Advanced Search
Volume 38 Issue 10
Oct.  2012
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  38(10): 1306-1310.
Huang Jun, Wu Zhe, Zhu Rongchanget al. Optimized Collocation of Combat Aircraft Weapon Systems for Air Force[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(5): 546-549. (in Chinese)
Citation: Xiang Jinwu, Zeng Kaichun, Nie Luet al. Elastic effects on flight mechanics of waverider[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(10): 1306-1310. (in Chinese)
shu

Elastic effects on flight mechanics of waverider

  • School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 06 Mar 2012
  • Publish Date: 30 Oct 2012
    Abstract
  • The impact of structural elasticity on the static properties and dynamic stability of a typical air-breathing hypersonic vehicle was investigated. An integrated aeropropulsive/aeroelastic model was developed for the longitudinal dynamics of hypersonic vehicles, with local piston theory for unsteady aerodynamics. A comparative analysis of level-flight trim control, trimmable region, open-loop poles and non-minimum phase zeros was performed when the fuselage was subjected to different bending stiffness. The results show that the structural elasticity has a significant influence on the flight mechanics of hypersonic waverider. The elevator operation mode of vehicles with flexible fuselage is reversed in high Mach number zone. As the fuselage bending stiffness decreases, the lift-drag ratio drops and dynamic stability deteriorates.

     

    • FullText(HTML)
    • References(10)
  • [1]
    Fidan B,Mirmirani M,Ioannou P.Flight dynamics and control of air-breathing hypersonic vehicles:review and new Directions .AIAA-2003-708,2003
    [2]
    Cockrell C E,Engelund W C.Integrated aeropropulsive computational fluid dynamics methodology for the hyper-X flight experiment[J].Journal of Spacecraft and Rockets,2001,38(6):836-843
    [3]
    黄喜元,王青,董朝阳.基于动态逆的高超声速飞行器鲁棒自适应控制[J].北京航空航天大学学报,2011,37(5):560-563 Huang Xiyuan,Wang Qing,Dong Chaoyang.Robust adaptive control for hypersonic vehicle based on dynamic inversion[J].Journal of Beijing University of Aeronautics and Astronautics,2011,37(5):560-563(in Chinese)
    [4]
    Heeg J,Zeiler T A,Pototzky AS,et al.Aerothermoelastic analysis of a NASP demonstrator model .NASA-TM-109007,1993
    [5]
    Clark A D,Mirmirani M D,Wu C,et al.An aero-propulsion integrated elastic model of a generic airbreathing hypersonic vehicle .AIAA-2006-6560,2006
    [6]
    Chavez F R,Schmidt D K.Analytical Aeropropulsive/Aeroelastic hypersonic vehicle model with dynamic analysis[J].AIAA Journal of Guidance,Control,and Dynamics,1994,17(6):1308-1319
    [7]
    Bolender M A,Doman D B.Nonlinear longitudinal dynamical model of an air-Breathing hypersonic vehicle[J].Journal of Spacecraft and Rockets,2007,44(2):374-387
    [8]
    McNamara J J,Crowell A R,Friedmann P R,et al.Approximate modeling of unsteady aerodynamics for hypersonic aeroelasticity[J].Joural of Aircraft,2010,47(6):1932-1945
    [9]
    Anderson J D.Modern compressible flow[M].2nd ed.New York:McGraw-Hill College,1995:77-91
    [10]
    方振平,陈万春,张曙光.航空飞行器飞行动力学[M].北京:北京航空航天大学出版社,2005:219-220 Fang Zhenping,Chen Wanchun,Zhang Shuguang.Aircraft flight dynamics[M].Beijing:Beihang University Press,2005:219-220(in Chinese)
    • Relative Articles

  • Relative Articles

    [1]PIAN Rong, YANG Fan, ZHANG Ling, LIU Feng-rui, WANG Lin-juan, ZHAO Li-bin. Failure mode study of composite laminated plates under compression-shear loading[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0084
    [2]REN W，LI J，WANG T Y，et al. Meshing theory and performance analysis of point-contact conjugate involute worm gear pair[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（10）：3183-3195 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0778.
    [3]ZHANG Luheng, WANG Wenyu, DING Dandan. A Hierarchical Rate Control Method for End-to-End Image Compression[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0461
    [4]CHANG Z N，HU M H，ZHANG Y，et al. A multi-objective optimal control trajectory optimization method for aircraft under wind influence[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（11）：3521-3531 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0836.
    [5]ZHAO Yifei, GU Ruijia, REN Xinhui. Method for small unmanned aerial vehicles path planning considering urban low-altitude wind fields[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0281
    [6]CENG Sheng-fu, LIANG Hao-quan, WANG Yan, SUN Kang-wen, ZHONG Zi-hong. status assessment of stratospheric airship based on improved combination weighting and cloud model[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0713
    [7]PAN C Z，HE G，LI Z J，et al. Adaptive filtered control for uncertain electro-hydraulic servo systems with time-varying output constraints[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：1819-1828 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0497.
    [8]WEN Bo-qun, MIAO Jing-gang, LU Ying, ZHOU Shu-yu. Short-term prediction of stratospheric wind field based on POD-LSTM network[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0608
    [9]SHE W Q，LIU Y B，CHEN B Y. Altitude control strategy for high-aspect-ratio wings with active morphing[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1746-1752 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0612.
    [10]BAI F C，YANG X X，DENG X L，et al. Station keeping control for aerostat in wind fields based on deep reinforcement learning[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（7）：2354-2366 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0629.
    [11]REN D J，XU S H，WANG S P，et al. Modeling and solution method of oil film dynamic coupling for spherical port pair[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（10）：2771-2779 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0724.
    [12]ZHANG C，ZHUANG K，YU P，et al. Process control net modelling and analyzing for satellite test and evaluation in launch site[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：1948-1955 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0628.
    [13]YUAN M Y，ZHOU J H，HAO Y，et al. Design of contactless power supply system for stratospheric airship anemometer[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（4）：972-980 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0344.
    [14]QU Y，WANG S，ZENG L C，et al. Path planning algorithm for airborne pseudolites installed on stratospheric airships[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（5）：1071-1082 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0385.
    [15]GAO Yang, XU Guo-ning, WANG Sheng, LI Yong-xiang, CAI Rong, YANG Yan-chu. Stability analysis of stratospheric airship energy system[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0020
    [16]ZHANG Y Z，LI W B，ZHENG T T. Inverted residual target detection algorithm based on LGC[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（6）：1287-1293 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0452.
    [17]ZHAI J Q，YANG X X，DENG X L，et al. Global path planning of stratospheric aerostat in uncertain wind field[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（5）：1116-1126 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0380.
    [18]ZHANG J L，YANG X X，DENG X L，et al. Altitude control of stratospheric aerostat based on deep reinforcement learning[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：2062-2070 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0622.
    [19]YANG Xi-xiang, HOU Zhong-xi, HAN Yu, YANG Yang. Multifactor effect on output performance of solar array for stratospheric airships[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2022.0651
    [20]LONG Yuan, DENG Xiaolong, YANG Xixiang, HOU Zhongxi. Short-term rapid prediction of stratospheric wind field based on PSO-BP neural network[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(10): 1970-1978. doi: 10.13700/j.bh.1001-5965.2021.0068
    • Supplements(0)
    • Cited By

  • Cited by

    Periodical cited type(2)

    1. 郑志东，刘宁，韩笑雪，戴秋敏. 临近空间飞艇保形升空过程热运动特性研究. 航天返回与遥感. 2023(02): 24-32 .
    2. 翟嘉琪，杨希祥，邓小龙，龙远，张经伦，柏方超. 不确定风场下平流层浮空器全局路径规划. 北京航空航天大学学报. 2023(05): 1116-1126 . 本站查看

    Other cited types(1)

  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(2226) PDF downloads(758) Cited by(3)
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return