Multifidelity Modeling of Deployable Wings: Multibody Dynamic Simulation and Wind Tunnel Experiment
Author:
Affiliation:
1. Tohoku University, Sendai 980-8579, Japan
2. University of Warwick, Coventry CV4 7AL, United Kingdom
3. Tohoku University, Sendai 980-8577, Japan
Funder
Institute of Fluid Science, Tohoku University
Japan Society for the Promotion of Science
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference34 articles.
1. Nonlinear Aeroelastic Study for Folding Wing Structures
2. Design of the ARES Mars Airplane and Mission Architecture
3. Comparing Aerial-Deployment-Mechanism Designs for Mars Airplane
4. Never-EVER Land - A Titan Flyer Concept
5. Optimal Flight Planning for a Z-Shaped Morphing-Wing Solar-Powered Unmanned Aerial Vehicle
Cited by 24 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. Hamel's field variational integrator for simulating dynamics of thin-walled geometrically exact beams with warping effects;Mechanism and Machine Theory;2023-12
2. Multibody Constraints in the Geometrically Nonlinear Intrinsic Formulation;Journal of Computational and Nonlinear Dynamics;2023-10-26
3. Moving Morphable Multi Components Introducing Intent of Designer in Topology Optimization;AIAA Journal;2023-04
4. Hamiltonian formulation with reduced variables for flexible multibody systems under linear constraints: Theory and experiment;Journal of Sound and Vibration;2023-03
5. Analysis-Oriented Moving Morphable Components for Topology Optimization;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