An optimized microphone array for the measurement of turbulent boundary layer wall pressure wavenumber-frequency spectra
Author:
Affiliation:
1. von Kármán Institute for Fluid Dynamics
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-2968
Reference25 articles.
1. Vehicle noise and vibration refinement
2. BOUNDARY LAYER INDUCED NOISE IN AIRCRAFT, PART I: THE FLAT PLATE MODEL
3. A WAVENUMBER APPROACH TO MODELLING THE RESPONSE OF A RANDOMLY EXCITED PANEL, PART II: APPLICATION TO AIRCRAFT PANELS EXCITED BY A TURBULENT BOUNDARY LAYER
4. Measured wavenumber: Frequency spectrum associated with acoustic and aerodynamic wall pressure fluctuations
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1. On the challenges of estimating the low-wavenumber wall pressure field beneath a turbulent boundary layer using a microphone array;Journal of Sound and Vibration;2024-03
2. Low-Wavenumber Wall Pressure Measurements in Zero-Pressure Gradient Boundary Layer Flow;AIAA SCITECH 2022 Forum;2022-01-03
3. Development of a test rig for the measurement of turbulent boundary layer wall pressure statistics;2018 AIAA/CEAS Aeroacoustics Conference;2018-06-24
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