Transition Point Detection from the Surface Pressure Distribution for Controller Design
Author:
Affiliation:
1. École de Technologie Supérieure, Montréal, Quebec H3C 1K3 Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.31488
Reference13 articles.
1. Optimized Natural-Laminar-Flow Airfoils
2. Adaptive Airfoils for Drag Reduction at Transonic Speeds
3. Laminar Separation, Transition, and Turbulent Reattachment near the Leading Edge of Airfoils
4. Effects of Flow Separation on Aerodynamic Loads in Linearized Thin Airfoil Theory
Cited by 55 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. Seamless morphing trailing edge flaps for UAS-S45 using high-fidelity aerodynamic optimization;Chinese Journal of Aeronautics;2024-02
2. Physics-Informed Machine Learning for Inverse Airfoil Shape Design;AIAA AVIATION 2023 Forum;2023-06-08
3. A simple boundary-layer transition detection method using mean static pressure measurements;Experiments in Fluids;2023-04
4. New Validation Methodology of an Adaptive Wing for UAV S45 for Fuel Reduction and Climate Improvement;Applied Sciences;2023-01-30
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