which commerical code can simulate accurately the shock wave induced boundary separation on a wing surface ?

Hi Pao,

I am doing a masters research project modelling shock diffraction and shock boundary layer interaction. I use CFD-Fastran, wich is a density based CFD code for compressible flow simulation. This software can model shock stuctures in great deatil. It can also model moving bodies through the use of overset grids. Chemistry is also available, enabling accuarate simulation of hypersonic flows.

The web site is www.cfdrc.com.

Hi: Mike Thanks for the information. Can I take a look of your research results if it is available?