Inviscid–viscous interaction on triple-deck scales in a hypersonic flow with strong wall cooling

DOI10.1017/S0022112090003275zbMath0711.76055MaRDI QIDQ3496064

No author found.

Publication date: 1990

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

zbMATH Keywords

boundary-layer methodsFinite-difference equationshigh supersonic flowInviscid-viscous interactionlarge-band matrix solverramp-induced pressuretriple-deck scaleswall-temperature influence

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Hypersonic flows (76K05)

Related Items

A note on the appearance of wave-packets in steady-state triple-deck solutions of supersonic flow past a compression corner ⋮ The propagation of perturbations in supersonic boundary layers ⋮ Global stability of supersonic flow over a hollow cylinder/flare ⋮ Laminar hypersonic leading edge separation – a numerical study ⋮ The influence of wall cooling on hypersonic boundary-layer separation and stability ⋮ Hypersonic compression corner flow with large separated regions ⋮ Numerical study of bluntness effects on laminar leading edge separation in hypersonic flow ⋮ The effects of displacement induced by thermal perturbations on the structure and stability of boundary-layer flows ⋮ Three-dimensionality of hypersonic laminar flow over a double cone

Cites Work

• D’Alembert’s Paradox
• Plate-injection into a separated supersonic boundary layer