Analysis of Fluid-Structure Interaction by Means of Dynamic Unstructured Meshes

F. Blom, P. Leyland
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引用次数: 33

Abstract

This paper presents a computational analysis on forced vibration and fluid-structure interaction in compressible flow regimes. A so-called staggered approach is pursued where the fluid and structure are integrated in time by distinct solvers. Their interaction is then taken into account by a coupling algorithm. The unsteady fluid motion is simulated by means of an explicit time-accurate solver. For the fluid-structure interaction problems which are considered here the effects due to the viscosity can be neglected. The fluid is hence modeled by the Euler equations for compressible inviscid flow. Unstructured grids are used to discretise the fluid domain. These grids are particularly suited to simulate unsteady flows over complex geometries by their capacity of being dynamically refined and derefined. Dynamic mesh adaptation is used to enhance the computational precision with minimal CPU and memory constraints. Fluid-structure interaction involves moving boundaries. Therefore the Arbitrary Lagrange Euler method (ALE-method) is adopted to solve the Euler equations on a moving domain. The deformation of the mesh is controlled by means of a spring analogy in conjunction with a boundary correction to circumvent the principle of Saint Venant. To take advantage of the differences between fluid and structure time scales, the fluid calculation is subcycled within the structural time step. Numerical results are presented for large rotation, pitching oscillation and aeroelastic motion of the NACA0012 airfoil. The boundary deformation is validated by comparing the numerical solution for a flat plate under supersonic flow with the analytical solution.
基于动态非结构网格的流固耦合分析
本文对可压缩流型中的强迫振动和流固耦合进行了计算分析。采用所谓的交错方法,其中流体和结构通过不同的求解器在时间上集成。然后通过耦合算法考虑它们的相互作用。采用显式时准求解器对非定常流体运动进行了模拟。对于这里所考虑的流固相互作用问题,粘度的影响可以忽略不计。因此,流体是用可压缩无粘流的欧拉方程来模拟的。非结构化网格用于离散流体域。这些网格特别适合于模拟复杂几何形状的非定常流,因为它们具有动态细化和定义的能力。采用动态网格自适应技术,在最小的CPU和内存约束下提高计算精度。流固耦合涉及移动边界。因此,采用任意拉格朗日欧拉法(ALE-method)求解运动域上的欧拉方程。网格的变形通过弹簧类比和边界校正来控制,以规避圣维南原理。为了利用流体和结构时间尺度的差异,流体计算在结构时间步长内进行了次循环。给出了NACA0012翼型大旋转、俯仰振荡和气动弹性运动的数值计算结果。通过数值解与解析解的比较,验证了超声速流动条件下平板边界变形的正确性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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