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

GOE 479 AIRFOIL (goe479-il)

GOE 479 AIRFOIL - Gottingen 479 airfoil


Airfoil goe479-il
Details Dat file Parser  
(goe479-il) GOE 479 AIRFOIL
Gottingen 479 airfoil
Max thickness 11.6% at 30% chord.
Max camber 4% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 479 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0263700
 0.0250000 0.0352400
 0.0500000 0.0485800
 0.0750000 0.0597100
 0.1000000 0.0684500
 0.1500000 0.0809200
 0.2000000 0.0889000
 0.3000000 0.0968500
 0.4000000 0.0958000
 0.5000000 0.0892500
 0.6000000 0.0772000
 0.7000000 0.0621500
 0.8000000 0.0446000
 0.9000000 0.0235500
 0.9500000 0.0120200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0141300
 0.0250000 -.0187600
 0.0500000 -.0225300
 0.0750000 -.0242900
 0.1000000 -.0250500
 0.1500000 -.0245700
 0.2000000 -.0231000
 0.3000000 -.0191500
 0.4000000 -.0157000
 0.5000000 -.0122500
 0.6000000 -.0088000
 0.7000000 -.0058500
 0.8000000 -.0034000
 0.9000000 -.0019500
 0.9500000 -.0009700
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

USA-35B AIRFOILPreviewDetails
CLARK Z AIRFOILPreviewDetails
Rhode St. Genese 32PreviewDetails
GOE 593 AIRFOILPreviewDetails
NACA 4412PreviewDetails
Davis AIRFOILPreviewDetails
GOE 623 AIRFOILPreviewDetails
CLARK W AIRFOILPreviewDetails
N-10PreviewDetails
GOE 693 AIRFOILPreviewDetails

Polars for GOE 479 AIRFOIL (goe479-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe479-il50,000931.6 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe479-il50,000535.4 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe479-il100,000953.9 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe479-il100,000555.3 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe479-il200,000975.1 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe479-il200,000572.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe479-il500,0009101.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe479-il500,000594.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe479-il1,000,0009121.5 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe479-il1,000,0005110.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit