TY - GEN
T1 - A Hydrodynamic/Acoustic Splitting Method with Fluid-structure Feedback for Flowinduced Noise
AU - He, Yanfei
AU - Zhang, Xingwu
AU - Zhang, Tao
AU - Geng, Jia
AU - Wang, Chenxi
AU - Chen, Xuefeng
N1 - Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2022
Y1 - 2022
N2 - A hydrodynamic/acoustic splitting (HAS) method is presented to simulate flow-induced noise in fluid-structure-sound interactions. This method consists of hydrodynamic governing equations and acoustic perturbed equations. The hydrodynamic governing equations are solved by wavelet immersed boundary method (IBM) to calculate fluid and structure fields, which will affect the acoustic propagation. The acoustic perturbed equations are computed by a dispersion-relation-preserving (DRP) difference scheme, as well as a low-dissipation and low-dispersion Runge-Kutta (LDDRK) scheme to acquire the acoustic field precisely. In addition, perfectly matched layers (PML) are constructed by PML governing equations to form no-reflective boundary conditions in the acoustic computation. Finally, two numerical examples, which include sound generation by flow over a cylinder or two parallel cylinders, are calculated to validate the new method is a simple and efficient method for fluid-structuresound interactions.
AB - A hydrodynamic/acoustic splitting (HAS) method is presented to simulate flow-induced noise in fluid-structure-sound interactions. This method consists of hydrodynamic governing equations and acoustic perturbed equations. The hydrodynamic governing equations are solved by wavelet immersed boundary method (IBM) to calculate fluid and structure fields, which will affect the acoustic propagation. The acoustic perturbed equations are computed by a dispersion-relation-preserving (DRP) difference scheme, as well as a low-dissipation and low-dispersion Runge-Kutta (LDDRK) scheme to acquire the acoustic field precisely. In addition, perfectly matched layers (PML) are constructed by PML governing equations to form no-reflective boundary conditions in the acoustic computation. Finally, two numerical examples, which include sound generation by flow over a cylinder or two parallel cylinders, are calculated to validate the new method is a simple and efficient method for fluid-structuresound interactions.
UR - https://www.scopus.com/pages/publications/85122925304
U2 - 10.2514/6.2022-0414
DO - 10.2514/6.2022-0414
M3 - 会议稿件
AN - SCOPUS:85122925304
SN - 9781624106316
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
BT - AIAA SciTech Forum 2022
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Y2 - 3 January 2022 through 7 January 2022
ER -