Numerical Virtual Flight Simulation of Quasi-Cobra Maneuver of a Fighter Aircraft-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Numerical Virtual Flight Simulation of Quasi-Cobra Maneuver of a Fighter Aircraft

Published:2021-01 Issue:1 Volume:58 Page:138-152
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Wang Nianhua¹,Ma Rong²,Chang Xinghua³,Zhang Laiping³

Affiliation:

1. State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, 621000 Mianyang, People’s Republic of China

2. China Aerodynamics Research and Development Center, 621000 Mianyang, People’s Republic of China

3. National Innovation Institute of Defense Technology, 100071 Beijing, People’s Republic of China

Funder

National Natural Science Foundation of China

Chinese National Key Research and Development Program

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference32 articles.

1. Sources of High Alpha Vortex Asymmetry at Zero Sideslip

2. Challenges in high-alpha vehicle dynamics

3. Detached Eddy Simulation of Complex Separation Flows Over a Modern Fighter Model at High Angle of Attack

4. A CFD-based numerical virtual flight simulator and its application in control law design of a maneuverable missile model

5. Vehicle Design of a Sharp CTV Concept Using a Virtual Flight Rapid Integration Test Environment

Cited by 9 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. Numerical virtual flight investigation for longitudinal maneuver of a generic fighter based on machine learning;Physics of Fluids;2024-07-01

2. Altering flight stability characteristics of a high-performance aircraft through wing strake modification;The Aeronautical Journal;2024-04-18

3. Dynamic characteristics of a dual-rotor system subject to foundation excitation;2023 IEEE International Conference on Mechatronics and Automation (ICMA);2023-08-06

4. An intelligent control method based on artificial neural network for numerical flight simulation of the basic finner projectile with pitching maneuver;Defence Technology;2023-07

5. Aerodynamic Identification and Control Law Design of a Missile Using Machine Learning;AIAA Journal;2023-07

同舟云学术

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