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July 27, 2004, 05:54 |
transonic axisymmetric flow
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#1 |
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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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August 24, 2004, 12:11 |
Re: transonic axisymmetric flow
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#2 |
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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
mendo002@bama.ua.edu dogma@rediffmail.com Johnson.Mendonca |
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