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peter.zhao June 16, 2002 23:40

Boundary Condition for spout.
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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