Overview of Unsteady Aerodynamic Response of Rigid Wings in Gust Encounters
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
2. Istanbul Technical University, 34469 Istanbul, Turkey
Funder
Air Force Office of Scientific Research
National Science Foundation
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J059602
Reference42 articles.
1. “Dynamic Gust Loads,” U.S. Dept. of Transportation, Federal Aviation Administration Advisory Circular 25.341-1, Dec. 2014.
2. Some Aspects of Non-Stationary Airfoil Theory and Its Practical Application
3. The Aerodynamic Force on an Airfoil in a Moving Gust
4. Airfoil Theory for Flows of Variable Velocity
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. Navigating vortex gust interactions and mitigations by plunging wings;Physics of Fluids;2024-01-01
2. Analysis of Flowfield Vortex Interactions of Nonlinear Sharp-Edged Transverse Gusts;AIAA AVIATION 2023 Forum;2023-06-08
3. Dimensional analysis of a transverse gust encounter;Aerospace Science and Technology;2023-06
4. Review of rotating wing dynamic stall: Experiments and flow control;Progress in Aerospace Sciences;2023-02
5. 低レイノルズ数領域において乱れ強さがNACA0012翼空力特性の非線形性に及ぼす影響;AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2023
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