The response of a laminar boundary layer in supersonic flow to small-amplitude progressive waves

DOI10.1017/S0022112090003019zbMath0706.76069MaRDI QIDQ3487024

Peter W. Duck

Publication date: 1990

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

zbMATH Keywords

laminar boundary layerboundary-layer thicknesssemi-infinite flat platesmall-amplitude progressive waveperturbation flowstreamwise zonesuniform supersonic free-stream flowunsteady linearized compressible boundary-layer equations

Mathematics Subject Classification ID

Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10) Supersonic flows (76J20)

Related Items (2)

Acoustic-roughness receptivity in subsonic boundary-layer flows over aerofoils ⋮ An adjoint compressible linearised Navier–Stokes approach to model generation of Tollmien–Schlichting waves by sound

Cites Work

• Triple-deck flow over unsteady surface disturbances: The three- dimensional development of Tollmien-Schlichting waves
• The evolution of Tollmien–Sclichting waves near a leading edge
• On boundary layers associated with oscillating streams
• The evolution of Tollmien-Schlichting waves near a leading edge. Part 2. Numerical determination of amplitudes
• Laminar flow over unsteady humps: the formation of waves
• On the first-mode instability in subsonic, supersonic or hypersonic boundary layers
• The unsteady laminar boundary layer on a semi-infinite flat plate due to small fluctuations in the magnitude of the free-stream velocity
• Two-dimensional boundary layers in a free stream which oscillates without reversing

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