Thrust Vectoring problem -- CFD Online Discussion Forums

July 8, 2004, 09:50	Thrust Vectoring problem	#1
Lewis Guest Posts: n/a	Hi, I'm trying to model a fluidic thrust vectoring convergent divergent jet engine nozzle in fluent 6. It's supersonic flow, but the only solver I can avoid divergence with is coupled explicit, which refuses to converge. I've tried starting with a simple model and gradually adding complexity, but as soon as I activate compressible flow I get divergence. Can anyone offer any advice? Lewis

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