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Old   July 8, 2004, 09:50
Default Thrust Vectoring problem
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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?

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