Effects of Perpendicular Blade-Vortex Interaction, Part 2: Parameter Study
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061-0203
2. Florida Atlantic University, Boca Raton, Florida 33431
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.7528
Reference5 articles.
1. Main Rotor Broadband Noise Study in the DNW
2. Effects of Perpendicular Blade-Vortex Interaction, Part 1: Turbulence Structure and Development
3. The structure and development of a wing-tip vortex
4. Prediction of blade wake interaction noise based on a turbulent vortex model
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. High-fidelity simulation of the interaction between a blade cascade and an ingested vortex;Aerospace Science and Technology;2024-09
2. Blade-Wake Interaction Noise for Small Hovering Rotors, Part I: Characterization Study;AIAA Journal;2023-05
3. Physics-informed Broadband Noise Source Identification and Prediction of an Ideally Twisted Rotor;AIAA Scitech 2021 Forum;2021-01-04
4. Underlying mechanisms of propeller wake interaction with a wing;Journal of Fluid Mechanics;2020-12-03
5. Multiple-Fidelity Modeling of Interactional Aerodynamics;Journal of Aircraft;2018-09
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