Revisiting Conventional Flaps at High Deflection Rate
Author:
Funder
US Air Force Research Lab
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055754
Reference21 articles.
1. Issues in active flow control: theory, control, simulation, and experiment
2. The control of flow separation by periodic excitation
3. High-Fidelity Simulations of Transitional Airfoil Interacting with Canonical Upstream Flow Disturbances
4. Scaling Vehicle Dynamics and Fluid Dynamics in Gusting Flows
5. Modeling and Experiment of Leading Edge Separation Control Using SDBD Plasma Actuators
Cited by 21 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. Closed-loop computational fluid dynamics simulations with time-varying boundary conditions for circulation control;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-07-18
2. Inviscid modeling of unsteady morphing airfoils using a discrete-vortex method;Theoretical and Computational Fluid Dynamics;2023-12-07
3. Dynamic Response of Circulation Control for Step and Sinusoidal Inputs;Journal of Aircraft;2023-11
4. Exploring the Impact of Rapidly Actuated Control Surfaces on Drone Aerodynamics;Drones;2023-07-27
5. Numerical Investigation of a Dynamically Morphing UAS-S45 Wing Airfoil at moderate Reynolds number;AIAA SCITECH 2023 Forum;2023-01-19
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