Advanced Search
Volume 27 Issue 1
Jan.  2001
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2001  >  27(1): 62-65.
Lin Qiang, Xiong Huagang, Zhang Qishanet al. Bandwidth allocation for FC-AL under hard real time condition[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(04): 443-446. (in Chinese)
Citation: LI Min, ZHU De-chao. Analytical and Experimental Research of Ball-Bar Impact under Low Velocity[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(1): 62-65. (in Chinese)
shu

Analytical and Experimental Research of Ball-Bar Impact under Low Velocity

  • Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics

  • Received Date: 28 Sep 1999
  • Publish Date: 31 Jan 2001
    Abstract
  • The analytical and experimental investigations of low speed impact of a ball on a bar were reported. The impact tests, which were carried out by means of laser vibrometer, verified the Hertz contact theorem. It was also shown that, the analysis of low speed impact problem can really be reformulated as the analysis of conventional dynamic response problem. Hence, such kind of problems can be calculated by using MSC/NASTRAN program and its special data card. The agreement between the experimental and analytical results is very well. Furthermore, some technical problems related to the impact measurement by using laser vibratormeter were clarified through this relatively fundamental impact test, thus providing the further more complicated structural impact test with experience and technology.

     

    • FullText(HTML)
    • References(1)
  • [1] Timoshenko S P,Goodier J N. Theory of elasticity[M]. New York:MacGraw-Hill, 1970. [2] Timoshenko S P. Vibration problem in engineering[M].3rd ed. New Jersey:Van Nostrand, 1955. [3] Graff K F. Wave motion in elastic solids[M]. Oxford :Clarendon, 1975. [4] Goldsmith W. Impact:the theory and physical behavior of colliding solids[M]. London:Edward Arnold, 1960. [5] Love A E H. A treatise on the mathematical theory of elasticity[M]. New York:Dover, 1944. [6] 诸德超,邢誉峰. 点弹性碰撞问题之解析解[J].力学学报,1996,28(1):99~103. [7] 诸德超,邢誉峰,李 敏. 结构弹性碰撞问题注 .见:王大钧主编. 工程力学进展 . 北京:北京大学出版社,1998．175~179. [8] Trowbridge D A, Grady J E, Aiello R A. Low velocity impact analysis with NASTRAN[J]. Computers & Structures, 1991, 40(4):977~984.
    • Relative Articles

  • Relative Articles

    [1]ZHANG X J，LIU F W，ZHANG Z Y，et al. Overview of low-altitude intelligent networked system[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（6）：1793-1815 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2025.0060.
    [2]WANG Qiang, WANG Jie, WANG Ning, GUO Fang, HAN Wei. Research on dynamics modeling and simulation for shifting center-of-mass flight with an eccentric rotating mass[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2025.0102
    [3]WANG W J，WANG Z，PANG W K，et al. Angular momentum envelope analysis method of gimbal-type momentum exchange device[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（5）：1591-1598 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0268.
    [4]WEI Wenjun, LIU Yanhao, ZHOU Zhongcheng, WANG Jie. Model-free adaptive predictive control for virtual grouping considering measurement noise and data packet dropout[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2025.0158
    [5]DONG Lei, WANG Qi, CHEN Xi, LIU Jiachen. Design of operational security guarantee method for DAA system based on runtime assurance[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2025.0122
    [6]ZHANG Dongping, WANG Mengting, LU Zhanhong, REN Ye, LIU Zhiyong, YANG Li. Intrusion Detection in Industrial Control Systems Based on Data Augmentation by Large Time Series Models[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0755
    [7]LI Xinyan, CHEN Xintao, ZHAO Huimin, DENG Wu. A Federated Learning Flight Operation Data Sharing Method for Balancing Privacy and Utility[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0413
    [8]SHI T X，CHEN L S，LI T S，et al. Distributed adaptive anti-disturbance control for power systems based on multi-agents[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1685-1692 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0496.
    [9]XIONG F，LI Q，LI J，et al. Time-triggered traffic scheduling-oriented virtual network embedding method[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：1982-1990 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0511.
    [10]LIU W，YAN S，WANG X B，et al. Consensus control of multi-agent systems with uncertain communication networks[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1463-1473 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0518.
    [11]CHEN T T，WANG F Y，XIA C Y，et al. Tracking control of multi-agent systems based on persistent-hold mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3321-3327 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0065.
    [12]LIU S，YANG D Z，FENG Q，et al. Modeling method of flight test requirements based on DoDAF[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：2129-2136 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0584.
    [13]XIE C C，ZHANG D Y，AN C. Reduced order method for large flexible wing structure based on dynamic response data[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（6）：1319-1330 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0439.
    [14]ZHANG Y X，WANG X J，WANG S P，et al. Mechanism of butterfly forward flight and prototype verification based on characteristic motion observation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1651-1660 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0497.
    [15]SONG Z R，ZHAO J C，YANG W F. Boundary protection control method of helicopter power system based on flight test analysis[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（1）：100-105 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0431.
    [16]JIA Y，YANG Y T，WU J H. Effect of powertrain arrangement on aerodynamic characteristics of blended-wing-body aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（5）：1156-1165 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0370.
    [17]LI Wen, CAI Yongqing, CHEN Mengfan, LIU Peng. Optical path simulation and design of NO rapid detection optical cavity structure[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(11): 2146-2152. doi: 10.13700/j.bh.1001-5965.2021.0105
    [18]YANG Han, ZHANG Xingjuan, WANG Chao, YANG Chunxin. Simulation and test study on split four-wheel air cycle refrigeration system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(12): 2203-2210. doi: 10.13700/j.bh.1001-5965.2019.0633
    [19]Wang Meiqing, Qin Haiping. Management of quality cost oriented to aerospace product development system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(5): 619-625.
    [20]Wang Xiaojun, Yang Haifeng, Qiu Zhiping, Song Weibo. Fuzzy theory for uncertain structural analysis based on measurement data[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(8): 887-891.
    • Supplements(0)
    • Cited By
  • Created with Highcharts 5.0.7Amount of accessChart context menuAbstract Views, HTML Views, PDF Downloads StatisticsAbstract ViewsHTML ViewsPDF Downloads2024-082024-092024-102024-112024-122025-012025-022025-032025-042025-052025-062025-0702.557.51012.5
    Created with Highcharts 5.0.7Chart context menuAccess Class DistributionFULLTEXT: 26.7 %FULLTEXT: 26.7 %META: 73.3 %META: 73.3 %FULLTEXTMETA
    Created with Highcharts 5.0.7Chart context menuAccess Area Distribution其他: 13.3 %其他: 13.3 %天津: 3.3 %天津: 3.3 %张家口: 13.3 %张家口: 13.3 %扬州: 3.3 %扬州: 3.3 %无锡: 3.3 %无锡: 3.3 %深圳: 23.3 %深圳: 23.3 %漯河: 3.3 %漯河: 3.3 %石家庄: 10.0 %石家庄: 10.0 %芒廷维尤: 13.3 %芒廷维尤: 13.3 %西宁: 13.3 %西宁: 13.3 %其他天津张家口扬州无锡深圳漯河石家庄芒廷维尤西宁

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(2696) PDF downloads(1435) 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