Space-time fluid-structure interaction methods

Kenji Takizawa, Tayfun E. Tezduyar*

*この研究の対応する著者

研究成果: Article査読

130 被引用数 (Scopus)

抄録

Since its introduction in 1991 for computation of flow problems with moving boundaries and interfaces, the Deforming-Spatial-Domain/Stabilized SpaceTime (DSD/SST) formulation has been applied to a diverse set of challenging problems. The classes of problems computed include free-surface and two-fluid flows, fluidobject, fluidparticle and fluidstructure interaction (FSI), and flows with mechanical components in fast, linear or rotational relative motion. The DSD/SST formulation, as a core technology, is being used for some of the most challenging FSI problems, including parachute modeling and arterial FSI. Versions of the DSD/SST formulation introduced in recent years serve as lower-cost alternatives. More recent variational multiscale (VMS) version, which is called DSD/SST-VMST (and also ST-VMS), has brought better computational accuracy and serves as a reliable turbulence model. Special spacetime FSI techniques introduced for specific classes of problems, such as parachute modeling and arterial FSI, have increased the scope and accuracy of the FSI modeling in those classes of computations. This paper provides an overview of the core spacetime FSI technique, its recent versions, and the special spacetime FSI techniques. The paper includes test computations with the DSD/SST-VMST technique.

本文言語English
論文番号1230001
ジャーナルMathematical Models and Methods in Applied Sciences
22
SUPPL.2
DOI
出版ステータスPublished - 2012 8

ASJC Scopus subject areas

  • モデリングとシミュレーション
  • 応用数学

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