The viscous interaction between sound waves and the trailing edge of a supersonic splitter plate

DOI10.1017/S0022112094000686zbMath0814.76056MaRDI QIDQ4304635

N. Peake

Publication date: 31 August 1994

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

zbMATH Keywords

asymptotic solutionpotential theoryvortex sheetWiener-Hopf theoryviscous shear flowtriple-deck structuretwo-region parabolic scheme

Mathematics Subject Classification ID

Hydro- and aero-acoustics (76Q05) Supersonic flows (76J20)

Related Items (3)

Receptivity to harmonic forcing of a finite-width mixing layer just downstream of the trailing edge of a flat plate ⋮ A model supersonic buried-nozzle jet: instability and acoustic wave scattering and the far-field sound ⋮ Instability of a vortex sheet leaving a right-angled wedge

Cites Work

• Sound generation by a supersonic aerofoil cutting through a steady jet flow
• Sound diffraction at a trailing edge
• Low-frequency sound radiation and generation due to the interaction of unsteady flow with a jet pipe
• On the viscous flow about the trailing edge of a rapidly oscillating plate
• Radiation properties of the semi-infinite vortex sheet: the initial-value problem
• The flow about the trailing edge of a supersonic oscillating aerofoil
• A review of the theory of trailing edge noise
• Trailing-edge stall
• Boundary-Layer Flow Near the Trailing Edge of a Flat Plate
• Instability of a Vortex Sheet Leaving a Semi‐Infinite Plate

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