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GOE 361 AIRFOIL (goe361-il)

GOE 361 AIRFOIL - Gottingen 361 airfoil


Airfoil goe361-il
Details Dat file Parser  
(goe361-il) GOE 361 AIRFOIL
Gottingen 361 airfoil
Max thickness 6.8% at 20% chord.
Max camber 5.5% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 361 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0170900
 0.0250000 0.0256900
 0.0500000 0.0408800
 0.0750000 0.0525600
 0.1000000 0.0617500
 0.1500000 0.0756300
 0.2000000 0.0825000
 0.3000000 0.0872500
 0.4000000 0.0845000
 0.5000000 0.0772500
 0.6000000 0.0660000
 0.7000000 0.0527500
 0.8000000 0.0375000
 0.9000000 0.0197500
 0.9500000 0.0106300
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0084100
 0.0250000 -.0073100
 0.0500000 -.0041200
 0.0750000 -.0004400
 0.1000000 0.0032500
 0.1500000 0.0096200
 0.2000000 0.0145000
 0.3000000 0.0222500
 0.4000000 0.0260000
 0.5000000 0.0277500
 0.6000000 0.0265000
 0.7000000 0.0227500
 0.8000000 0.0175000
 0.9000000 0.0087500
 0.9500000 0.0036300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 361 AIRFOIL (goe361-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe361-il50,000939.3 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe361-il50,000542.4 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe361-il100,000957.8 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe361-il100,000559.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe361-il200,000976.6 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe361-il200,000577.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe361-il500,0009103.8 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe361-il500,0005101.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe361-il1,000,0009123.4 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe361-il1,000,0005119.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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