boundary conditions compressible flow -- CFD Online Discussion Forums

June 7, 2006, 11:55	boundary conditions compressible flow	#1
newposter Guest Posts: n/a	hi, I want to simulate a shock in laval nozzle with my pressure-correction based SIMPLE code. I want to prescribe at Inlet: u,v,w and T at the Outlet: p_Stat I can`t get convergence, the residuals are oszillating. What can I do, please help?!

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