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August 29, 2015, 07:55
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Thermal plume
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Senior Member
sunil
Join Date: Jul 2012
Location: Bangalore
Posts: 179
Rep Power: 14  |
Hello Every one
I am trying to simulate thermal plume from a nozzle exit and for that i am referring "Study on infrared signature of solid rocket motor afterburning exhaust plume" Paper. For details about geometry, boundary conditions and solver settings please refer attached images. mass momentum and energy equations are not converging. please suggest me if i did any thing wrong while assigning boundary conditions or solver settings. (mesh is very fine) http://postimg.org/image/4zut4r7hx/ http://postimg.org/image/iut3n81x1/ http://postimg.org/image/9oaszxwol/ |
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