Effect of Inertial and Constitutive Properties on Body-Freedom Flutter for Flying Wings
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332
2. University of California, Los Angeles, Los Angeles, California 90095
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033435
Reference28 articles.
1. Nonlinear aeroelasticity and flight dynamics of High-Altitude Long-Endurance aircraft
2. LIMIT-CYCLE OSCILLATIONS IN HIGH-ASPECT-RATIO WINGS
3. Basis Vector Quantification of Flutter Analysis Structural Modes
4. Body Freedom Flutter of High Aspect Ratio Flying Wings
5. An Optimization Method for the Determination of the Important Flutter Modes
Cited by 17 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. Time-Domain Analysis of Body Freedom Flutter Based on 6DOF Equation;Computer Modeling in Engineering & Sciences;2024
2. Design and Feasibility Study of Novel Flying Wing Carrier for Launching Small Satellites in Low Earth Orbit;Applied Sciences;2023-04-08
3. Aeroelasticity of Very Flexible Aircraft: Prof. Dewey Hodges’ Three-decade Contributions to the Field;AIAA SCITECH 2023 Forum;2023-01-19
4. Investigating Low-Dimensional Representations for Body Freedom Flutter;AIAA SCITECH 2023 Forum;2023-01-19
5. Flutter Analysis of Space Solar Power Satellite Under Thermal Loading;AIAA Journal;2022-09
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