Thrust vectoring of rocket nozzle by a jet tab -- CFD Online Discussion Forums

January 17, 2017, 08:33	Thrust vectoring of rocket nozzle by a jet tab	#1
umesh k. New Member UMK Join Date: Sep 2015 Posts: 12 Rep Power: 11	hello, 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? Thanks.

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