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GOE 386 AIRFOIL (goe386-il)

GOE 386 AIRFOIL - Gottingen 386 airfoil


Airfoil goe386-il
Details Dat file Parser  
(goe386-il) GOE 386 AIRFOIL
Gottingen 386 airfoil
Max thickness 20.3% at 29% chord.
Max camber 5.4% at 39% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 386 AIRFOIL
       17.       17.

 0.0000100 0.0000000
 0.0100700 0.0358800
 0.0214000 0.0531500
 0.0447900 0.0769400
 0.0685500 0.0952500
 0.0926200 0.1088800
 0.1412200 0.1295700
 0.1903200 0.1428000
 0.2896300 0.1530400
 0.3897100 0.1518200
 0.4906200 0.1383600
 0.5920000 0.1180400
 0.6935600 0.0950200
 0.7954300 0.0674300
 0.8976000 0.0354600
 0.9487200 0.0189200
 1.0000000 0.0016000

 0.0000100 0.0000000
 0.0144700 -.0289200
 0.0276000 -.0382300
 0.0531600 -.0466000
 0.0784100 -.0501800
 0.1036600 -.0538700
 0.1537900 -.0557700
 0.2036900 -.0542900
 0.3033100 -.0488400
 0.4028600 -.0420900
 0.5024000 -.0353400
 0.6019400 -.0285900
 0.7014800 -.0218400
 0.8010200 -.0150900
 0.9005700 -.0083400
 0.9503400 -.0049700
 1.0000000 -.0016000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 386 AIRFOIL (goe386-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe386-il50,00093.4 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe386-il50,000516.2 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe386-il100,000933.2 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe386-il100,000540.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe386-il200,000961.7 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe386-il200,000559.9 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe386-il500,000988.7 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe386-il500,000576.6 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe386-il1,000,0009103.6 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe386-il1,000,000594 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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