Separation length in high-enthalpy shock/boundary-layer interaction

DOI10.1063/1.1289553zbMath1184.76125OpenAlexW1980136290MaRDI QIDQ3553435

B. Sturtevant, Jean-Paul Davis

Publication date: 22 April 2010

Published in: Physics of Fluids (Search for Journal in Brave)

Full work available at URL: https://authors.library.caltech.edu/3630/

zbMATH Keywords

laminar flowshock wavesboundary layershypersonic flowflow separationexternal flowsnonequilibrium flow

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Related Items (6)

Numerical assessment of correlations for shock wave boundary layer interaction ⋮ Effect of leading edge bluntness on the interaction of ramp induced shock wave with laminar boundary layer at hypersonic speed ⋮ Spatial linear stability of a hypersonic shear layer with nonequilibrium thermochemistry ⋮ Shock-induced leading-edge separation in hypersonic flows ⋮ On the length scales of hypersonic shock-induced large separation bubbles near leading edges ⋮ Hypersonic flow over spherically blunted double cones

Cites Work

• Laminar boundary layer oblique shock wave interaction on flat and curved plates
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