A small Strouhal number analysis for acoustic wave-jet flow-pipe interaction

DOI10.1016/0022-460X(83)91019-2zbMath0531.76019OpenAlexW2114704005MaRDI QIDQ3313451

Sjoerd W. Rienstra

Publication date: 1983

Published in: Journal of Sound and Vibration (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0022-460x(83)91019-2

zbMATH Keywords

asymptotic expansionsreflection coefficientarbitrary Mach numberend- impedanceend-correctioninfluence of Kutta condition at lip of pipeMunt's exact formal solutionpressure and velocity fluctuationssmall Strouhal number

Mathematics Subject Classification ID

Hydro- and aero-acoustics (76Q05) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Related Items (5)

Aeroacoustic power generated by a compact axisymmetric cavity: prediction of self-sustained oscillation and influence of the depth ⋮ Finite-wavelength scattering of incident vorticity and acoustic waves at a shrouded-jet exit ⋮ Acoustic propagation and scattering in the exhaust flow from coaxial cylinders ⋮ Acoustic scattering at a hard-soft lining transition in a flow duct ⋮ A model supersonic buried-nozzle jet: instability and acoustic wave scattering and the far-field sound

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