Experiments on stability and transition at Mach 3

DOI10.1017/S0022112002002094zbMath1024.76508MaRDI QIDQ4409248

Garry L. Brown, Paolo Graziosi

Publication date: 24 November 2003

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

zbMATH Keywords

stabilitytransitionreceptivityhot wiresflat-plate laminar boundary layer

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Parallel shear flows in hydrodynamic stability (76E05) Supersonic flows (76J20)

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Wall heat transfer effects on Klebanoff modes and Tollmien–Schlichting waves in a compressible boundary layer ⋮ Nonlinear unsteady streaks engendered by the interaction of free-stream vorticity with a compressible boundary layer ⋮ Response and receptivity of the hypersonic boundary layer past a wedge to free-stream acoustic, vortical and entropy disturbances ⋮ Sensitivity of high-speed boundary-layer stability to base-flow distortion ⋮ Continuous mode transition in high-speed boundary-layers ⋮ Free-stream coherent structures in parallel compressible boundary-layer flows at subsonic and moderate supersonic Mach numbers ⋮ Compressible unsteady Görtler vortices subject to free-stream vortical disturbances ⋮ Response of a compressible laminar boundary layer to free-stream vortical disturbances ⋮ Excitation and evolution of radiating modes in supersonic boundary layers. II: Back effect of spontaneously radiated Mach waves

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