Experimental Validation of a Semi-Analytical Trailing-Edge Noise Model Including Broadband Scattering
Author:
Affiliation:
1. von Kármán Institute for Fluid Dynamics
2. University of Sherbrooke
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2531
Reference50 articles.
1. On the Use of Embedded Meshes in the LES of External Flows
2. Acoustic radiation from an airfoil in a turbulent stream
3. Noise due to turbulent flow past a trailing edge
4. Numerical Solution of Acoustic Propagation Problems Using Linearized Euler Equations
Cited by 6 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. On a three-dimensional investigation of airfoil turbulence-impingement noise and its reduction by leading-edge tubercles;Journal of Sound and Vibration;2022-03
2. Turbulent boundary layer trailing-edge noise: Theory, computation, experiment, and application;Progress in Aerospace Sciences;2021-10
3. Direct Numerical Simulation of the Self-Noise Radiated by the Installed Controlled-Diffusion Airfoil at Transitional Reynolds Number;2018 AIAA/CEAS Aeroacoustics Conference;2018-06-24
4. Direct Numerical Simulation of Transitional Airfoil Noise;23rd AIAA/CEAS Aeroacoustics Conference;2017-06-02
5. Aeroacoustic Simulations of a Simplified High-Lift Device Accounting for Some Installation Effects;AIAA Journal;2017-03
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