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March 23, 2010, 02:43 |
supersonic flow over flat plate
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#1 |
Member
varun
Join Date: Apr 2009
Posts: 35
Rep Power: 17 |
hello!
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 varun jain |
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March 23, 2010, 09:26 |
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#2 |
Senior Member
Join Date: Jul 2009
Posts: 357
Rep Power: 19 |
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.
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