Optimisation of slanted septum core and multiple folded cavity acoustic liners for aero-engines
Author:
Affiliation:
1. University of Southampton
2. Rolls-Royce Group plc
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-2172
Reference25 articles.
1. Folded Cavity Liners for Turbofan Engine Intakes
2. Smeared Impedance Model for Variable Depth Liners
3. Effect of the acoustic boundary layer on the wave propagation in ducts
4. Effect of mean-velocity profile shapes on sound transmission through two-dimensional ducts
5. On the acoustic boundary condition in the presence of flow
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1. On enhancing the noise-reduction performance of the acoustic lined duct utilizing the phase-modulating metasurface;Scientific Reports;2023-12-13
2. Aeroacoustic Liner Impedance Metamodel from Simulation and Experimental Data Using Probabilistic Learning;AIAA Journal;2023-11
3. On enhancing the noise-reduction performance of the acoustic lined duct utilizing the phase-modulating metasurface;2023-08-01
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5. An Initial Assessment of Variable Depth Liner Optimization for Ducted Proprotor Applications;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13
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