[Lee97]

Can anyone recommend to me what is the best validation case for incompressible 3D finite wing?

Onera M6 is transonic

I need subsonic, incompressible.

[aerosayan]

Originally Posted by Lee97

Can anyone recommend to me what is the best validation case for incompressible 3D finite wing?

Onera M6 is transonic

I need subsonic, incompressible.

Low Mach solutions have been studied for ONERA M6. Here's one for Mach 0.3 : https://www.grc.nasa.gov/www/wind/va.../m6wing02.html

Original ONERA M6 validation test page:https://www.grc.nasa.gov/www/wind/va...ng/m6wing.html

[Lee97]

Originally Posted by aerosayan

Low Mach solutions have been studied for ONERA M6. Here's one for Mach 0.3 : https://www.grc.nasa.gov/www/wind/va.../m6wing02.html

Original ONERA M6 validation test page:https://www.grc.nasa.gov/www/wind/va...ng/m6wing.html

Oh... thx, but in specific, I need viscous, 3D finite, incompressible, subsonic and fixed wing.

Nobody..?