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Boundary Condition for spout.

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Old   June 16, 2002, 23:40
Default Boundary Condition for spout.
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Hi,everyone,I want to know how to implement boundary condition (B.C) for spout in a combustor with two layers of phantom cells ( namely halo cells) in finite volume method. How to give the values on the phantom cells, when I know the total pressure, total temperature and the Mach number at the exit of spout? All comments are appreciated! Thanks in advance!
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