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.

Posting Rules
You may not post new threads You may not post replies You may not post attachments You may not edit your posts BB code is On Smilies are On [IMG] code is On HTML code is Off Trackbacks are Off Pingbacks are On Refbacks are On Forum Rules

Similar Threads
Thread	Thread Starter	Forum	Replies	Last Post
compressible, rhoSimpleFoam, multi-species, steady state, rocket nozzle	David_C	OpenFOAM Running, Solving & CFD	1	April 18, 2017 12:01
Thrust vectoring in jets	umesh k.	Main CFD Forum	0	November 22, 2016 00:46
Need help with a rocket nozzle simulation	badboyz31	CFX	14	September 22, 2014 01:06
Calculating thrust for a rocket nozzle for a biphasic fluid	toniatop	CFX	0	January 17, 2013 20:15
C-D nozzle supersonic jet boundary	Gland	FLUENT	4	May 24, 2012 01:25

All times are GMT -4. The time now is 12:36.