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Backflow in nozzle exit (combustion chamber with nozzle)

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Old   June 9, 2020, 08:15
Default Backflow in nozzle exit (combustion chamber with nozzle)
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Lee Jo
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Hi..
I'm modelling a 3d combustion chamber with nozzle...the operating pressure are very high and fuels used are CH4 and liquid Oxygen (cryogenic temperature)

Inlets : 8MPa
Outlet : tried both 0MPa and 101325 Pa

Operating conditions: 6MPa

I am getting backflow in the outlet and the setup diverges...my mesh is good and have no skewness at exit or inside chamber and nozzle..my mesh is fine..

I even tried long slender gradually increasing length mesh at outlet so that the backflows stop..

My outlet pressure outlet backflow specification: Normal to boundary...

Anyone knows how to solve this...??!!
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Old   June 15, 2020, 07:37
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It appears to be a compressible flow. Use value of 0 Pa as operating pressure and apply all boundary pressure values as absolute values. You may also want to choose non-reflecting condition at the outlet.
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Old   June 15, 2020, 09:51
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Quote:
Originally Posted by vinerm View Post
It appears to be a compressible flow. Use value of 0 Pa as operating pressure and apply all boundary pressure values as absolute values. You may also want to choose non-reflecting condition at the outlet.
Yeah..I'm using SRK real gas equations..my outlet is a pressure outlet and how do I set it as a non reflecting condition??
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Old   June 15, 2020, 09:55
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That option is available within boundary condition panel. Open pressure outlet and you will see Acoustic condition options.
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