On a turbulent mixing layer created downstream of a ``\(\Lambda \) notch simulating one wavelength of a Chevron nozzle

DOI10.1007/S10494-009-9217-ZzbMath1422.76010OpenAlexW2041651429MaRDI QIDQ1037418

J. Blot

Publication date: 16 November 2009

Published in: Flow, Turbulence and Combustion (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10494-009-9217-z

zbMATH Keywords

flow controlflow structuremixing layerstreamwise vortices

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Direct numerical and large eddy simulation of turbulence (76F65) Turbulent transport, mixing (76F25) Control of turbulent flows (76F70)

Related Items (1)

The application of boundary layer independence principle to three-dimensional turbulent mixing layers

Cites Work

• The effect of streamwise vortices on the aeroacoustics of a Mach 0.9 jet
• Vortical structures in a laminar V-notched indeterminate-origin jet
• Turbulent Flows
• A new mechanism of small-scale transition in a plane mixing layer: core dynamics of spanwise vortices
• On the periodically excited plane turbulent mixing layer, emanating from a jagged partition

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