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Computational Aeroacoustics: Issues and Methods

机译:计算航空声学:问题和方法

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摘要

Computational Fluid Dynamics (CFD) has made tremendous progress especially in aerodynamics and aircraft design over the past 20 years. An obvious question to ask in "why not use CFD methods to solve aeroacoustics problems?". Most aerodynamics problems are time independent whereas aeroacoustics problems are, by definition, time dependent. The nature, characteristics and objectives of aeroacoustics problems are also quite different from the commonly encountered CFD problems. There are computational issues that are unique to aeroacoustics. For these reasons computational aeroacoustics requires somewhat independent thinking and development. The objectives of this paper are twofold. First, issues pertinent to aeroacoustics that may or may not be relevant to computational aerodynamics are discussed. The second objective is to review computational methods developed recently which are designed especially for computational aeroacoustics applications. Some of the computational methods to be reviewed are quite different from traditional CFD methods. They should be of interest to the CFD and fluid dynamics communities.
机译:在过去的20年中,计算流体动力学(CFD)取得了巨大进步,尤其是在空气动力学和飞机设计方面。 “为什么不使用CFD方法解决航空声学问题?”是一个显而易见的问题。大多数空气动力学问题是与时间无关的,而根据定义,空气声学问题是与时间相关的。航空声学问题的性质,特征和目标也与通常遇到的CFD问题大不相同。存在航空声学特有的计算问题。由于这些原因,计算航空声学需要一定程度的独立思考和发展。本文的目的是双重的。首先,讨论了与空气声学相关的问题,这些问题可能与计算空气动力学无关。第二个目的是回顾最近开发的专门用于计算航空声学应用的计算方法。一些需要审查的计算方法与传统的CFD方法大不相同。 CFD和流体动力学界应该对它们感兴趣。

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