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GOE 380 AIRFOIL (goe380-il)

GOE 380 AIRFOIL - Gottingen 380 airfoil


Airfoil goe380-il
Details Dat file Parser  
(goe380-il) GOE 380 AIRFOIL
Gottingen 380 airfoil
Max thickness 6.6% at 30% chord.
Max camber 5.6% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 380 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124500 0.0180300
 0.0249300 0.0280600
 0.0498900 0.0441200
 0.0748600 0.0556900
 0.0998400 0.0642500
 0.1498100 0.0758700
 0.1997900 0.0835000
 0.2997800 0.0887500
 0.3997800 0.0870000
 0.4998000 0.0792500
 0.5998300 0.0690000
 0.6998600 0.0557500
 0.7999000 0.0395000
 0.8999500 0.0212500
 0.9499700 0.0108700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125100 -.0024700
 0.0250100 -.0024400
 0.0500000 0.0006200
 0.0749900 0.0051900
 0.0999700 0.0102500
 0.1499600 0.0153700
 0.1999500 0.0195000
 0.2999400 0.0232500
 0.3999400 0.0235000
 0.4999500 0.0207500
 0.5999600 0.0170000
 0.6999700 0.0117500
 0.7999800 0.0065000
 0.9000000 0.0012500
 0.9500000 0.0003700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 380 AIRFOIL (goe380-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe380-il50,000931.1 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe380-il50,000540.9 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe380-il100,000954.4 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe380-il100,000560 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe380-il200,000975.6 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe380-il200,000578 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe380-il500,0009103.4 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe380-il500,0005103.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe380-il1,000,0009125.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe380-il1,000,0005124.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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