4.7 Article

An immersed boundary method for fluid-structure interaction with compressible multiphase flows

期刊

JOURNAL OF COMPUTATIONAL PHYSICS
卷 346, 期 -, 页码 131-151

出版社

ACADEMIC PRESS INC ELSEVIER SCIENCE
DOI: 10.1016/j.jcp.2017.06.008

关键词

Fluid-structure interaction; Immersed-boundary method; Viscous compressible flow; Multiphase flow; Large structure deformations; Shock wave

资金

  1. Australian Research Council Discovery Early Career Researcher Award [DE160101098]
  2. International Graduate Exchange Program of Beijing Institute of Technology
  3. Early Career Researcher Grants Scheme, UNSW Canberra

向作者/读者索取更多资源

This paper presents a two-dimensional immersed boundary method for fluid-structure-interaction with compressible multiphase flows involving large structure deformations. This method involves three important parts: flow solver, structure solver and fluid-structure interaction coupling. In the flow solver, the compressible multiphase Navier-Stokes equations for ideal gases are solved by a finite difference method based on a staggered Cartesian mesh, where a fifth-order accuracy Weighted Essentially Non-Oscillation (WENO) scheme is used to handle spatial discretization of the convective term, a fourth-order central difference scheme is employed to discretize the viscous term, the third-order TVD Runge-Kutta scheme is used to discretize the temporal term, and the level-set method is adopted to capture the multi-material interface. In this work, the structure considered is a geometrically non-linear beam which is solved by using a finite element method based on the absolute nodal coordinate formulation (ANCF). The fluid dynamics and the structure motion are coupled in a partitioned iterative manner with a feedback penalty immersed boundary method where the flow dynamics is defined on a fixed Lagrangian grid and the structure dynamics is described on a global coordinate. We perform several validation cases ( including fluid over a cylinder, structure dynamics, flow induced vibration of a flexible plate, deformation of a flexible panel induced by shock waves in a shock tube, an inclined flexible plate in a hypersonic flow, and shock induced collapse of a cylindrical helium cavity in the air), and compare the results with experimental and other numerical data. The present results agree well with the published data and the current experiment. Finally, we further demonstrate the versatility of the present method by applying it to a flexible plate interacting with multiphase flows. (C) 2017 Elsevier Inc. All rights reserved.

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