Acoustic receptivity of Mach 4.5 boundary layer with leading-edge bluntness

DOI10.1007/S00162-007-0050-5zbMath1161.76560OpenAlexW2026257866MaRDI QIDQ1020441

Ponnampalam Balakumar, Mujeeb R. Malik

Publication date: 29 May 2009

Published in: Theoretical and Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: http://hdl.handle.net/2060/20070035910

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Finite volume methods applied to problems in fluid mechanics (76M12) Boundary-layer theory for compressible fluids and gas dynamics (76N20) Stability and instability of nonparallel flows in hydrodynamic stability (76E09)

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Transition mechanisms in cross-flow-dominated hypersonic flows with free-stream acoustic noise ⋮ 3D global optimal forcing and response of the supersonic boundary layer

Cites Work

• Excitation of unstable modes in a supersonic boundary layer by acoustic waves
• Interaction between a supersonic boundary layer and acoustic disturbances
• Numerical methods for hypersonic boundary layer stability
• The evolution of Tollmien–Sclichting waves near a leading edge
• Receptivity of a high-speed boundary layer to acoustic disturbances
• Receptivity of a supersonic boundary layer over a flat plate. Part 2. Receptivity to free-stream sound
• Receptivity of a supersonic boundary layer over a flat plate. Part 3. Effects of different types of free-stream disturbances
• Prehistory of instability in a hypersonic boundary layer.

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