The interactive breakdown in supersonic ramp flow

DOI10.1017/S0022112091001714zbMath0765.76042OpenAlexW2088585115MaRDI QIDQ3971842

Ahmad Farid Khorrami, Frank T. Smith

Publication date: 25 June 1992

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

Full work available at URL: https://doi.org/10.1017/s0022112091001714

zbMATH Keywords

separating flowglobal Newton iteration procedureinteractive-boundary-layer approachlarge adverse pressure gradientlinear multi-sweepinglinearized shootinglocal breakdownreversed-flow regionsecond- order accurate windward differencing

Mathematics Subject Classification ID

Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (14)

A note on the appearance of wave-packets in steady-state triple-deck solutions of supersonic flow past a compression corner ⋮ Global stability of supersonic flow over a hollow cylinder/flare ⋮ Instability of supersonic compression ramp flow ⋮ High-frequency instabilities in supersonic compression-ramp flow ⋮ Hypersonic flow over spherically blunted double cones ⋮ Laminar hypersonic leading edge separation – a numerical study ⋮ The influence of wall cooling on hypersonic boundary-layer separation and stability ⋮ Separation phenomenon in a hypersonic flow with strong wall cooling: Subcritical regime ⋮ Temperature factor effect on the structure of the separated flow within a supersonic gas stream ⋮ Homoclinic bifurcation in Blasius boundary-layer flow ⋮ Hypersonic compression corner flow with large separated regions ⋮ Occurrence of global instability in hypersonic compression corner flow ⋮ 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

Cites Work

• Triple-deck solutions for subsonic flow past humps, steps, concave or convex corners and wedged trailing edges
• Shock-wave laminar boundary-layer interaction in supercritical transonic flow
• Separated supersonic flow past a trailing edge at incidence
• Boundary-Layer Interaction Theory
• Laminar flow over unsteady humps: the formation of waves
• Two-dimensional disturbance travel, growth and spreading in boundary layers
• D’Alembert’s Paradox

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