Shock-wave laminar boundary-layer interaction in supercritical transonic flow

DOI10.1016/0045-7930(86)90002-2zbMath0589.76077OpenAlexW2054295479MaRDI QIDQ1074443

R. J. Bodonyi, Frank T. Smith

Publication date: 1986

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7930(86)90002-2

zbMATH Keywords

laminar boundary layerviscous-inviscid interactionoblique shock waveintervening plateau region of nearly constant pressurenonlinear triple deck problemorder one shock strengthsreattachment regionsshock strength parametersupercritical transonic flow

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Transonic flows (76H05) Basic methods in fluid mechanics (76M99)

Related Items

The interactive breakdown in supersonic ramp flow ⋮ Transonic flow over localised heating elements in boundary layers ⋮ A numerical method for treating strongly interactive three-dimensional viscous-inviscid flows ⋮ Laminar hypersonic leading edge separation – a numerical study ⋮ On boundary-layer transition in transonic flow ⋮ An efficient interacting boundary layer method for supersonic flow in the transonic regime

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