Lateral oscillations of an aircraft model at high angles of attack

被引：0
|
作者：
Department of Mechanical Engineering, National Chung-Hsing University, Taichung, Taiwan [1 ]
不详 [2 ]
机构：
来源：
J. Fluids Struct. | / 6卷 / 601-614期
关键词：
Financial support from the National Science Council; Contract NSC 82-0401-D-005-004; Republic of China; for this work is gratefully acknowledged. The authors wish to thank Dr Q.-Y. Shen and the technical group in the Aeronautical Research Laboratory for their assistance in the course of this experimental work;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
16
引用
下载
收藏
相关论文
共 50 条
  • [41] Gust Response at High Angles of Attack
    Mallik, Wrik
    Raveh, Daniella E.
    AIAA JOURNAL, 2019, 57 (08) : 3250 - 3260
  • [42] Time delay compensation in lateral-directional flight control systems at high angles of attack
    Lin SHEN
    Da HUANG
    Genxing WU
    Chinese Journal of Aeronautics , 2021, (04) : 1 - 18
  • [43] Time delay compensation in lateral-directional flight control systems at high angles of attack
    Lin SHEN
    Da HUANG
    Genxing WU
    Chinese Journal of Aeronautics, 2021, 34 (04) : 1 - 18
  • [44] Time delay compensation in lateral-directional flight control systems at high angles of attack
    Shen, Lin
    Huang, Da
    Wu, Genxing
    CHINESE JOURNAL OF AERONAUTICS, 2021, 34 (04) : 1 - 18
  • [45] Mathematical description of nonstationary aerodynamic characteristics of a passenger aircraft model in longitudinal motion at large angles of attack
    Petoshin, V. I.
    Chasovnikov, E. A.
    JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS, 2011, 52 (03) : 390 - 396
  • [46] Mathematical description of nonstationary aerodynamic characteristics of a passenger aircraft model in longitudinal motion at large angles of attack
    V. I. Petoshin
    E. A. Chasovnikov
    Journal of Applied Mechanics and Technical Physics, 2011, 52 : 390 - 396
  • [47] Numerical solution for complete aircraft's subsonic-transonic-supersonic flow at high angles of attack
    E, Q
    Yang, GW
    Li, FW
    COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1997, 148 (1-2) : 11 - 21
  • [48] THREE DIMENSIONAL VORTEX WAKE MODEL FOR MISSILES AT HIGH ANGLES OF ATTACK.
    Sheffield, J.Steven
    Deffenbaugh, F.D.
    NASA Contractor Reports, 1980, (3208):
  • [49] A Weighted Feature Fusion Model for Unsteady Aerodynamic Modeling at High Angles of Attack
    Dong, Wenzhao
    Wang, Xiaoguang
    Lin, Qi
    Cheng, Chuan
    Zhu, Liangcong
    AEROSPACE, 2024, 11 (05)
  • [50] Supersonic test cases at high angles of attack
    Damljanovic, Dijana
    Vukovic, Dorde
    Isakovic, Jovan
    Milos, Marko
    MATERIALS TODAY-PROCEEDINGS, 2019, 12 : 239 - 245
12345