Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Mechanics of Materials,Aerospace Engineering
Reference208 articles.
1. A doublet lattice method for calculating lift distributions on oscillating surfaces in subsonic flow;Albano;AIAA Journal,1969
2. Kier TM. Comparison of unsteady aerodynamic modelling methodologies with respect to flight loads analysis. In: AIAA atmospheric flight mechanics conference, AIAA 2005-6027, San Francisco, CA, USA, 2005.
3. Lucia DJ. The SensorCraft configurations: a non-linear aeroservoelastic challenge for aviation. In: 46th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference, Austin, TX, United States, 2005. pp. 1768–74, AIAA Paper 2005-1943.
4. Nonlinear flight dynamics of very flexible aircraft;Shearer;Journal of Aircraft,2007
5. Aeroelastic characteristics of a highly flexible aircraft;van Schoor;Journal of Aircraft,1990
Cited by 221 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. Unsteady Lifting-Line Free-Wake Aerodynamic Modeling for Morphing Wings;Aerospace;2024-09-11
2. Implementation and Linearization of a Coupled Panel and Vortex Particle Method in State-Space Form;AIAA Journal;2024-09
3. Analytical Linearization of Aerodynamic Loads in Unsteady Vortex-Lattice Method for Nonlinear Aeroelastic Applications;AIAA Journal;2024-08-23
4. Unsteady Lifting-Line Theory for Camber Morphing Wings State-Space Aeroelastic Modeling;AIAA Journal;2024-08-23
5. Accelerating aeroelastic UVLM simulations by inexact Newton algorithms;Computational Mechanics;2024-05-25
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