Noise Reduction with Fluidic Inserts in Supersonic Jets Exhausting Over a Simulated Aircraft Carrier Deck
Author:
Affiliation:
1. Pennsylvania State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2374
Reference42 articles.
1. Measurements of Jet Noise Aboard US Navy Aircraft Carriers
2. Noise reduction in supersonic jets by nozzle fluidic inserts
3. Noise Reduction Technology for F/A-18 E/F Aircraft
4. Aero-Performance Efficient Noise Reduction for the F404-400 Engine
Cited by 15 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. Impact of an Adjacent Surface on a Rectangular Overexpanded Supersonic Jet;Flow, Turbulence and Combustion;2023-11-06
2. A study of noise reduction mechanisms of jets with fluid inserts;Journal of Sound and Vibration;2020-06
3. Effectiveness of Fluid Injection on Supersonic Jet Noise at High Exhaust Temperatures;AIAA Scitech 2020 Forum;2020-01-05
4. Unsteady Simulations of Fluid Inserts for Supersonic Jet Noise Reduction;AIAA Scitech 2019 Forum;2019-01-06
5. Noise and Noise Reduction in Supersonic Jets;Flinovia—Flow Induced Noise and Vibration Issues and Aspects-II;2018-05-26
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
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3