计算机科学与技术

声道中气动声学问题的光滑粒子动力学模拟

  • 魏建国 ,
  • 韩江 ,
  • 侯庆志 ,
  • 王颂 ,
  • 党建武
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  • 1. 天津大学 软件学院, 天津 300350, 中国;
    2. 天津大学 计算机科学与技术学院, 天津 300350, 中国;
    3. 北陆先端科学技术大学院大学 信息科学学院, 石川923-1292, 日本

收稿日期: 2016-06-24

  网络出版日期: 2016-11-15

SPH simulations of aeroacoustic problems in vocal tracts

  • WEI Jianguo ,
  • HAN Jiang ,
  • HOU Qingzhi ,
  • WANG Song ,
  • DANG Jianwu
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  • 1. School of Computer Software, Tianjin University, Tianjin 300350, China;
    2. School of Computer Science and Technology, Tianjin University, Tianjin 300350, China;
    3. School of Information Science, Japan Advanced Institute of Science and Technology, Ishikawa 923-1292, Japan

Received date: 2016-06-24

  Online published: 2016-11-15

摘要

在人体发音过程仿真中,考虑声道边界的动态变化以及气流的流动,可以更加准确、真实地模拟声波在声道中的传播。在处理带有移动边界的气动声学问题时,相比传统声道声学研究中广泛应用的网格方法,无网格方法可以避免网格重构、网格畸变等。基于Euler体系下的气动声学波动方程,推导了Lagrange体系下声波传播的控制方程,并建立了无网格光滑粒子动力学(smoothed particle hydrodynamics,SPH)方法的数值离散格式。通过对比静止流体中声传播问题的SPH解和时域有限差分(finite difference time domain,FDTD)解,验证了SPH方法在声学计算中的准确性和可靠性。对于一维和二维流动流体中的声传播问题,通过与基于Doppler效应的理论解对比,阐明了利用SPH方法求解复杂气动声学问题的可行性。

本文引用格式

魏建国 , 韩江 , 侯庆志 , 王颂 , 党建武 . 声道中气动声学问题的光滑粒子动力学模拟[J]. 清华大学学报(自然科学版), 2016 , 56(11) : 1242 -1248 . DOI: 10.16511/j.cnki.qhdxxb.2016.26.019

Abstract

Simulation of human sound wave propagation need to take into account the moving boundaries and fluid flow within the vocal tract for accurate realistic models. Traditional mesh-based methods that are widely used to study human sound production have many problems due to mesh reconstruction and distortion, so they are not as effective as meshless methods. The aeroacoustic wave equations in the Eulerian framework are transformed to the governing equations for wave propagation in the Lagrangian form and discretized using the smoothed particle hydrodynamics (SPH) method. The accuracy and reliability of SPH for wave propagation in a static media are shown by comparisons with finite difference time domain (FDTD) results. This method is validated against the Doppler effect based theoretical solutions for one-and two-dimensional aeroacoustics to verify the ability of SPH to solve complex aeroacoustic problems.

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