Effect of Deflector Shape on Acoustic Field of Launch Vehicle at Lift-Off-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Effect of Deflector Shape on Acoustic Field of Launch Vehicle at Lift-Off

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Tsutsumi Seiji¹,Kato Susumu¹,Fukuda Kota¹,Takaki Ryoji¹,Ui Kyoichi¹

Affiliation:

1. Japan Aerospace Exploration Agency

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-328

Reference17 articles.

1. 1Eldred,K.M.,andetal."AcousticLoadsGeneratedbythePropulsionSystem,"NASASP-8072,June1971.

Cited by 17 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Supersonic jet noise from launch vehicles: 50 years since NASA SP-8072;The Journal of the Acoustical Society of America;2022-02

2. Lunar PAD - On the Development of a Unique ISRU-Based Planetary Landing Pad for Cratering and Dust Mitigation;AIAA Scitech 2021 Forum;2021-01-04

3. Acoustic Wave Generation from Two-Dimensional Supersonic Inviscid Jet Impinging on Inclined Plate;AIAA Journal;2020-08

4. Spectral Analysis of the Acoustic Near Field of a Solid-Propellant Rocket;AIAA Journal;2018-03

5. Numerical Aspects of Rocket Lift-off Noise with Launch-Pad Aqueous Injection;2018 AIAA Aerospace Sciences Meeting;2018-01-07

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线，采集、加工和组织学术论文而形成的新型学术文献查询和分析系统，可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容，当前同舟云学术共收录了国内外主流学术期刊6万余种，收集的期刊论文及会议论文总量共计约1.5亿篇，并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询！咨询电话：010-8811{复制后删除}0370

www.globalauthorid.com

TOP