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Thrust vectoring of rocket nozzle by a jet tab

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Old   January 17, 2017, 07:33
Default Thrust vectoring of rocket nozzle by a jet tab
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I am dealing with the issue of divergence in fluent while running a simulation on thrust vectoring of the rocket using a jet tab placed in the flow direction.
I played with meshing and adaption, but divergence is coming all the time, what should I do for convergence?
Any other technique for analysis?
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