On the numerical oscillation of the direct-forcing immersed-boundary method for moving boundaries

被引:125
|
作者
Luo, Haoxiang [1 ]
Dai, Hu [1 ]
de Sousa, Paulo J. S. A. Ferreira [1 ]
Yin, Bo [1 ]
机构
[1] Vanderbilt Univ, Dept Mech Engn, Nashville, TN 37235 USA
基金
美国国家科学基金会;
关键词
Immersed-boundary method; Direct forcing; Moving boundaries; Numerical oscillations; Flapping flight; NAVIER-STOKES EQUATIONS; CARTESIAN GRID METHOD; FLOW PAST SPHERES; INCOMPRESSIBLE FLOWS; SIMULATING FLOWS; INTERFACE METHOD; REYNOLDS-NUMBER; WAKE; HUMMINGBIRD; COMPUTATIONS;
D O I
10.1016/j.compfluid.2011.11.015
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
A family of sharp-interface immersed boundary methods using the so-called "direct forcing" approach have been developed for a range of applications because of their simple formulation and relative ease in handling complex geometries. Numerical interpolations are typically adopted in these methods to approximate the flow variables at the grid points near the solid surface, which provides an implicit force in the flow so that the no-slip and no-penetration conditions are satisfied. When dealing with moving boundaries, however, these methods could be prone to numerical oscillations because the nodal points where the direct forcing is applied may change from one time step to next. Noticing that the oscillations are caused by the instantaneous change of the numerical description at the direct-forcing points, we propose a formulation that allows for a smooth transition of the numerical description at these points. This new formulation preserves the spatial accuracy of the original immersed-boundary formulation and can effectively suppress the force oscillations. In this paper, we present a specific example of such formulation in both two- and three-dimensions and validate the implementation for both fixed and moving boundaries. Finally, a full-body simulation of flapping flight is demonstrated using the proposed method. (C) 2011 Elsevier Ltd. All rights reserved.
引用
收藏
页码:61 / 76
页数:16
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