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Old   July 27, 2004, 04:54
Default transonic axisymmetric flow
ejaz ahmed
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hello! i have problem in computations for an axisymmetric bump with a mach number of 0.875 and reynold number at bump is 13.1e05.these are the only considitons given to me without any indication of the static pressure at the inlet or outlet.i am having problems in setting up the proper boundary conditions.
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Old   August 24, 2004, 11:11
Default Re: transonic axisymmetric flow
Johnson Mendonca
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There are several other papers by 1)liu & squire 2)D.A Johnson, Horstman and W.D Bachalo which talk about axisymmetric bump cases. They have more detailed info. Search for those papers else contact me via e-mail

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