Low-Reynolds-Number Aerodynamic Characteristics of Airfoils with Piezocomposite Trailing Surfaces
Author:
Affiliation:
1. Rutgers University, Piscataway, New Jersey 08854
Funder
Dept. of Energy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061214
Reference16 articles.
1. A Review of Morphing Aircraft
2. A review of modelling and analysis of morphing wings
3. Morphing aircraft based on smart materials and structures: A state-of-the-art review
4. Macro-fiber composite actuators for a swept wing unmanned aircraft
5. Macro-Fiber Composite actuated simply supported thin airfoils
Cited by 5 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. Aerodynamic Modeling and Design Optimization of a Variable-Camber Piezocomposite Rotor;AIAA Journal;2024-09
2. Data-driven transient lift attenuation for extreme vortex gust–airfoil interactions;Journal of Fluid Mechanics;2024-08-10
3. Laminar post-stall wakes of tapered swept wings;Journal of Fluid Mechanics;2023-11-24
4. Optimization of Low Reynolds number airfoil design using Full Inverse Design method;2023-06-05
5. PowerLine Unmanned Surfer (PLUS): Concept and Morphing Flight Dynamics;2023 American Control Conference (ACC);2023-05-31
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