Once again on the supersonic flow separation near a corner

DOI10.1017/S0022112002008777zbMath1128.76330OpenAlexW2112856715MaRDI QIDQ4786757

G. L. Korolev, Anatoly I. Ruban, Jitesh S. B. Gajjar

Publication date: 8 January 2003

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/s0022112002008777

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20)

Related Items (21)

On unsteady boundary-layer separation in supersonic flow. Part 1. Upstream moving separation point ⋮ A note on the appearance of wave-packets in steady-state triple-deck solutions of supersonic flow past a compression corner ⋮ An effective numerical method for solving viscous–inviscid interaction problems ⋮ Comparison of computations of asymptotic flow models in a constricted channel ⋮ Global stability of separated flows: subsonic flow past corners. Global stability of separated flows ⋮ Separation zones in the flow near a small-angle convex corner ⋮ Global stability of supersonic flow over a hollow cylinder/flare ⋮ Double-deck structure revisited ⋮ High-frequency instabilities in supersonic compression-ramp flow ⋮ Hypersonic flow over spherically blunted double cones ⋮ Laminar hypersonic leading edge separation – a numerical study ⋮ Subsonic flow past localised heating elements in boundary layers ⋮ Temperature factor effect on the structure of the separated flow within a supersonic gas stream ⋮ Hypersonic compression corner flow with large separated regions ⋮ Direct simulation Monte Carlo computations and experiments on leading-edge separation in rarefied hypersonic flow ⋮ Global flow instability in a lid-driven cavity ⋮ Occurrence of global instability in hypersonic compression corner flow ⋮ Numerical solution of unsteady boundary-layer separation in supersonic flow: upstream moving wall ⋮ Local temperature perturbations of the boundary layer in the regime of free viscous–inviscid interaction ⋮ Three-dimensionality of hypersonic laminar flow over a double cone ⋮ On wave-packets and discontinuities in triple-deck solutions of supersonic separated flows at a compression corner

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