|February 19, 2009, 07:26||
Numerical simulation of Supersonic Combustion
im working on simulation of a pipe flow with an orifice with supersonic flow with one end closed and the other end open. The flow near the inlet is patched to 2000 k and i am looking for the propogation of flame front to the open end.
The fluid is taken as H2-O2 mixture at stiochiometric ratio, turbulence model as K-epsilon.
the problem im facing is the temperature is going beyond 6000k and the arrhenious rate of reaction in orders of magnitude
can someone suggest me where i would have gone wrong
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