Design method of controllability of low aspect-ratio flying wing configuration combat aircraft

被引：0
|
作者：
School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China [1 ]
机构：
来源：
Hangkong Xuebao | 2008年 / 4卷 / 788-794期
关键词：
Control surfaces;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [1] Directional axis flying qualities assessment of low aspect-ratio combat flying wings
    School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
    [J]. Hangkong Xuebao, 2009, 6 (972-978):
  • [2] Stability features of low aspect-ratio flying wings
    Li, Lin
    Ma, Chao
    Wang, Lixin
    [J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2007, 28 (06): : 1312 - 1317
  • [3] Vortex control in low aspect ratio flying wing
    School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
    [J]. Kongqi Donglixue Xuebao, 2008, 4 (435-439):
  • [4] Investigation on combined control surfaces for the yaw control of low aspect ratio flying wing configuration
    Zhang, Binqian
    Ma, Yi
    Chu, Hubing
    Chen, Zhenli
    Chen, Yingchun
    [J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2013, 34 (11): : 2435 - 2442
  • [5] The Dynamic Properties and Control Method of a Flying Wing with High Aspect-Ratio and Strong Coupling Between Aeroelasticity and Flight Dynamics
    Zhang S.
    Wang Z.-J.
    Chen H.
    [J]. Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology, 2020, 40 (02): : 157 - 162
  • [6] Aerodynamic performance of low aspect-ratio flapping wing with active wing-chord adjustment
    Cong, Longfei
    Teng, Bin
    Chen, Lifen
    Bai, Wei
    Jin, Ruijia
    Chen, Biaosong
    [J]. JOURNAL OF FLUIDS AND STRUCTURES, 2023, 122
  • [7] Integrate topology/shape/size optimization into high aspect-ratio wing design
    College of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China
    不详
    [J]. J. Mech. Strength, 2008, 4 (596-600): : 596 - 600
  • [8] Pitching effect on transonic wing stall of a blended flying wing with low aspect ratio
    Tao, Yang
    Zhao, Zhongliang
    Wu, Junqiang
    Fan, Zhaolin
    Zhang, Yi
    [J]. MODERN PHYSICS LETTERS B, 2018, 32 (12-13):
  • [9] Bifurcation analysis of wing rock and routes to chaos of a low aspect ratio flying wing
    Jiang, Yun
    Li, Daochun
    Kan, Zi
    Dong, Bohao
    Zhen, Chong
    Xiang, Jinwu
    [J]. NONLINEAR DYNAMICS, 2024,
  • [10] Numerical study on the influence of wall temperature gradient on aerodynamic characteristics of low aspect ratio flying wing configuration
    Peng Lin
    Xueqiang Liu
    Neng Xiong
    Xiaobing Wang
    Ma Shang
    Guangyuan Liu
    Yang Tao
    [J]. Scientific Reports, 11
12345