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AEROELASTIC-ACOUSTICS SIMULATION OF FLIGHT SYSTEMS

机译:飞行系统的气弹声模拟

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This paper describes the details of a novel numerical finite-element-based analysis procedure and a resulting code for the simulation of the acoustics phenomenon arising from aeroelastic interactions. Both computational fluid dynamics and structural simulations are based on finite element discretisation employing unstructured grids. The sound pressure level on structural surfaces is calculated from the root mean square of the unsteady pressure, and the acoustic-wave frequencies are computed from a fast Fourier transform of the unsteady pressure distribution as a function of time. The newly developed tool proves to be unique, as it is designed to analyze complex practical problems involving computations in a routine fashion.
机译:本文介绍了一种新颖的基于有限元数值分析程序的细节,以及由此产生的代码,用于模拟由气动弹性相互作用引起的声学现象。计算流体动力学和结构模拟均基于采用非结构化网格的有限元离散化。根据非稳态压力的均方根计算结构表面上的声压级,并根据非稳态压力分布随时间的快速傅立叶变换来计算声波频率。新开发的工具被证明是独特的,因为它被设计为以常规方式分析涉及计算的复杂实际问题。

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