Technical Papers
Apr 13, 2024

Detecting the Inherent Modulation Phenomenon of High-Lift Configuration Noise Using the Hilbert–Huang Transform

Publication: Journal of Aerospace Engineering
Volume 37, Issue 4

Abstract

The phenomenon of multiple tones is a typical feature of high-lift configuration noise, and the underlying nonlinear and nonstationary features need to be revealed through time-frequency analysis. This paper introduces the Hilbert–Huang transform method to detect the inherent amplitude modulation and frequency modulation phenomena of multiple tones from 30P30N three-element high-lift configuration with both slat and flap completely stowed. The acoustic modes are extracted from the multiple tones firstly and then the variation features of amplitude and instantaneous frequency are analyzed. The results show that the acoustic energy concentrates on the primary mode with much larger amplitude. Moreover, both the amplitude and instantaneous frequency are periodically varied in time and the predicted modulation frequencies are equal to the frequency intervals between nearby tones, confirming that the inherent temporal features of multiple tones are amplitude modulation and frequency modulation.

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Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.

Acknowledgments

This work is financially supported by the National Natural Science Foundation of China (Grant No. 12002021) and the Laboratory of Aerodynamic Noise Control (governed by the China Aerodynamics Research and Development Center) under the grant code of ANCL20230104.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 37Issue 4July 2024

History

Received: Sep 15, 2023
Accepted: Feb 6, 2024
Published online: Apr 13, 2024
Published in print: Jul 1, 2024
Discussion open until: Sep 13, 2024

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Associate Professor, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, China; Associate Professor, Laboratory of Aerodynamic Noise Control, China Aerodynamics Research and Development Center, Mianyang, Sichuan Province 621000, China (corresponding author). ORCID: https://orcid.org/0009-0001-9054-9624. Email: [email protected]
Peiqing Liu
Professor, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, China.

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