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Forum: FLUENT

November 16, 2010, 03:37

Replies: 2

Con-Div Nozzle Shock structure problem

Views: 3,163

Posted By padmanathan

thanks for your reply, chris. by now, i...

thanks for your reply, chris.

by now, i changed my solution from second order upwind scheme to first order scheme. now i can able to simulate by increasing the back pressure upto some level. and...

Forum: FLUENT

October 29, 2010, 02:26

Replies: 2

Con-Div Nozzle Shock structure problem

Views: 3,163

Posted By padmanathan

Con-Div Nozzle Shock structure problem

Dear All,

I'm working in simulation of supersonic flow through Nozzle.

I need to simulate shock structure at the exit of the nozzle.

My problem is, I need to simulate normal shock at the...

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