Sound generated from the interruption of a steady flow by a supersonically moving aerofoil

DOI10.1017/S0022112088002344zbMath0669.76102MaRDI QIDQ3823324

No author found.

Publication date: 1988

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

zbMATH Keywords

aerofoilKirchhoff's theoremairfoil gust responseuniform cylindrical jet

Mathematics Subject Classification ID

Gas dynamics (general theory) (76N15) Hydro- and aero-acoustics (76Q05) Supersonic flows (76J20) Basic methods in fluid mechanics (76M99) First-order hyperbolic systems (35L40)

Related Items (6)

Sound generation by a supersonic aerofoil cutting through a steady jet flow ⋮ Asymptotic analysis of the radiation by volume sources in supersonic rotor acoustics ⋮ Unsteady transonic flow past a quarter-plane ⋮ Canonical sound fields in the frequency-domain theory of supersonic leading-edge noise ⋮ The scattering of vorticity waves by a supersonic rectangular wing ⋮ Basic singular fields in the theory of impulsive supersonic leading-edge noise

Cites Work

• Sound radiation into uniformly flowing fluid by compact surface vibration
• Radiation from line vortex filaments exhausting from a two-dimensional semi-infinite duct

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