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GOE 411 AIRFOIL (goe411-il)

GOE 411 AIRFOIL - Gottingen 411 airfoil


Airfoil goe411-il
Details Dat file Parser  
(goe411-il) GOE 411 AIRFOIL
Gottingen 411 airfoil
Max thickness 13.2% at 30% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 411 AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0125000 0.0115000
 0.0250000 0.0184000
 0.0500000 0.0305000
 0.0750000 0.0388000
 0.1000000 0.0460000
 0.1500000 0.0550000
 0.2000000 0.0605000
 0.3000000 0.0660000
 0.4000000 0.0655000
 0.5000000 0.0605000
 0.6000000 0.0530000
 0.7000000 0.0440000
 0.8000000 0.0320000
 0.9000000 0.0180000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0115000
 0.0250000 -.0184000
 0.0500000 -.0305000
 0.0750000 -.0388000
 0.1000000 -.0460000
 0.1500000 -.0550000
 0.2000000 -.0605000
 0.3000000 -.0660000
 0.4000000 -.0655000
 0.5000000 -.0605000
 0.6000000 -.0530000
 0.7000000 -.0440000
 0.8000000 -.0320000
 0.9000000 -.0180000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 411 AIRFOIL (goe411-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe411-il50,000930.1 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe411-il50,000528 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe411-il100,000940.7 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe411-il100,000534.1 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe411-il200,000943.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe411-il200,000535.6 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe411-il500,000945.8 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe411-il500,000542.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe411-il1,000,000948.7 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe411-il1,000,000553.4 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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