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

GOE 629 AIRFOIL (goe629-il)

GOE 629 AIRFOIL - Gottingen 629 airfoil


Airfoil goe629-il
Details Dat file Parser  
(goe629-il) GOE 629 AIRFOIL
Gottingen 629 airfoil
Max thickness 13.6% at 29.4% chord.
Max camber 2.8% at 39.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 629 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0111100 0.0231700
 0.0230600 0.0323800
 0.0472200 0.0463300
 0.0716300 0.0563000
 0.0961500 0.0642700
 0.1454300 0.0762300
 0.1949200 0.0846900
 0.2944400 0.0926700
 0.3943800 0.0936600
 0.4947400 0.0876800
 0.5953400 0.0777200
 0.6961700 0.0637700
 0.7972500 0.0458300
 0.8985400 0.0244100
 0.9492500 0.0124600
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0136800 -.0196800
 0.0267100 -.0284000
 0.0523000 -.0383600
 0.0776000 -.0433400
 0.1027800 -.0463300
 0.1528700 -.0478300
 0.2028400 -.0473300
 0.3026000 -.0433400
 0.4022700 -.0378600
 0.5019100 -.0318900
 0.6015600 -.0259100
 0.7012000 -.0199300
 0.8008100 -.0134500
 0.9004200 -.0069700
 0.9502100 -.0034900
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

RG 15A 2.5/13.0 AIRFOILPreviewDetails
BOEING 106 AIRFOILPreviewDetails
MRC-16PreviewDetails
GOE 575 AIRFOILPreviewDetails
E197 (13.49%)PreviewDetails
NACA 2414PreviewDetails
S2027PreviewDetails
DELFT DU84-132V3 AIRFOIL (MEASURED)PreviewDetails
RAF 38 AIRFOILPreviewDetails
SD7062 (14%)PreviewDetails

Polars for GOE 629 AIRFOIL (goe629-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe629-il50,000929.4 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe629-il50,000532.2 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe629-il100,000950.3 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe629-il100,000550.3 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe629-il200,000970 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe629-il200,000566.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe629-il500,000994.7 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe629-il500,000581.9 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe629-il1,000,0009107.2 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe629-il1,000,000592.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit