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October 15, 2010, 07:51
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boundary conditions for supersonic inlets
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New Member
prop
Join Date: Oct 2010
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I am a beginner to fluent. i use fluent 6.3. I am trying to solve the flow through supersonic inlet,for the inlet i used pressure farfield condition. But am not sure abt what type of exit boundary condition to use as i don know the exit flow condition.
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