TY - JOUR
T1 - Low-frequency sound attenuation by coiled-up meta-liner with nonuniform cross sections under grazing flow
AU - Wang, Hao
AU - Zeng, Xiangyang
AU - Ren, Shuwei
AU - Xue, Dongwen
AU - Li, Zhuohan
AU - Wang, Haitao
AU - Lei, Ye
N1 - Publisher Copyright:
© 2024 Author(s).
PY - 2024/5/28
Y1 - 2024/5/28
N2 - We report a kind of coiled-up meta-liners with nonuniform cross sections (CMNC), which can efficiently attenuate low-frequency sound waves under grazing flow with a deep subwavelength thickness (e.g., ∼λ/17 at 500 Hz). At a grazing flow Mach number of 0.26, the average transmission loss of the meta-liner is 12.6 dB at 500-1000 Hz, which is twice as much as that of a double-degree-of-freedom acoustic liner of the same size. Physically, the nonuniform cross-sectional distribution and significant cross-sectional area ratio enhances vortex shedding, thus resulting in severe acoustic energy dissipation. The excellent low-frequency acoustic attenuation performance of CMNC is investigated thoroughly with experimental, theoretical, and numerical methods. This work provides an avenue for low-frequency noise reduction in grazing flow scenarios (e.g., in a high bypass ratio turbofan engine).
AB - We report a kind of coiled-up meta-liners with nonuniform cross sections (CMNC), which can efficiently attenuate low-frequency sound waves under grazing flow with a deep subwavelength thickness (e.g., ∼λ/17 at 500 Hz). At a grazing flow Mach number of 0.26, the average transmission loss of the meta-liner is 12.6 dB at 500-1000 Hz, which is twice as much as that of a double-degree-of-freedom acoustic liner of the same size. Physically, the nonuniform cross-sectional distribution and significant cross-sectional area ratio enhances vortex shedding, thus resulting in severe acoustic energy dissipation. The excellent low-frequency acoustic attenuation performance of CMNC is investigated thoroughly with experimental, theoretical, and numerical methods. This work provides an avenue for low-frequency noise reduction in grazing flow scenarios (e.g., in a high bypass ratio turbofan engine).
UR - http://www.scopus.com/inward/record.url?scp=85194156256&partnerID=8YFLogxK
U2 - 10.1063/5.0203941
DO - 10.1063/5.0203941
M3 - 文章
AN - SCOPUS:85194156256
SN - 0021-8979
VL - 135
JO - Journal of Applied Physics
JF - Journal of Applied Physics
IS - 20
M1 - 203107
ER -