|March 23, 2010, 02:43||
supersonic flow over flat plate
Join Date: Apr 2009
Posts: 35Rep Power: 8
i have been writing C code to solve supersonic flow over flat plate, using finite difference method.
I'm using assuming steady state solution.
I'm using the boudary layer eqns, or reduced N-S eqns. I have been getting decent results for subsonic flow.
but for supersonic flow, i realized that boundary conditions cannot be fress stream conditions, so can anyone suggest what boundary conditions @ leading edge should i use..
thank you very much
|March 23, 2010, 09:26||
Join Date: Jul 2009
Posts: 200Rep Power: 9
You'll probably want to take a look at Riemann boundary conditions. These utilize the Riemann invariants based on the local state of the flow at the boundary.
|Thread||Thread Starter||Forum||Replies||Last Post|
|Supersonic flow over flat plate||Nikhil||Main CFD Forum||6||May 20, 2013 12:48|
|incompressible, 2-D laminar flow over flat plate...||varunjain89||Main CFD Forum||3||March 6, 2012 12:13|
|supersonic flow past flat plate||shuo||Main CFD Forum||0||July 28, 2007 19:47|
|PIV - transitional flat plate flows||MC||Main CFD Forum||0||July 4, 2007 08:21|
|Conjugate heat transfer for film-cooled flat plate||Michele||FLUENT||0||July 3, 2006 08:42|