Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

GOE 300 (FRIEDRICHSHAFEN G20) AIRFOIL (goe300-il)

GOE 300 (FRIEDRICHSHAFEN G20) AIRFOIL - Gottingen 300 (Friedrichshafen G20) airfoil


Airfoil goe300-il
Details Dat file Parser  
(goe300-il) GOE 300 (FRIEDRICHSHAFEN G20) AIRFOIL
Gottingen 300 (Friedrichshafen G20) airfoil
Max thickness 8.4% at 30% chord.
Max camber 6.7% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 300 (FRIEDRICHSHAFEN G20) AIRFOIL
       14.       14.

 0.0000000 0.0000000
 0.0250000 0.0389500
 0.0500000 0.0566000
 0.1000000 0.0784000
 0.1500000 0.0915000
 0.2000000 0.1015000
 0.3000000 0.1090000
 0.4000000 0.1078000
 0.5000000 0.0989000
 0.6000000 0.0854000
 0.7000000 0.0685000
 0.8000000 0.0485000
 0.9000000 0.0256000
 1.0000000 0.0018000

 0.0000000 0.0000000
 0.0250000 -.0097500
 0.0500000 -.0080000
 0.1000000 0.0030000
 0.1500000 0.0125000
 0.2000000 0.0186000
 0.3000000 0.0247000
 0.4000000 0.0245000
 0.5000000 0.0215000
 0.6000000 0.0173000
 0.7000000 0.0130000
 0.8000000 0.0086000
 0.9000000 0.0040000
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

NACA M23 AIRFOILPreviewDetails
NACA M20 AIRFOILPreviewDetails
GOE 81 AIRFOILPreviewDetails
GOE 304 (FRIEDRICHSHAFEN G02)PreviewDetails
GOE 15 AIRFOILPreviewDetails
GOE 92 AIRFOILPreviewDetails
NACA6409 9%PreviewDetails
GOE 118 (MVA MK.7) AIRFOILPreviewDetails
GOE 336 (MVA H.44) AIRFOILPreviewDetails
GOE 140 (MVA H.17) AIRFOILPreviewDetails

Polars for GOE 300 (FRIEDRICHSHAFEN G20) AIRFOIL (goe300-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe300-il50,000919.9 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe300-il50,000538.1 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe300-il100,000954.9 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe300-il100,000561 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe300-il200,000979.1 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe300-il200,000581.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe300-il500,0009107.6 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe300-il500,0005105.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe300-il1,000,0009130.4 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe300-il1,000,0005126.9 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit