Abstract
We consider self-sustained oscillations of the grazing flow along the neck of a Helmholtz-like resonator. Such oscillations are driven by a coupling between the intrinsic instability of the shear layer, separating the main flow from the cavity, and the resonant acoustical field in the cavity. Depending on details of the shape of the neck, acoustical velocities through the neck of the resonator of the same order of magnitude as the main flow velocity can be reached. For particular neck geometries, whistling is suppressed. A nonlinear model, which assumes that the vorticity of the shear layer is concentrated in line vortices traveling at constant velocity, provides insight into the phenomenon. For rounded edges, the model predicts the pulsation amplitude of the first hydrodynamic mode surprisingly well but severely overestimates the amplitude of higher hydrodynamic modes. For sharp edges, a
modification of the original model is proposed, which yields a reasonable prediction of the pulsation amplitude (within a factor of two) of the first hydrodynamic mode and does not overestimate higher hydrodynamic modes.
modification of the original model is proposed, which yields a reasonable prediction of the pulsation amplitude (within a factor of two) of the first hydrodynamic mode and does not overestimate higher hydrodynamic modes.
Original language | English |
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Pages (from-to) | 408-415 |
Number of pages | 8 |
Journal | AIAA journal |
Volume | 41 |
Issue number | 3 |
DOIs | |
Publication status | Published - 2003 |
Externally published | Yes |
Event | 7th AIAA/CEAS Aeroacoustics Conference 2001 - Maastricht, Netherlands Duration: 28 May 2001 → 30 May 2001 Conference number: 7 |