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Unstructured grid solution of the eikonal equation for acoustics

机译:声学方程方程的非结构网格解

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摘要

An acoustic eikonal equation solution procedure, that is easy to implement in unstructured grid Navier-Stokes equation flow solvers, is outlined. The approach is readily parallelizable. The method is tested for the following canonical point source cases: quiescent flow; subsonic uniform flow; supersonic uniform flow and an idealized jet flow. Then, as further validation, sound propagation of a wave front through a viscous vortex is considered. For these cases, encouraging agreement is found with analytic data and a high-fidelity numerical solution of the Euler equations. Finally, as demonstration cases, the use of the approach to study the shielding of noise from a planar jet is considered along with wave propagation in a complex three-dimensional geometry. At lower Mach numbers (<0.25), for complex geometries, robust multigrid convergence acceleration is found.
机译:概述了一种声学方程方程求解方法,该方法易于在非结构化网格Navier-Stokes方程流动求解器中实施。该方法易于并行化。该方法针对以下典型点源情况进行了测试:静态流;亚音速均匀流超音速均匀流和理想射流。然后,作为进一步的验证,考虑了波前通过粘性涡旋的声音传播。对于这些情况,在解析数据和Euler方程的高保真数值解中找到令人鼓舞的一致性。最后,作为演示案例,考虑了使用该方法研究平面喷气飞机的噪声屏蔽以及在复杂的三维几何中传播波的方法。在较低的马赫数(<0.25)下,对于复杂的几何图形,可以找到鲁棒的多网格收敛加速。

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