TY - GEN
T1 - Numerical study on sound absorption characteristics of a non-locally reacting liner
AU - Chen, C.
AU - Li, X. D.
AU - Thiele, F.
N1 - Publisher Copyright:
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2017
Y1 - 2017
N2 - For acoustic liners used in commercial nacelles, due to the drainage slots which cut into the partition walls of closely packed cavities, the Helmholtz resonator liners are inevitably not simply locally reacting. Previous investigations confirm that the drainage slots introduce a non-locally reacting behavior which has a significant effect on the absorption spectrum comparing to the equivalent locally reacting liner design. How- ever, the resulting effects of these drainage slots are currently not taken into account during the acoustic liner design process. Therefore, a numerical investigation based on computational aeroacoustic methods (CAA) is carried out to investigate the influence of drainage slots on acoustic attenuation characteristics of liner. Different slot configurations are designed and simulated. Both 2-D and 3-D direct numerical simulations are carried out. Numerical results show that comparing with the locally reacting liner configuration the cell interaction causes an additional dissipation peak which is higher than the Helmholtz resonance and it increases with the size of the slot. Under high sound pressure level incoming waves, the basic characteristics of the spectrum remain. However, vortex shedding transpires at the resonance around both the slits and the drainage slot which generally increases the dissipation and makes the absorption procedure much more intricate. Vorticity contours indicate the connection of two coupled cavities decreases the strength of vortex shedding around the Helmholtz resonance and significantly increases the vorticity magnitude near the additional peak frequency. Finally, an empirical model to predict the extra attenuation peak frequency is derived based on the numerical results.
AB - For acoustic liners used in commercial nacelles, due to the drainage slots which cut into the partition walls of closely packed cavities, the Helmholtz resonator liners are inevitably not simply locally reacting. Previous investigations confirm that the drainage slots introduce a non-locally reacting behavior which has a significant effect on the absorption spectrum comparing to the equivalent locally reacting liner design. How- ever, the resulting effects of these drainage slots are currently not taken into account during the acoustic liner design process. Therefore, a numerical investigation based on computational aeroacoustic methods (CAA) is carried out to investigate the influence of drainage slots on acoustic attenuation characteristics of liner. Different slot configurations are designed and simulated. Both 2-D and 3-D direct numerical simulations are carried out. Numerical results show that comparing with the locally reacting liner configuration the cell interaction causes an additional dissipation peak which is higher than the Helmholtz resonance and it increases with the size of the slot. Under high sound pressure level incoming waves, the basic characteristics of the spectrum remain. However, vortex shedding transpires at the resonance around both the slits and the drainage slot which generally increases the dissipation and makes the absorption procedure much more intricate. Vorticity contours indicate the connection of two coupled cavities decreases the strength of vortex shedding around the Helmholtz resonance and significantly increases the vorticity magnitude near the additional peak frequency. Finally, an empirical model to predict the extra attenuation peak frequency is derived based on the numerical results.
UR - https://www.scopus.com/pages/publications/85085850696
U2 - 10.2514/6.2017-3026
DO - 10.2514/6.2017-3026
M3 - 会议稿件
AN - SCOPUS:85085850696
SN - 9781624105043
T3 - 23rd AIAA/CEAS Aeroacoustics Conference, 2017
BT - 23rd AIAA/CEAS Aeroacoustics Conference, 2017
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 23rd AIAA/CEAS Aeroacoustics Conference, 2017
Y2 - 5 June 2017 through 9 June 2017
ER -