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October 29, 2022, 17:27 |
Defining Supersonic Outlet in Ansys Fluent
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#1 |
Member
İbrahim
Join Date: Jun 2017
Posts: 31
Rep Power: 9 |
I have an hypersonic flow internal case. In user guide, it said that "Should the flow become locally supersonic, the specified pressure will no longer be used; pressure will be extrapolated from the flow in the interior. All other flow quantities are extrapolated from the interior." However when i change the backflow pressure, mach number of exit plane is changed. Secondly, in hypersonic case example in official tutorial case fluent document, pressure outlet is set 25 Pa. If it were surpass, the value would have been zero.
Could you help me about clarifying the issue? |
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October 29, 2022, 18:08 |
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#2 |
Senior Member
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,761
Rep Power: 66 |
There are no hard constraints at supersonic outlets that needs defining. However, you need to make sure that it is supersonic first. There are boundary conditions that will result in a subsonic flow, namely too high a pressure.
Set a low enough pressure such that the exit becomes supersonic. If you set a high enough backflow pressure, the outlet becomes an inlet! |
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October 29, 2022, 18:40 |
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#3 | |
Member
İbrahim
Join Date: Jun 2017
Posts: 31
Rep Power: 9 |
Quote:
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October 29, 2022, 21:38 |
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#4 |
Senior Member
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,761
Rep Power: 66 |
To be even more clear, use a pressure outlet and set a low enough pressure such that the flow becomes supersonic.
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October 30, 2022, 04:59 |
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#5 |
Member
İbrahim
Join Date: Jun 2017
Posts: 31
Rep Power: 9 |
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