Prediction of Sound Generated by Complex Flows at Low Mach Numbers
Author:
Affiliation:
1. Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.42583
Reference35 articles.
1. On sound generated aerodynamically I. General theory
2. The influence of solid boundaries upon aerodynamic sound
3. Computation of Trailing-Edge Flow and Noise Using Large-Eddy Simulation
4. Trailing-edge noise reduction using derivative-free optimization and large-eddy simulation
5. LES Prediction of Wall-Pressure Fluctuations and Noise of a Low-Speed Airfoil
Cited by 69 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. Comparative experimental studies on flow and noise of cylinder affected by coated and downstream metal foams;Aerospace Science and Technology;2024-10
2. Characteristics of the flow around finite wall-mounted square cylinders and the mechanism of tonal noise;Physics of Fluids;2024-06-01
3. An Improved Boundary Element Method for Predicting Half-Space Scattered Noise Combined with Permeable Boundaries;Advances in Mathematical Physics;2024-05-27
4. Cylinder flow and noise control by active base blowing;Journal of Fluid Mechanics;2024-04-16
5. Hydroacoustics of turbulent flow over superhydrophobic and oscillating cylinders;Ocean Engineering;2024-02
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