The jet edge-tone feedback cycle; linear theory for the operating stages

DOI10.1017/S002211209200082XzbMath0850.76153OpenAlexW2037928718MaRDI QIDQ3991464

David G. Crighton

Publication date: 28 June 1992

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

Full work available at URL: https://doi.org/10.1017/s002211209200082x

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Wakes and jets (76D25)

Related Items (8)

Finite-wavelength scattering of incident vorticity and acoustic waves at a shrouded-jet exit ⋮ Self-sustained oscillations with acoustic feedback in flows over a backward-facing step with a small upstream step ⋮ A 2D finite-element scheme for fluid-solid-acoustic interactions and its application to human phonation ⋮ Coupled oscillations of flow along a perforated plate ⋮ Shear layer oscillation along a perforated surface: A self-excited large-scale instability ⋮ Asymptotic factorization of Wiener-Hopf kernels. ⋮ Vortical–acoustic resonance in an acoustic resonator: Strouhal number variation, destabilization and stabilization ⋮ A throttling mechanism sustaining a hole tone feedback system at very low Mach numbers

Cites Work

• Asymptotic factorization for perturbed Wiener-Hopf problems
• The coupling between flow instabilities and incident disturbances at a leading edge
• Acoustics as a branch of fluid mechanics
• On the unsteady wake-induced lift on a slotted airfoil, part II: The influence of displacement thickness fluctuations
• Radiation properties of the semi-infinite vortex sheet: the initial-value problem
• On vortex sound at low Mach number
• Resonance in flows with vortex sheets and edges
• Instability of a Vortex Sheet Leaving a Semi‐Infinite Plate
• The excess noise field of subsonic jets

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