首页> 外文会议>AIAA 32nd Aerospace Sciences Meeting Exhibit January 10-13, 1994/Reno, NV >Wall Boundary Conditions for High-Order Finite Difference Schemes in Computational Aeroacoustics
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Wall Boundary Conditions for High-Order Finite Difference Schemes in Computational Aeroacoustics

机译:计算航空声学中高阶有限差分方案的壁边界条件

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High order finite difference schemes are less dispersive and dissipative, at the same time, more isotropic than low order schemes. They are well suited for solving computational acoustics problems. High order finite difference equations, however, support extraneous wave solutions which bear no resemblance to the exact solution of the original partial differential equations. These extraneous wave solutions, which invariably degrade the quality of the numerical solutions, are usually generated when solid wall boundary conditions are imposed. A set of numerical boundary conditions simulating the presence of a solid wall for high order finite difference schemes using a minimum number of ghost values is proposed. The effective-ness of the numerical boundary conditions in producing quality solutions is analyzed and demonstrated by comparing the results of direct numerical simulations and exact solutions.
机译:与低阶方案相比,高阶有限差分方案的色散和耗散较小,同时各向同性更高。它们非常适合解决计算声学问题。但是,高阶有限差分方程支持无关的波解,这些波解与原始偏微分方程的精确解没有相似之处。这些外来波解通常会在施加实心壁边界条件时生成,这些解总是会降低数值解的质量。提出了一组数值边界条件,它使用最少数量的幻影值来模拟高阶有限差分方案中实心墙的存在。通过比较直接数值模拟和精确解的结果,分析和证明了数值边界条件在产生优质解中的有效性。

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