The Analysis of Motion Characteristics of Variable Forward-swept Wing Mechanism with a Double Slideways

被引:0
|
作者
Su, Xin Bing [1 ]
Zhou, Zhou [1 ,2 ]
Wang, Xu [2 ]
Shi, Jing Cheng [2 ]
Chen, Peng [2 ]
机构
[1] Northwestern Poly Tech Univ, Natl Key Lab Sci & Technol UAV, Xian 710072, Peoples R China
[2] Air Force Engn Univ, Inst Aeronaut & Astronaut Engn, Xian 710038, Peoples R China
关键词
variable forward-swept wing; wing-body switching mechanism; two slideways; motion characteristic;
D O I
10.4028/www.scientific.net/AMM.456.137
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Based on the variable forward-swept wing configuration, this paper utilized a variable forward-swept wing mechanism with a double slideways, which make it possible for the aircraft to switch among orthogonal wing, forward-swept wing and delta wing freely. The general configuration of the variable forward-swept wing mechanism with a double slideways was elucidated by means of a three-dimensional model plot and then the mathematic simulation model was also established. The motion characteristics of linear motion were simulated, analyzed and optimized. The results indicated that the variable forward-swept wing mechanism with a double slideways can meet the aerodynamic requirements better. Moreover, there exists great linear relationship between the position of nut and the wing forward-swept angle. Therefore, this mechanism may serve as a useful reference when developing a morphing aircraft.
引用
收藏
页码:137 / +
页数:2
相关论文
共 50 条
  • [21] Supersonic Forward-Swept Wing Design Using Multifidelity Efficient Global Optimization
    Kishi, Yuki
    Kanazaki, Masahiro
    Makino, Yoshikazu
    JOURNAL OF AIRCRAFT, 2022, 59 (04): : 1027 - 1040
  • [22] Experimental and Numerical Studies on Static Aeroelastic Behaviours of a Forward-Swept Wing Model
    Ouyang, Yan
    Zeng, Kaichun
    Kou, Xiping
    Gu, Yingsong
    Yang, Zhichun
    SHOCK AND VIBRATION, 2021, 2021
  • [23] ANALYTICAL STUDIES ON STATIC AEROELASTIC BEHAVIOR OF FORWARD-SWEPT COMPOSITE WING STRUCTURES
    LIBRESCU, L
    THANGJITHAM, S
    JOURNAL OF AIRCRAFT, 1991, 28 (02): : 151 - 157
  • [24] Flow control technique for forward-swept wing blended body tailless configuration
    School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China
    不详
    Hangkong Xuebao, 2009, 3 (397-402):
  • [25] Numerical Research on the Flow Separation Characteristics of Forward-swept Blades
    Liang, Di
    Wang, Si-Jie
    Li, Yi-Min
    Feng, Fei-Fan
    Zhou, Zhong-Ning
    Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2021, 42 (11): : 2849 - 2857
  • [26] Study of control characteristics for split rudder in variable forward swept wing configuration
    Wang, X. (wanxuii@yahoo.com), 1600, Chinese Society of Astronautics (34):
  • [27] Shock characteristics measured upstream of both a forward-swept and an aft-swept fan
    Podboy, Gary G.
    Krupar, Martin J.
    Sutliff, Daniel L.
    Horvath, Csaba
    Proceedings of the ASME Turbo Expo 2007, Vol 6, Pts A and B, 2007, : 1455 - 1478
  • [28] Structure and Topology Analysis of Separated Vortex in Forward-Swept Blade
    Liang, D.
    Li, Y.
    Zhou, Z.
    Wisniewski, P.
    Dykas, S.
    FRONTIERS IN ENERGY RESEARCH, 2021, 9
  • [29] Divergence experiment prediction techniques of flat-plate forward-swept wing in wind tunnel
    Wan, Zhi-Qiang
    Tang, Chang-Hong
    Zou, Cong-Qing
    Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica, 2002, 19 (03): : 88 - 93
  • [30] Control characteristics analysis of split rudder of elastic forward swept wing
    Ma B.
    Su X.
    Feng H.
    Wang N.
    Zhang Y.
    Su, Xinbing (sxinbing01@163.com), 1849, Beijing University of Aeronautics and Astronautics (BUAA) (43): : 1849 - 1858