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April 5, 2000, 03:17
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Wake flow of missile body
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Guest
Posts: n/a
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I am investigating wake flow of an missile body in supersonic. I have problem to get uniform pressure on the baseplane, with both the standard k-epsilon, RNG and Realizable k-epsilon modelles. With 2-D flow i have get uniform pressure but in axisymmetric i have problems.
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