Numerical modeling of the receptivity of a supersonic boundary layer to acoustic disturbances

DOI10.1007/s10697-006-0020-4zbMath1198.76115OpenAlexW4239692403MaRDI QIDQ604569

Sumit K. Garg

Publication date: 11 November 2010

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

Full work available at URL: https://doi.org/10.1007/s10697-006-0020-4

zbMATH Keywords

Navier-Stokes equationsperturbationssupersonic flowboundary layernumerical modelingacoustics

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Hydro- and aero-acoustics (76Q05) Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (8)

Numerical modeling of the stabilization of a supersonic flat-plate boundary layer by a porous coating ⋮ Numerical modeling of the disturbances of the separated flow in a rounded compression corner ⋮ Numerical modeling of the interaction between a supersonic boundary layer and an acoustic wave ⋮ Numerical modeling of the receptivity of a supersonic boundary layer to entropy disturbances ⋮ Transition mechanisms in cross-flow-dominated hypersonic flows with free-stream acoustic noise ⋮ Wave processes in a viscous shock layer and control of fluctuations ⋮ Receptivity of a boundary layer to external sonic waves ⋮ Nonlinear wave processes in a hypersonic shock layer

Cites Work

• Excitation of unstable modes in a supersonic boundary layer by acoustic waves
• Numerical modeling of perturbation propagation in a supersonic boundary layer
• Leading-edge receptivity of a hypersonic boundary layer on a flat plate
• Leading-edge receptivity to free-stream disturbance waves for hypersonic flow over a parabola
• Receptivity of a high-speed boundary layer to acoustic disturbances
• Receptivity of a supersonic boundary layer over a flat plate. Part 1. Wave structures and interactions
• Receptivity of a supersonic boundary layer over a flat plate. Part 2. Receptivity to free-stream sound
• Prehistory of instability in a hypersonic boundary layer.

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