Effects of transverse helium injection on hypersonic boundary layers

DOI10.1063/1.1401813zbMath1184.76039OpenAlexW2064981357MaRDI QIDQ3555684

Alexander Smits, B. Auvity, Michael R. Etz

Publication date: 22 April 2010

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

Full work available at URL: https://doi.org/10.1063/1.1401813

zbMATH Keywords

vorticeshypersonic flowboundary layer turbulenceheliumflow visualisationRayleigh scattering

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Related Items (2)

Hypersonic boundary layer transition on a concave wall: stationary Görtler vortices ⋮ Newly identified principle for aerodynamic heating in hypersonic flows

Cites Work

• Transition studies on an elliptic cone in Mach 8 flow using filtered Rayleigh scattering

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