Further Invesitgation of Modeling Limit Cycle Oscillation Behavior of the F-16 Fighter Using a Harmonic Balance Approach
Author:
Affiliation:
1. Duke University
2. Eglin Air Force Base
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1917
Reference11 articles.
1. Computation of Unsteady Nonlinear Flows in Cascades Using a Harmonic Balance Technique
2. Nonlinear Inviscid Aerodynamic Effects on Transonic Divergence, Flutter, and Limit-Cycle Oscillations
3. 4Thomas, J. P., Dowell, E. H., and Hall, K. C. "Modeling Viscous Transonic Limit Cycle Oscillation Behavior Using a Harmonic Balance Approach," AIAA Paper 2002-1414.
4. 5Thomas, J. P., Dowell, E. H., and Hall, K. C. "A Harmonic Balance Approach for Modeling Three-Dimensional Nonlinear Unsteady Aerodynamics and Aeroelasticity," ASME Paper IMECE-2002-32532.
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. Shock migration on an oscillating straked delta wing using an unsteady Euler solver;Journal of Fluids and Structures;2023-10
2. Methodology for Numerically Stabilizing a Harmonic-Balance-Based Forced Response Aeroelastic Solution Approach;AIAA Journal;2023-02
3. Aeroelastic Modeling of the AGARD 445.6 Wing Using the Harmonic-Balance-Based One-Shot Method;AIAA Journal;2019-11
4. Efficient Aeroelastic Solution Based on Time-Spectral Fluid–Structure Interaction Method;AIAA Journal;2019-07
5. A novel approach for flutter prediction of pitch–plunge airfoils using an efficient one-shot method;Journal of Fluids and Structures;2018-10
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