Impact location on a stiffened composite panel using improved linear array

被引:12
|
作者
Zhong, Yongteng [1 ]
Xiang, Jiawei [1 ]
机构
[1] Wenzhou Univ, Coll Mech & Elect Engn, Wenzhou 325035, Peoples R China
基金
美国国家科学基金会;
关键词
improved linear array; omni-directional; impact localization; 2D-MUSIC; time difference; SIGNAL CLASSIFICATION ALGORITHM; SOURCE LOCALIZATION; DAMAGE DETECTION; MULTI-IMPACT; FILTER;
D O I
10.12989/sss.2019.24.2.173
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
Due to the degradation of beamforming properties at angles close to 0 degrees to 180 degrees, linear array does not have a complete 180 degrees inspection range but a smaller one. This paper develops a improved sensor array with two additional sensors above and below the linear sensor array, and presents time difference and two dimensional multiple signal classification (2D-MUSIC) based impact localization for omni-directional localization on composite structures. Firstly, the arrival times of impact signal observed by two additional sensors are determined using the wavelet transform and compared, and the direction range of impact source can be decided in general, 0 degrees to 180 degrees or 180 degrees to 360 degrees. And then, 2D-MUSIC based spatial spectrum formula using uniform linear array is applied for locate accurate position of impact source. When the arrival time of impact signal observed by two additional sensors is equal, the direction of impact source can be located at 0 degrees or 180 degrees by comparing the first and last sensor of linear array. And then the distance is estimated by time difference algorithm. To verify the proposed approach, it is applied to a quasi-isotropic epoxy laminate plate and a stiffened composite panel. The results are in good agreement with the actual impact occurring position.
引用
收藏
页码:173 / 182
页数:10
相关论文
共 50 条
  • [1] Detection of impact location for composite stiffened panel using FBG sensors
    Park, S. O.
    Jang, B. W.
    Lee, Y. G.
    Kim, Y. Y.
    Kim, C. G.
    Park, C. Y.
    Lee, B. W.
    MULTI-FUNCTIONAL MATERIALS AND STRUCTURES III, PTS 1 AND 2, 2010, 123-125 : 895 - +
  • [2] Impact location on stiffened composite structures using neural networks
    Liu, N.
    Penny, J.E.T.
    Wei, C.Y.
    Irving, P.E.
    Dykes, N.
    Zhu, Q.M.
    Key Engineering Materials, 2001, 204-205 : 395 - 408
  • [3] Impact location on stiffened composite structures using neural networks
    Liu, N
    Penny, JET
    Wei, CY
    Irving, PE
    Dykes, N
    Zhu, QM
    DAMAGE ASSESSMENT OF STRUCTURES, 2001, 204-2 : 395 - 407
  • [4] Impact Analysis of Embedded Delamination Location in Hybrid Curved Laminated Composite Stiffened Panel
    Naini, Jeevan Kumar
    Babu, Ramesh P.
    APPLIED COMPOSITE MATERIALS, 2016, 23 (04) : 639 - 658
  • [5] Impact Analysis of Embedded Delamination Location in Hybrid Curved Laminated Composite Stiffened Panel
    Jeevan Kumar Naini
    Ramesh Babu P
    Applied Composite Materials, 2016, 23 : 639 - 658
  • [6] Determination of impact location on composite stiffened panels
    Sharif-Khodaei, Z.
    Ghajari, M.
    Aliabadi, M. H.
    SMART MATERIALS AND STRUCTURES, 2012, 21 (10)
  • [7] Autonomous impact damage monitoring in a stiffened composite panel
    Banerjee, Sauvik
    Ricci, Fabrizio
    Monaco, Ernesto
    Lecce, Leonardo
    Mal, Ajit
    JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2007, 18 (06) : 623 - 633
  • [8] Impact localization on a composite stiffened panel using reference signals with efficient training process
    Jang, Byeong-Wook
    Kim, Chun-Gon
    COMPOSITES PART B-ENGINEERING, 2016, 94 : 271 - 285
  • [9] Impact Damage Detection In A Stiffened Composite Wing Panel Using Digital Shearography And Thermosonics
    De Angelis, G.
    Meo, M.
    Almond, D. P.
    Pickering, S. G.
    Polimeno, U.
    COMPOSITE SCIENCE AND TECHNOLOGY, PTS 1 AND 2, 2011, 471-472 : 904 - +
  • [10] LOW-VELOCITY IMPACT ANALYSIS OF A STIFFENED COMPOSITE PANEL
    Akula, Venkata M. K.
    ASME PRESSURE VESSELS AND PIPING CONFERENCE - 2015, VOL 3, 2015,