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- W2044133693 abstract "When a uniform stream of strength U1 mixes with a parallel stream of strength U2 (0<U2≤U1) at a trailing edge the high Reynolds number (R»1) viscous-flow structure is shown to be a straightforward generalization of the ‘triple-deck’ structure which is present in the case U1 = U2. This is confirmed by a full numerical solution of the governing equations in the ‘lower deck’ for the case of two supersonic stream. For an incompressible fluid the limit in which U2→0 is considered and here it is shown that the triple-deck is no longer the dominant feature of the flow; instead the major influence of the trailing edge is confined to a much smaller region inside the boundary layer where the full Navier-Stokes equations apply. A detailed study of the trailing-edge flow in this case reveals the formation of a comparatively broad boundary layer, of thickness O(R−¼), along the plate in the stagnant fluid. Consideration of the flow at the trailing edge also leads to the unique determination of the location of the dividing streamline in the wake. The theory is also directly applicable to the flow of a uniform stream over a backward-facing step." @default.
- W2044133693 created "2016-06-24" @default.
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- W2044133693 date "1977-01-01" @default.
- W2044133693 modified "2023-09-25" @default.
- W2044133693 title "VISCOUS MIXING AT A TRAILING EDGE" @default.
- W2044133693 doi "https://doi.org/10.1093/qjmam/30.3.319" @default.
- W2044133693 hasPublicationYear "1977" @default.
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