• 文献检索
  • 文档翻译
  • 深度研究
  • 学术资讯
  • Suppr Zotero 插件Zotero 插件
  • 邀请有礼
  • 套餐&价格
  • 历史记录
应用&插件
Suppr Zotero 插件Zotero 插件浏览器插件Mac 客户端Windows 客户端微信小程序
定价
高级版会员购买积分包购买API积分包
服务
文献检索文档翻译深度研究API 文档MCP 服务
关于我们
关于 Suppr公司介绍联系我们用户协议隐私条款
关注我们

Suppr 超能文献

核心技术专利：CN118964589B侵权必究
粤ICP备2023148730 号-1Suppr @ 2026

文献检索

告别复杂PubMed语法，用中文像聊天一样搜索，搜遍4000万医学文献。AI智能推荐，让科研检索更轻松。

立即免费搜索

文件翻译

保留排版，准确专业，支持PDF/Word/PPT等文件格式，支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述，25分钟生成高质量综述，智能提取关键信息，辅助科研写作。

立即免费体验

相似文献

1
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.
2
Summary of recent NASA studies of human response to sonic booms.美国国家航空航天局（NASA）近期关于人类对音爆反应的研究总结。
J Acoust Soc Am. 2002 Jan;111(1 Pt 2):586-98. doi: 10.1121/1.1371767.
3
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.
4
Loudness and short-term annoyance of sonic boom signatures at low levels.低声爆信号的响度和短期烦恼度在低水平下。
J Acoust Soc Am. 2021 Mar;149(3):2004. doi: 10.1121/10.0003779.
5
Estimating the noise dose range of the NASA X-59 aircraft in supersonic cruise using PCBoom propagation simulations.使用 PCBoom 传播模拟估算 NASA X-59 飞机在超音速巡航中的噪声剂量范围。
JASA Express Lett. 2023 May 1;3(5). doi: 10.1121/10.0019501.
6
A computational analysis of sonic booms penetrating a realistic ocean surface.对穿透实际海洋表面的声爆的计算分析。
J Acoust Soc Am. 2001 Mar;109(3):899-908. doi: 10.1121/1.1346684.
7
Predicting transmission of shaped sonic booms into a residential house structure.预测成形声爆在住宅建筑结构中的传播情况。
J Acoust Soc Am. 2010 Jun;127(6):3347-55. doi: 10.1121/1.3409733.
8
[Changes of pulse rate caused by sonic bomms during sleep (author's transl)].
Eur J Appl Physiol Occup Physiol. 1975 Dec 5;34(4):279-89. doi: 10.1007/BF00999941.
9
Field measurements of sonic boom penetration into the ocean.声爆穿透海洋的现场测量。
J Acoust Soc Am. 2000 Jun;107(6):3073-83. doi: 10.1121/1.429336.
10
Subjective response of people to simulated sonic booms in their homes.
J Acoust Soc Am. 2004 Sep;116(3):1573-84. doi: 10.1121/1.1781189.

本文引用的文献

1
Stability of sonic boom metrics regarding signature distortions from atmospheric turbulence.关于大气湍流引起的信号失真的音爆指标稳定性。
J Acoust Soc Am. 2017 Jun;141(6):EL592. doi: 10.1121/1.4986209.
2
Effects of indoor rattle sounds on annoyance caused by sonic booms.室内拨浪鼓声音对音爆引起的烦恼的影响。
J Acoust Soc Am. 2015 Jul;138(1):EL43-8. doi: 10.1121/1.4922535.
3
A unified approach to an augmented Burgers equation for the propagation of sonic booms.一种用于声爆传播的增强型伯格斯方程的统一方法。
J Acoust Soc Am. 2015 Apr;137(4):1857-66. doi: 10.1121/1.4916833.
4
Laboratory-scale experiment to study nonlinear N-wave distortion by thermal turbulence.
J Acoust Soc Am. 2014 Aug;136(2):556-66. doi: 10.1121/1.4887458.
5
Random focusing of nonlinear acoustic N-waves in fully developed turbulence: laboratory scale experiment.非线性声 N 波在完全发展湍流中的随机聚焦：实验室规模实验。
J Acoust Soc Am. 2011 Dec;130(6):3595-607. doi: 10.1121/1.3652869.
6
Nonlinear and diffraction effects in propagation of N-waves in randomly inhomogeneous moving media.N 波在随机非均匀运动介质中传播的非线性和绕射效应。
J Acoust Soc Am. 2011 Apr;129(4):1760-72. doi: 10.1121/1.3557034.
7
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.
8
COMMUNITY REACTIONS TO SONIC BOOMS IN THE OKLAHOMA CITY AREA. AMRL-TR-65-37.俄克拉荷马城地区对音爆的社区反应。AMRL - TR - 65 - 37。
AMRL TR. 1965 Feb:1-43. doi: 10.21236/ad0613620.
9
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.
10
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。
J Acoust Soc Am. 2002 Jan;111(1 Pt 2):520-9. doi: 10.1121/1.1377631.

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。