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飞机噪声的产生与评估 第5部分 - 整车系统噪声,第d节 - 声爆

Aircraft Noise Generation and Assessment Section 5-Overall Vehicle System Noise, Part d-Sonic Boom.

作者信息

Page J A, Loubeau A

机构信息

Volpe US National Transportation Systems Center, United States.

National Aeronautics and Space Administration, Langley Research Center, United States.

出版信息

CEAS Aeronaut J. 2019 Mar 13;10(1):335-353. doi: 10.1007/s13272-019-00379-0. Epub 2019 Mar 16.

DOI:10.1007/s13272-019-00379-0
PMID:33505532
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC7837502/
Abstract

There has been a renewed interest globally in civil supersonic overland flight that has fostered numerous research and technology development activities. It is now possible to design a low-boom aircraft with a carefully tailored vehicle shape that controls the far field pressures and minimizes sonic booms on the ground. This section will describe recent international advances and cooperative research in sonic boom design, propagation modeling, and human subjective response in preparation of potential international rule changes that will permit civil supersonic flight over land.

摘要

全球范围内对民用超声速陆上飞行重新产生了兴趣,这推动了众多研究和技术开发活动。现在有可能设计一种具有精心定制的飞行器形状的低爆音飞机,这种形状可以控制远场压力并将地面上的音爆降至最低。本节将描述在音爆设计、传播建模和人类主观反应方面的最新国际进展及合作研究,为可能允许民用超声速陆上飞行的国际规则变化做准备。

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Aircraft Noise Generation and Assessment Section 5-Overall Vehicle System Noise, Part d-Sonic Boom.飞机噪声的产生与评估 第5部分 - 整车系统噪声,第d节 - 声爆
CEAS Aeronaut J. 2019 Mar 13;10(1):335-353. doi: 10.1007/s13272-019-00379-0. Epub 2019 Mar 16.
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本文引用的文献

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Diffraction of sonic booms around buildings resulting in the building spiking effect.建筑物周围的音爆绕射导致建筑物峰值效应。
J Acoust Soc Am. 2011 Mar;129(3):1250-60. doi: 10.1121/1.3543984.
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State of the art of sonic boom modeling.音爆建模的技术现状。
J Acoust Soc Am. 2002 Jan;111(1 Pt 2):530-6. doi: 10.1121/1.1379075.
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Atmospheric turbulence conditions leading to focused and folded sonic boom wave fronts.导致聚焦和折叠音爆波阵面的大气湍流条件。
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