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An experimental investigation of flow-induced oscillations of the Bruel and Kjaer in-flow microphoneOne source contributing to wind tunnel background noise is microphone self-noise. An experiment was conducted to investigate the flow-induced acoustic oscillations of Bruel & Kjaer (B&K) in-flow microphones. The results strongly suggest the B&K microphone cavity behaves more like an open cavity. Their cavity acoustic oscillations are likely caused by strong interactions between the cavity shear layer and the cavity trailing edge. But the results also suggest that cavity shear layer oscillations could be coupled with cavity acoustic resonance to generate tones. Detailed flow velocity measurements over the cavity screen have shown inflection points in the mean velocity profiles and high disturbance and spectral intensities in the vicinity of the cavity trailing edge. These results are the evidence for strong interactions between cavity shear layer oscillations and the cavity trailing edge. They also suggest that beside acoustic signals, the microphone inside the cavity has likely recorded hydrodynamic pressure oscillations, too. The results also suggest that the forebody shape does not have a direct effect on cavity oscillations. For the FITE (Flow Induced Tone Eliminator) microphone, it is probably the forebody length and the resulting boundary layer turbulence that have made it work. Turbulence might have thickened the boundary layer at the separation point, weakened the shear layer vortices, or lifted them to miss impinging on the cavity trailing edge. In addition, the study shows that the cavity screen can modulate the oscillation frequency but not the cavity acoustic oscillation mechanisms.
Document ID
19960013908
Acquisition Source
Ames Research Center
Document Type
Thesis/Dissertation
Authors
Fields, Richard S., Jr.
(California Polytechnic State Univ. San Luis Obispo, CA United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1995
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:199982
NASA-CR-199982
Report Number: NAS 1.26:199982
Report Number: NASA-CR-199982
Accession Number
96N19067
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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