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SIMULATION OF HIGH RE BOUNDARY LAYER FLOWS USING VORTICITY CONFINEMENT

机译:利用涡度约束模拟高稀土边界层流

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摘要

We describe how Vorticity Confinement (VC) can be regarded as a new pde formulation of the slightly viscous incompressible flow equations. These equations, when discretized and solved, generate nonlinear solitary waves that can be used to efficiently approximate a large class of external flow problems, including the effects of separating turbulent boundary layers. These problems can involve subsonic flow over complex structures such as ships, buildings, and realistic topography such as hills. These problems typically involve the simulation of a large ensemble of flow conditions for each configuration to be designed or analyzed. One of the most difficult aspects of these simulations is that often the main effects of the dynamics of thin evolving vortical structures must be solved for. The VC method appears to be effective for many of these problems, since it requires much less computing and setup time than current Navier Stokes "RANS" approximations. The method involves treating the flow over a solid body as a two-scale problem: The first component is an "outer" smoothly varying, mainly irrotational flow with perhaps large scale vortical components where standard CFD techniques can be used. The second component is composed of thin vortical regions. These vortical parts consist of mostly thin attached boundary layers, thin separating vortex sheets, which roll up and thin vortex filaments, which result from roll up. The VC method involves treating these regions with a single equation that has three equilibrium states corresponding to these regions. The equation allows transition between these equilibrium states so that for example, boundary layers can separate and roll up into vortex filaments, and vortex filaments can join and reconnect with other filaments. These properties survive discretization and require no extra logic. VC can be used to treat the entire flow in a locally-Cartesian computational grid with the solid surfaces "immersed" in the grid so that they can be quickly generated for many configurations. Adaptive or conforming fine scale grid cells are then not required to approximate the thin vortical boundary layers, or thin separating vortex sheets. Instead, vortical structures created with Vorticity Confinement, which are essentially thin, non-diffusing, or confined "Nonlinear Solitary Waves" (NSW's) are used to "carry" the vorticity in these regions. The VC method has the efficiency of panel methods, but the generality and ease of use of fixed grid Euler equation methods. In this paper we concentrate on attached and separating boundary layers; there are already in the literature a large number of papers describing the use of VC for free, convecting vortices.
机译:我们描述了如何将涡度限制(VC)视为微粘性不可压缩流动方程的新pde公式。这些方程式经离散化和求解后,会生成非线性孤波,可用于有效地近似一大类外部流动问题,包括分离湍流边界层的影响。这些问题可能涉及亚音速流过复杂结构(例如船舶,建筑物)和现实地形(例如山丘)的情况。这些问题通常涉及要设计或分析的每种配置的大量流动条件的仿真。这些模拟最困难的方面之一是,通常必须解决薄演化的涡旋结构动力学的主要影响。 VC方法对于其中的许多问题似乎是有效的,因为与当前的Navier Stokes“ RANS”近似值相比,它所需的计算和设置时间要少得多。该方法涉及将固体上的流动视为两个尺度的问题:第一个分量是“外部”平滑变化的,主要是不旋转的流动,可能带有大规模涡旋分量,可以使用标准CFD技术。第二部分由薄的涡旋区组成。这些涡旋部分主要由附着的薄边界层,卷起的分离涡流片和卷起的涡流细丝组成。 VC方法包括用一个方程式处理这些区域,该方程式具有对应于这些区域的三个平衡状态。该方程式允许在这些平衡状态之间进行转换,以便例如边界层可以分离并卷成涡旋丝,而涡旋丝可以连接并与其他细丝重新连接。这些属性在离散化后仍然存在,并且不需要额外的逻辑。 VC可用于处理局部笛卡尔计算网格中的所有流,其中实体表面“沉浸”在网格中,以便可以针对许多配置快速生成它们。这样就不需要自适应或符合要求的精细尺度网格单元来近似薄的涡旋边界层或薄的分离涡旋片。取而代之的是,通过涡度限制创建的涡旋结构基本上是薄的,非扩散的或受约束的“非线性孤波”(NSW's),用于在这些区域“承载”涡旋。 VC方法具有面板方法的效率,但是具有固定网格Euler方程方法的通用性和易用性。在本文中,我们专注于附着和分离的边界层。文献中已经有大量描述免费使用对流涡流的VC的论文。

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