Advanced Search
Volume 37 Issue 7
Jul.  2011
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2011  >  37(7): 833-838.
Shi Peng, Li Baojun, Zhao Yushanet al. Orbital maintenance and control of spacecraft fly-around with finite-thrust[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(07): 757-760. (in Chinese)
Citation: Xie Changchuan, Wang Weijian, Yang Chaoet al. Flutter analysis of inflatable wings[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(7): 833-838. (in Chinese)
shu

Flutter analysis of inflatable wings

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

  • Received Date: 08 Jul 2010
  • Publish Date: 30 Jul 2011
    Abstract
  • The stiffness of inflatable wing is determined by the internal pressure, so the static and dynamic coupling method should be established to solve the flutter problems of such wings. The structural stiffness and the normal modes should be calculated on the base of the static analysis. Then the unsteady aerodynamics can be calculated and the flutter characteristics of the wing can be analyzed using the traditional methods. For an inflated wing, the finite element model was created using membrane elements. The structure stiffness of the wing was derived by the static analysis and the normal modes were calculated. Then the flutter of the wing was analyzed. The results show that, as the internal pressure increases, each mode-s natural frequencies increases. Except for the typical bending and torsion modes, the chord-wise bending modes have low frequencies. The chord-warping modes can induce flutter besides the conventional bending-torsion flutter type. The critical flutter speed of the inflatable wing presents nearly linearity with internal pressure increased in specific range and the corresponding flutter modes dose not change as well.

     

    • FullText(HTML)
    • References(1)
  • [1] Norris R K,Pulliam W J.Historical perspectiveon inflatable wing structures .AIAA-2009-2145,2009 [2] Andrew S,Johnathan R,Suzanne S.Aeroelastic deformation and bucking of inflatable wings under dynamic loads .AIAA-2007-2239,2007 [3] 纪秀玲,何光林.管式发射巡飞弹的气动特点与设计[J].北京理工大学学报,2008,28(11):953-956 Ji Xiuling,He Guanglin.Aerodynamic characteristics of guan-launched loitering munitions and Its shape design[J].Journal of Beijing Institute of Technology,2008,28(11):953-956(in Chinese) [4] 朱亮亮,叶正寅.充气式机翼的通用设计方法[J].空军工程大学学报:自然科学版,2009,10(5):17-21 Zhu Liangliang,Ye Zhengyin.Research on a universal design method for inflatable wings[J].Journal of Air Force Engineering University:Natural Science Edition,2009,10(5):17-21(in Chinese) [5] Johnathan M R,Suzanne W S.Development of a finite element model of warping inflatable wings .AIAA-2006-1697,2006 [6] 贾青萍.充气式机翼结构设计及性能分析 .北京:北京航空航天大学航空科学与工程学院,2006 Jia Qingping.Structure design and performance analysis of inflatable wings .Beijing:School of Aeronautic Scienee and Engineering,Beijing University of Aeronautics and Astronautics,2006 [7] Simpson A,Usui M,Jacob J,et al.Aeromechanics of inflatable airfoils .AIAA-2004-2233,2004 [8] Simpson A,Smith S W,Jacob J.Aeroelastic behavior of inflatable wings:wind tunnel and flight testing .AIAA-2007-1069,2007 [9] Gaddam P,Hill J,Jacob J D.Aerostructural interaction and optimization of inflatable wings .AIAA-2010-4610,2010 [10] Peter C.Divergence of inflated wing[J].J Aircraft,1999,37(1):953-956 [11] Leyland G Y,Pai P F.Numerical and experimental dynamic characteristics of thin film membranes .AIAA-2004-1618,2004 [12] 方同,薛璞.振动理论及应用[M].西安:西北工业大学出版社,1998:251-258 Fang Tong,Xue Pu.Vibration theory and applications[M].Xi-an:Northwest Industrial University Press,1998:251-258(in Chinese) [13] 江见鲸,何放龙,何益斌,等.有限元法及其应用[M].北京:机械工业出版社,2006:142-144 Jiang Jianjing,He Fanglong,He Yibing,et al.Finite element method and its application[M].Beijing:Mechanism Industry Press,2006:142-144(in Chinese) [14] 诸德超,邢誉峰.工程振动基础[M].北京:北京航空航天大学出版社,2004:73-76 Zhu Dechao,Xing Yufeng.Foundation of engineering vibration[M].Beijing:Beijing University of Aeronautics and Astronautics Press,2004:73-76(in Chinese) [15] 管德.非定常空气动力计算[M].北京:北京航空航天大学出版社,1991:100-141 Guan De.Unsteady aerodynamics compution[M].Beijing:Beijing University of Aeronautics and Astronautics Press,1991:100-141(in Chinese) [16] 陈桂彬,邹丛青,杨超.气动弹性设计基[M].北京:北京航空航天大学出版社,2004:64-74 Chen Guibin,Zou Congqing,Yang Chao.Elements of aeroelastics[M].Beijing:Beijing University of Aeronautics and Astronautics Press,2004:64-74(in Chinese)
    • Relative Articles

  • Relative Articles

    [1]XU Zhiqiang, GUO Yudong, ZHANG Wenqiang, LIU Yatong, LI Ang, WANG Anni. Research on aerodynamic flow field characteristics of guide-injected icing detector[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0767
    [2]RAN Y T，PAN B F. A method for calculating reachability regions of lift re-entry vehicles with multiple constraints[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（3）：904-909 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0157.
    [3]DONG J C，GAO Q H，LIU Z H. Planar motion control of distributed-driven vehicles considering dynamic hysteresis[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3842-3853 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0887.
    [4]WANG Su, HUANG Hongdian, ZHAO Jianwen, ZHOU Hongjin, LI Qian. Master-slave AUV cooperative localization algorithm based on factor graph[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0378
    [5]CHEN Kejia, XIA Ruidong, LIN Hongxi. Textual sentiment classification incorporating dual emoji attention mechanisms[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0318
    [6]LIU H B，SHI X M，QU J B，et al. Design of Bayesian acceptance scheme for missile hit accuracy based on multinomial distribution[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：1991-2000 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0516.
    [7]LI Z B，SUN W，ZHANG Y N，et al. Computation on aerodynamic and aeroacoustic characteristics of scissor tail-rotor under sideslip condition[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3794-3805 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0037.
    [8]MAO Qinghua, ZHAO Bing, LI Yang. CHAOS ephemeran algorithm combining polynomial difference learning and dimensional variation[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0698
    [9]YANG B，LIU Z，WEI X J，et al. A safety analysis approach for embedded system[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：1930-1939 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0185.
    [10]GONG K Q，WEI H K，LI J W，et al. Trajectory optimization algorithm of skipping missile based on deep reinforcement learning[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（6）：1383-1393 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0436.
    [11]HAN X，WANG Y X，CHENG X C，et al. A decentralized multi-sensor fusion estimator using finite memory buffers[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（2）：335-343 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0240.
    [12]ZHAO G R，GU H L，HAN X，et al. NNS distributed fusion estimator under multiple network constraints[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（2）：229-241 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0225.
    [13]ZHAO Q，FENG K. Noncontact damage imaging method in lattice sandwich structures[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（1）：206-211 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0194.
    [14]SUN Y Q，QIANG H R，DONG K H，et al. Derivation and application of iterative scheme for angle-only orbit determination[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3245-3252 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0062.
    [15]FU J W，WANG C. Configuration and multibody separation scheme of compact missile swarm[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1630-1638 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0508.
    [16]CHEN Y，CHEN J，TAO M F. Mural inpainting progressive generative adversarial networks based on structure guided[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（6）：1247-1259 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0440.
    [17]LI Yongchang, DAI Yuting, YANG Chao. Fluid and structure coupling analysis of split drag rudder[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2494-2501. doi: 10.13700/j.bh.1001-5965.2021.0151
    [18]ZHANG Zhiwen, DU Wenjie, LIANG Junfei, ZHANG Yangang, WU Yawen. Layered control of hybrid power loader based on fuel cell[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(11): 2165-2176. doi: 10.13700/j.bh.1001-5965.2021.0099
    [19]ZHENG Rao, CHEN Xiaozhu, LI Shuangxi, ZHAO Xiang, SHI Renjie, SONG Zifeng. Opening characteristics of inlaid floating ring seal with high-speed gas film[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(11): 2111-2120. doi: 10.13700/j.bh.1001-5965.2021.0083
    [20]LIU Yanbin, WANG Xuesheng, QIN Xinya, WANG Hao, CHEN Qinzhu, ZHAO Sai. Design and characteristics of reverse direct-acting high-pressure reducing valve for pneumatic actuator[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(7): 1164-1173. doi: 10.13700/j.bh.1001-5965.2021.0292
    • Supplements(0)
    • Cited By
  • 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(4036) PDF downloads(1138) Cited by()
    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