Hello Everybody, do u know from where i can get the mesh files for the NACA 0012 airfoil to use in gambit . . . . .

Thanks in advance

Hi,

I do not know anywhere to get the mesh files from, but there are extensive references on the web to generate the NACA profile and you can generate meshes yourself from there. Do a google search on NACA0012 and you'll find heaps.

Glenn Horrocks

I searched the CFD-online message index and found out that there are reference websites for airfoils design.

The direct link is the following: http://www.pagendarm.de/trapp/progra...les/NACA4.html

Thanks Glenn

HELLO.

I DON'T KNOW TO MESHING THE AIRFOIL IN TURBULENT FLOW

THANKS

Sir,

i need pressure distribution curve over NACA 0012 at different anagles of attack(5,10,15,20,25 deg). free stream velocity = 100.8 km/hr, density = 1.224 kg/ cubic meter

Please , I need to help you about information the NACA0012 , because I will do work the project.

you can find a small program which generates points for airfoil definition, including NACA0012 which is a very standard airfoil.

The way to mesh it is using inflated prism mesh around the airfoil to capture the boundary layer.

good luck.