Excitation of unstable modes in a supersonic boundary layer by acoustic waves

DOI10.1007/BF01050314zbMath0825.76247OpenAlexW2056308370MaRDI QIDQ1190908

S. Singh

Publication date: 27 September 1992

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01050314

Mathematics Subject Classification ID

Hydro- and aero-acoustics (76Q05) Hydrodynamic stability (76E99) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items

Numerical modeling of the receptivity of a supersonic boundary layer to acoustic disturbances, Numerical modeling of the disturbances of the separated flow in a rounded compression corner, A unified explanation of energy growth sources for unstable modes in flat-plate boundary layers, Numerical modeling of the receptivity of a supersonic boundary layer to entropy disturbances, Response and receptivity of the hypersonic boundary layer past a wedge to free-stream acoustic, vortical and entropy disturbances, Receptivity of a boundary layer to external sonic waves, Interactions between vortical, acoustic and thermal components during hypersonic transition, Generation of first Mack modes in supersonic boundary layers by slow acoustic waves interacting with streamwise isolated wall roughness, Acoustic receptivity of Mach 4.5 boundary layer with leading-edge bluntness, Receptivity of inviscid modes in supersonic boundary layers to wall perturbations, Non-localized boundary layer instabilities resulting from leading edge receptivity at moderate supersonic Mach numbers, Receptivity of supersonic boundary layers over smooth and wavy surfaces to impinging slow acoustic waves, First-mode-induced nonlinear breakdown in a hypersonic boundary layer, Perturbation Analysis of Nonlinear Stages in Hypersonic Transition

Cites Work

• The evolution of Tollmien–Sclichting waves near a leading edge
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