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Forum: FLUENT

November 6, 2014, 07:06

Replies: 4

convergence problem in 2D steady supersonic flow

Views: 2,069

Posted By sehs15

thank you bro ,, but it seems like pressure...

thank you bro ,, but it seems like pressure boundaries also have fluctuations , i will try to extend the domain much more ans see

Forum: FLUENT

November 5, 2014, 07:47

Replies: 4

convergence problem in 2D steady supersonic flow

Views: 2,069

Posted By sehs15

yeah the domain behind the airfoil is about 10...

yeah the domain behind the airfoil is about 10 times the chord .. i tried pressure inlet boundary and its much much more better than velocity inlet with little oscillations ,, i will try to reduce...

Forum: FLUENT

November 4, 2014, 07:10

Replies: 4

convergence problem in 2D steady supersonic flow

Views: 2,069

Posted By sehs15

convergence problem in 2D steady supersonic flow

Hello Guys ..

I'm simulating a flow over a 2D supersonic airfoil with fluent, steady state, density based solver, structured quad cells with yplus around 2 and SA turbulence model, boundaries are...

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