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

GOE 480 AIRFOIL (goe480-il)

GOE 480 AIRFOIL - Gottingen 480 airfoil


Airfoil goe480-il
Details Dat file Parser  
(goe480-il) GOE 480 AIRFOIL
Gottingen 480 airfoil
Max thickness 11.8% at 30% chord.
Max camber 5.5% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 480 AIRFOIL
       13.       13.

 0.0000000 0.0000000
 0.0250000 0.0366400
 0.0500000 0.0522700
 0.1000000 0.0750500
 0.2000000 0.1006000
 0.3000000 0.1106500
 0.4000000 0.1107000
 0.5000000 0.1032500
 0.6000000 0.0898000
 0.7000000 0.0708500
 0.8000000 0.0494000
 0.9000000 0.0259500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0218600
 0.0500000 -.0237200
 0.1000000 -.0219500
 0.2000000 -.0134000
 0.3000000 -.0068500
 0.4000000 -.0008000
 0.5000000 0.0027500
 0.6000000 0.0048000
 0.7000000 0.0048500
 0.8000000 0.0034000
 0.9000000 0.0014500
 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 406 AIRFOILPreviewDetails
GOE 365 AIRFOILPreviewDetails
NACA 6412PreviewDetails
GOE 591 AIRFOILPreviewDetails
St. CYR 24 (Bartel 35-IIIC)PreviewDetails
GOE 509 AIRFOILPreviewDetails
USA 27 AIRFOILPreviewDetails
GOE 332 (PFALZ 61) AIRFOILPreviewDetails
MH 115 11.06%PreviewDetails
GOE 701 AIRFOILPreviewDetails

Polars for GOE 480 AIRFOIL (goe480-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe480-il50,000910.2 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe480-il50,000530.3 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe480-il100,000952.1 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe480-il100,000557.3 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe480-il200,000979 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe480-il200,000579.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe480-il500,0009112.5 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe480-il500,0005107.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe480-il1,000,0009138.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe480-il1,000,0005127.8 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit