4.7 Article

An immersed boundary method with implicit body force for compressible viscous flow

期刊

JOURNAL OF COMPUTATIONAL PHYSICS
卷 459, 期 -, 页码 -

出版社

ACADEMIC PRESS INC ELSEVIER SCIENCE
DOI: 10.1016/j.jcp.2022.111125

关键词

Immersed boundary method; Stress/heat flux boundary conditions; Porous boundary; Compressible flow

资金

  1. NASA [NNX17AD10G]
  2. NASA [1003267, NNX17AD10G] Funding Source: Federal RePORTER

向作者/读者索取更多资源

This paper introduces a new immersed boundary method for simulating compressible viscous flow, which adds surface singularities to the governing equations. Generalizing from the well-known no-slip and isothermal condition to stress and heat flux conditions, as well as extending to porous surfaces, the method is applicable to flow-structure interaction problems.
We present a new immersed boundary method for the simulation of compressible viscous flow. The method is based on the singular source approach where the immersed boundary adds surface singularities to the governing equations. The strengths of the surface singularities are treated as algebraic variables under the framework of differential-algebraic equations and are implicitly calculated to enforce the corresponding boundary conditions. Discrete delta functions are used to approximate the surface singularities in the Eulerian grid and interpolate variables back to the surface mesh. A half-explicit Runge-Kutta method is used to achieve desired temporal accuracy. The method has been generalized from the well-known no-slip and isothermal condition to stress and heat flux conditions. The latter necessitates the introduction of further singularities in the stresses and heat flux, which is a new feature of the formulation. Furthermore, the approach has been extended to porous surfaces. The method is also applicable to flow-structure interaction problems. Two-and three-dimensional numerical tests are carried out to demonstrate accuracy. The results are compared with previous numerical and experimental studies or analytical solutions. Finally, a fully three-dimensional fluid-structure interaction simulation of a subsonic parachute is showcased to demonstrate applicability to a real problem. (C) 2022 Elsevier Inc. All rights reserved.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.7
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

暂无数据
暂无数据