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How can we give the boundary conditions for Inlet jet in Forward facing jet?

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Old   January 1, 2014, 15:05
Default How can we give the boundary conditions for Inlet jet in Forward facing jet?
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Madhu
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I am working on Drag reduction in hyper sonic vehicles problem.
I would like to give the boundary conditions for forward facing jet problems in Fluent.

If it is a Pressure-inlet condition, explain me what is the difference between Total gauge pressure and Supersonic/initial gauge pressure?

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madhu gundeti
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