoil
Max thickness 9.8% at 30% chord.
Max camber 5% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 746 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0194900
 0.0250000 0.0299700
 0.0500000 0.0474500
 0.0750000 0.0599200
 0.1000000 0.0704000
 0.1500000 0.0848500
 0.2000000 0.0933000
 0.3000000 0.0992000
 0.4000000 0.0921000
 0.5000000 0.0755000
 0.6000000 0.0559000
 0.7000000 0.0353000
 0.8000000 0.0167000
 0.9000000 0.0051000
 0.9500000 0.0020500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0093100
 0.0250000 -.0095200
 0.0500000 -.0085500
 0.0750000 -.0070700
 0.1000000 -.0061000
 0.1500000 -.0036500
 0.2000000 -.0017000
 0.3000000 0.0017000
 0.4000000 0.0026000
 0.5000000 0.0005000
 0.6000000 -.0041000
 0.7000000 -.0092000
 0.8000000 -.0108000
 0.9000000 -.0084000
 0.9500000 -.0049500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 746 AIRFOIL (goe746-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe746-il50,00097.9 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe746-il50,000520.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe746-il100,000946.3 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   goe746-il100,000549.1 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe746-il200,000973.4 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe746-il200,000573.8 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe746-il500,0009106.3 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe746-il500,0005102.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe746-il1,000,0009129.6 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe746-il1,000,0005118.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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