Wang Yuhui, Zhang Yuru, Wang Dangxiaoet al. Haptic rendering algorithm based on discrete energy optimization method of preparation of human tooth[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(07): 785-788. (in Chinese)
Citation: Deng Ying, Yan Xiaojun, Zhang Huiet al. Net barrier strength and performance evaluation of AAS by FE method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(2): 171-174. (in Chinese)

Net barrier strength and performance evaluation of AAS by FE method

  • Received Date: 24 Dec 2009
  • Publish Date: 28 Feb 2011
  • The performance of aircraft arresting system (AAS) and strength of net barrier was evaluated by means of nonlinear finite element (FE), considering contact, net mass and material properties. Key problems, such as FE model, boundary condition and numerical convergence caused by complex nonlinear system, were solved. The simulation results provide stress distribution of AAS to evaluate strength margin of the net barrier. It is worth well of pointing out that the method can also be used to check effectiveness of controller-s method. The results also show that this method could describe arresting processes closely to actual state. Consequently, the procedures can be effective in an AAS design.

     

  • [1] Hartzer R B.From sandbags to MAAS: aircraft arresting systems[J].Air Force Civil Engineer Magazine,1993,7:1-3 [2] Hsin C C.Arresting landing studies for STOL aircraft [J].Journal of Aircraft,1974,11(3):159-165 [3] Edit group of world aircraft manual.World aircraft manual[M].China: Aviation Industry Press,2001 [4] Hsin C C.Arrested landing studies for STOL aircraft //Hsin C C.Annual Meeting and Technical Display,Washington D C: Virginia University,Charlottesville,1973: 1-10 [5] 李启明,冯蕴雯,于立明.飞机拦阻着陆动力学分析与仿真[J].计算机仿真,2010,27(1): 27-31 Li Qiming,Feng Yunwen,Yu Liming.Kinetics Analysis and simulation of aircraft arrested shore-landing[J].Computer Simulation,2010,27(1): 27-31(in Chinese) [6] 张明晖,袁理,洪冠新.航空母舰液压拦阻系统拦阻力建模与仿真[J].北京航空航天大学学报,2010,36(1): 100-103 Zhang Minghui,Yuan Li,Hong Guanxin.Aircraft carrier hydraulic arresting gear arresting force modeling and simulation[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(1): 100-103(in Chinese)
  • Relative Articles

    [1]LI L Y,YANG R N,WANG Y,et al. CAP planning method based on elliptic fitting of optimal detection routes[J]. Journal of Beijing University of Aeronautics and Astronautics,2025,51(1):293-302 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0978.
    [2]SUN K,HU Q S,ZHENG X F,et al. Multi-Bernoulli extended target tracking based on orientation and half axes lengths of an ellipse[J]. Journal of Beijing University of Aeronautics and Astronautics,2024,50(11):3367-3376 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0869.
    [3]CHEN Hui, LIU Meng-bo, LIAN Feng, HAN Chong-zhao. Star convex irregular shape multi-extended target PMBM filter[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0766
    [4]PANG C,LIU D J,TIAN G,et al. Experimental and simulation study on fatigue multi crack fusion of 2195-T8 Al-Li alloy[J]. Journal of Beijing University of Aeronautics and Astronautics,2024,50(1):350-358 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0249.
    [5]ZHANG Xu, ZHAO Rui, LI Yu, YANG Guang, WANG Li-yan. Component of gas-injection effects on wall heat flux and skin-friction of vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0009
    [6]ZHOU K,CHEN W J,CHEN W H,et al. Extended subtraction speech enhancement based on cubic spline interpolation[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(10):2826-2834 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0744.
    [7]WANG J M,GUO Y Q,YU H F. Extension method of engine low speed characteristics based on backbone features[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(9):2351-2360 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0634.
    [8]LIU Qiang, YIN Yu, LI Kai. Research on image preprocessing acceleration method based on RISC-V vector extension[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0208
    [9]ZHANG Yun-jie, ZHOU Jie-xin, ZHANG Feng-zhe, ZHOU Rui, ZOU Ting. Reachability Evaluation Method for Ballistic Missile Based on Extended Boundary Method[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0630
    [10]HAN J K,YUAN T,LIU Z K,et al. Expanding hexagon search method based on honeycomb structure[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(10):2731-2740 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0718.
    [11]XIN T D,CUI C Y,LIU Y,et al. Non-probabilistic reliability analysis method for propellent tank with crack defect[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(9):2330-2336 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0651.
    [12]FAN X H,GOU B Y,CHEN T,et al. Hole edge crack monitoring technology of flexible eddy current array sensor[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(3):726-734 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0306.
    [13]LI Y,ZONG H H,CAI J,et al. Hydroplaning behavior of aircraft wheel group and additional resistance due to accumulated water on pavement[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(5):1099-1107 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0402.
    [14]WEN C,DONG W H,XIE W J,et al. Multi-UAVs 3D cooperative curve path planning method based on CEA-GA[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(11):3086-3099 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0787.
    [15]ZHOU Quan-zhi, YANG You-xu, SUN Lu-bin, ZHANG Xing-cui, WU Yi-fei, HUO Meng-wen. Aeroelastic Optimization Design of SpaRibs Wing Structure[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0343
    [16]WANG Z X,WAN Z Q,WANG X Z,et al. Fast stability analysis method for composite panel with variable angle tow fiber[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(2):353-366 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0259.
    [17]WU Sunyong, ZHOU Yusong, XIE Yun, CAI Ruhua, FAN Xiangting. Extended target tracking algorithm based on MM-GGIW-PMBM filter[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2356-2364. doi: 10.13700/j.bh.1001-5965.2021.0162
    [18]PENG Chaoyong, XU Songbai, DU Chuangzhou, ZHANG Jie. Ultrasonic phased array imaging on aviation aluminum block fatigue crack[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2398-2404. doi: 10.13700/j.bh.1001-5965.2021.0161
    [19]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
    [20]XIA Fei, XUE Jianghong, HE Zanhang, JIN Fusong. Interfacial crack growth of delaminated composite laminates under hygrothermal environment[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2460-2472. doi: 10.13700/j.bh.1001-5965.2021.0137
  • 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

    Article Metrics

    Article views(3283) PDF downloads(1011) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return