TY - GEN
T1 - Trailing edge noise reduction using velvety serrations
AU - Zhou, Peng
AU - Li, Xiangtian
AU - Li, Yuhong
AU - Jiang, Hanbo
AU - Guo, Jingwen
AU - Zhong, Siyang
AU - Zhang, Xin
AU - Angland, David
N1 - Funding Information:
This work is supported by the National Natural Science Foundation of China (NSFC11972029) and the Hong Kong Research Grants Council (GRF16202520, GRF16204721). This work was performed in Aerodynamics, Acoustics & Noise control Technology Centre (aantc.ust.hk).
Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA., All rights reserved.
PY - 2022/6
Y1 - 2022/6
N2 - This work studies the trailing edge noise reduction potentials of combining trailing edge serrations and porous membrane/velvet structures made of non-woven fabrics. Anechoic wind tunnel experiments were conducted based on a flat plate model, at a chord-based Reynolds number between 2 × 105 and 5 × 105 and zero angle of attack, with fully tripped boundary layers. Different alignment conditions between the serrations and the undisturbed wake flow were tested. It was observed that the noise reduction capability of the conventional serrations deteriorates significantly when the serrations were misaligned with the flow, while the performances of the combined structures were only slightly affected by misalignment. The porous membrane structure was found to generate extra high-frequency noise, while the porous velvet structure effectively suppressed the high-frequency noise. In addition, porous velvet structures with serrated trailing edge provided additional noise reduction at lower frequencies, which is likely due to the additional destructive interference at the serrated end of the porous velvet structure. The optimal combination could achieve approximately 10 dB noise reduction in a wide frequency range, in both flow-aligned and flow-misaligned conditions. Further hotwire wake survey revealed the possible mechanisms for the additional noise reduction capability of the combined treatments.
AB - This work studies the trailing edge noise reduction potentials of combining trailing edge serrations and porous membrane/velvet structures made of non-woven fabrics. Anechoic wind tunnel experiments were conducted based on a flat plate model, at a chord-based Reynolds number between 2 × 105 and 5 × 105 and zero angle of attack, with fully tripped boundary layers. Different alignment conditions between the serrations and the undisturbed wake flow were tested. It was observed that the noise reduction capability of the conventional serrations deteriorates significantly when the serrations were misaligned with the flow, while the performances of the combined structures were only slightly affected by misalignment. The porous membrane structure was found to generate extra high-frequency noise, while the porous velvet structure effectively suppressed the high-frequency noise. In addition, porous velvet structures with serrated trailing edge provided additional noise reduction at lower frequencies, which is likely due to the additional destructive interference at the serrated end of the porous velvet structure. The optimal combination could achieve approximately 10 dB noise reduction in a wide frequency range, in both flow-aligned and flow-misaligned conditions. Further hotwire wake survey revealed the possible mechanisms for the additional noise reduction capability of the combined treatments.
UR - http://www.scopus.com/inward/record.url?scp=85135017548&partnerID=8YFLogxK
U2 - 10.2514/6.2022-2893
DO - 10.2514/6.2022-2893
M3 - Conference article published in proceeding or book
AN - SCOPUS:85135017548
SN - 9781624106644
T3 - 28th AIAA/CEAS Aeroacoustics Conference, 2022
BT - 28th AIAA/CEAS Aeroacoustics Conference, 2022
PB - American Institute of Aeronautics and Astronautics Inc. (AIAA)
T2 - 28th AIAA/CEAS Aeroacoustics Conference, 2022
Y2 - 14 June 2022 through 17 June 2022
ER -