Effect of sound-absorbing materials on intensity of disturbances in the shock layer on a flat plate aligned at an angle of attack

DOI10.1134/S0021894412020034zbMath1298.76111OpenAlexW1969777015MaRDI QIDQ468859

I. S. Tsyryul'nikov, S. G. Mironov, S. V. Kirilovskij, Tatiana V. Poplavskaya, Anatoly A. Maslov

Publication date: 10 November 2014

Published in: Journal of Applied Mechanics and Technical Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0021894412020034

zbMATH Keywords

experimentnumerical simulationscontrol of disturbanceshypersonic shock layersound-absorbing coatings

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Shock waves and blast waves in fluid mechanics (76L05) Hypersonic flows (76K05)

Related Items (3)

Application of the skeleton model of a highly porous cellular material in modeling supersonic flow past a cylinder with a forward gas-permeable insert ⋮ Control of disturbances of a hypersonic viscous shock layer on a flat plate ⋮ Supersonic flow around a cylinder with a permeable high-porosity insert: experiment and numerical simulation

Cites Work

• Receptivity of a hypersonic boundary layer over a flat plate with a porous coating
• An experimental study of density waves in a hypersonic shock layer on a flat plate
• Wave processes in a viscous shock layer and control of fluctuations
• Stabilization of a hypersonic boundary layer using an ultrasonically absorptive coating
• Experimental study and direct numerical simulation of the evolution of disturbances in a viscous shock layer on a flat plate

This page was built for publication: Effect of sound-absorbing materials on intensity of disturbances in the shock layer on a flat plate aligned at an angle of attack