Tone-like noise from an isolated two dimensional airfoil
Author:
Affiliation:
1. Mitsubishi Electric Corp., Amagasaki, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1986-1947
Reference18 articles.
1. Broad band noise from an isolated two dimensional airfoil
2. A review of the theory of trailing edge noise
3. Comparison of broadband noise mechanisms, analyses, and experiments on rotors
4. and 1984,
5. Trailing edge noise prediction from measured surface pressures
Cited by 14 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. Experimental investigation of the laminar boundary layer vortex-shedding noise by an airfoil within a closed-vein wind tunnel;International Journal of Aeroacoustics;2022-11
2. Airfoil dual acoustic feedback mechanisms at low-to-moderate Reynolds number;2018 AIAA/CEAS Aeroacoustics Conference;2018-06-24
3. Control of trailing-edge noise from airfoil using a plasma actuator;Journal of Fluid Science and Technology;2018
4. Suppression of Tonal Trailing-Edge Noise From an Airfoil Using a Plasma Actuator;AIAA Journal;2013-07
5. Study of tonal noise behavior of an airfoil by using parabolized stability equations;Theoretical and Computational Fluid Dynamics;2012-01-05
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