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August 12, 2007, 23:48	hai	#1
rav_aero Guest Posts: n/a	I m trying to model a 2-dimensional axisymmetric flow, for 0.7 mach no... Can somebody please tell me as to what boundary conditions and tubulence model i should use. thank u

August 13, 2007, 06:00	Re: hai	#2
Joe Guest Posts: n/a	Look at the choked nozzle flow tutorial.

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