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DAMAS Processing for a Phased Array Study in the NASA Langley Jet Noise Laboratory

机译:在美国宇航局Langley喷气噪声实验室进行相控阵研究的DAMAS处理

摘要

A jet noise measurement study was conducted using a phased microphone array system for a range of jet nozzle configurations and flow conditions. The test effort included convergent and convergent/divergent single flow nozzles, as well as conventional and chevron dual-flow core and fan configurations. Cold jets were tested with and without wind tunnel co-flow, whereas, hot jets were tested only with co-flow. The intent of the measurement effort was to allow evaluation of new phased array technologies for their ability to separate and quantify distributions of jet noise sources. In the present paper, the array post-processing method focused upon is DAMAS (Deconvolution Approach for the Mapping of Acoustic Sources) for the quantitative determination of spatial distributions of noise sources. Jet noise is highly complex with stationary and convecting noise sources, convecting flows that are the sources themselves, and shock-related and screech noise for supersonic flow. The analysis presented in this paper addresses some processing details with DAMAS, for the array positioned at 90 (normal) to the jet. The paper demonstrates the applicability of DAMAS and how it indicates when strong coherence is present. Also, a new approach to calibrating the array focus and position is introduced and demonstrated.
机译:使用相控麦克风阵列系统对一系列喷嘴配置和流量条件进行了喷射噪声测量研究。测试工作包括会聚和会聚/发散单流喷嘴,以及常规和人字形双流芯和风扇配置。冷射流在有风洞并流的情况下进行测试,而热射流仅在有风道并流的情况下进行测试。测量工作的目的是允许评估新的相控阵技术分离和量化喷射噪声源分布的能力。在本文中,阵列后处理方法是DAMAS(用于声源映射的去卷积方法),用于定量确定噪声源的空间分布。射流噪声非常复杂,包括固定和对流噪声源,对流本身就是对流,以及与超声流有关的与冲击有关的尖叫声。本文介绍的分析解决了DAMAS的一些处理细节,即阵列位于射流90度(法线)处。本文演示了DAMAS的适用性,以及它如何指示何时存在强一致性。此外,还介绍并演示了一种校准阵列焦点和位置的新方法。

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