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GOE 741 AIRFOIL (goe741-il)

GOE 741 AIRFOIL - Gottingen 741 airfoil


Airfoil goe741-il
Details Dat file Parser  
(goe741-il) GOE 741 AIRFOIL
Gottingen 741 airfoil
Max thickness 15.3% at 30% chord.
Max camber 4.8% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 741 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0307300
 0.0250000 0.0444600
 0.0500000 0.0639200
 0.0750000 0.0793900
 0.1000000 0.0908500
 0.1500000 0.1080700
 0.2000000 0.1180000
 0.3000000 0.1248500
 0.4000000 0.1171000
 0.5000000 0.0982500
 0.6000000 0.0751000
 0.7000000 0.0499500
 0.8000000 0.0268000
 0.9000000 0.0091500
 0.9500000 0.0033800
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0212700
 0.0250000 -.0267400
 0.0500000 -.0317800
 0.0750000 -.0341100
 0.1000000 -.0346500
 0.1500000 -.0347300
 0.2000000 -.0323000
 0.3000000 -.0284500
 0.4000000 -.0271000
 0.5000000 -.0277500
 0.6000000 -.0264000
 0.7000000 -.0245500
 0.8000000 -.0224000
 0.9000000 -.0138500
 0.9500000 -.0074300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 741 AIRFOIL (goe741-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe741-il50,00093.9 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe741-il50,000514.1 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe741-il100,000917.5 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe741-il100,000539 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe741-il200,000961.6 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe741-il200,000566.9 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe741-il500,0009101.4 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe741-il500,000593 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe741-il1,000,0009122.4 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe741-il1,000,0005106.3 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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