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

GOE 420 AIRFOIL (goe420-il)

GOE 420 AIRFOIL - Gottingen 420 airfoil


Airfoil goe420-il
Details Dat file Parser  
(goe420-il) GOE 420 AIRFOIL
Gottingen 420 airfoil
Max thickness 18.8% at 30% chord.
Max camber 4.3% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 420 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0280100
 0.0250000 0.0435100
 0.0500000 0.0630200
 0.0750000 0.0770400
 0.1000000 0.0885500
 0.1500000 0.1065800
 0.2000000 0.1186000
 0.3000000 0.1311500
 0.4000000 0.1307000
 0.5000000 0.1227500
 0.6000000 0.1068000
 0.7000000 0.0853500
 0.8000000 0.0584000
 0.9000000 0.0289500
 0.9500000 0.0144700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0269900
 0.0250000 -.0344900
 0.0500000 -.0434700
 0.0750000 -.0494600
 0.1000000 -.0539500
 0.1500000 -.0584300
 0.2000000 -.0604000
 0.3000000 -.0563500
 0.4000000 -.0473000
 0.5000000 -.0367500
 0.6000000 -.0267000
 0.7000000 -.0166500
 0.8000000 -.0096000
 0.9000000 -.0025500
 0.9500000 -.0000200
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

GOE 646 AIRFOILPreviewDetails
GOE 255 (MVA CA.6) AIRFOILPreviewDetails
EPPLER 856 AIRFOILPreviewDetails
EPPLER 748 AIRFOILPreviewDetails
EPPLER 1098 AIRFOILPreviewDetails
GOE 679 AIRFOILPreviewDetails
NACA 4418PreviewDetails
HQ 3.5/18 AIRFOILPreviewDetails
FX 66-S-196 V1 AIRFOILPreviewDetails
WORTMANN FX 66-17AII-182 AIRFOIL (ASPreviewDetails

Polars for GOE 420 AIRFOIL (goe420-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe420-il50,00094 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe420-il50,000513.4 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe420-il100,000932.7 at α=11.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe420-il100,000544.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe420-il200,000966.7 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe420-il200,000562.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe420-il500,000989.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe420-il500,000583.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe420-il1,000,0009111.3 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe420-il1,000,0005102.2 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit