Development of an electromagnetic compatible composite-insert embedded in a double-curved sandwich panel

被引:0
|
作者
Mokhtari, Majid [1 ]
机构
[1] Natl Univ Skills NUS, Dept Mech Engn, Tehran, Iran
关键词
Nanocomposites; strength; mechanical testing; joints; insert; BEHAVIOR; JOINTS;
D O I
10.1177/10996362241282826
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Composite sandwich structures, which are widely employed in engineering structures, require a multitude of inserts. In certain instances, the necessity for a specialized insert arises from the unique characteristics of a particular application. In applications such as weather radar radomes, double-curved sandwich panels should be designed with electromagnetic (EM) transparency as a primary objective. The use of metal inserts should be restricted to the absolute minimum. Given the limitations of using metal materials to protect against EM radiation and the need to enhance the load-bearing capacity of the joint against pull-out loads, a composite insert has developed as an innovative solution. In this study, a composite insert of a double-curved sandwich dome has been developed using silica nanoparticles, and its mechanical strength against pull-out load has been evaluated through both experimental and numerical analysis. The strength results obtained have been compared with analytical estimates. Additionally, the buckling of the double-curved sandwich dome against a wind speed of 220 km/h has been investigated numerically. The critical buckling load for wind loading for the full-scale sandwich radome was estimated to be 16,303 N. According to the numerical results obtained with the Abaqus finite element (FE) software, the maximum pull-out force applied to the connection area is approximately 10.7 kN. A parametric study of geometric variables and experimental results showed that it is possible to achieve a stronger composite insert (by 1 wt % nano silica particles) by 20.7% lighter and 102.65% more bearing capacity.
引用
收藏
页码:1509 / 1531
页数:23
相关论文
共 43 条
  • [1] Post-buckling and vibration analysis of double-curved sandwich panels with SMA embedded faces
    Khorramabadi, Reza
    Ferdosi, Sima Besharat
    COMPOSITES PART C: OPEN ACCESS, 2023, 12
  • [2] DOUBLE-CURVED FORM APPROXIMATION WITH IDENTICAL DISCRETE PANEL GEOMETRIES
    Klemmt, Christoph
    Sodhi, Rajat
    PROCEEDINGS OF THE 22ND INTERNATIONAL CONFERENCE ON COMPUTER-AIDED ARCHITECTURAL DESIGN RESEARCH IN ASIA (CAADRIA 2017): PROTOCOLS, FLOWS AND GLITCHES, 2017, : 457 - 466
  • [3] An amendment method for stress and strain of double-curved laminated composite
    Liu, Yongshou
    Liu, Jun
    Wang, Anqiang
    Yue, Zhufeng
    PRICM 6: SIXTH PACIFIC RIM INTERNATIONAL CONFERENCE ON ADVANCED MATERIALS AND PROCESSING, PTS 1-3, 2007, 561-565 : 757 - 760
  • [4] Finite element analysis of formability of aluminum alloy double-curved panel by VPF
    Li, Yi
    Wang, Zhongjin
    Li, Yanping
    ADVANCED MANUFACTURING TECHNOLOGY, PTS 1-4, 2012, 472-475 : 817 - +
  • [5] Modal interaction in chaotic vibrations of a shallow double-curved shell-panel
    Maruyama, S.
    Nagai, K.
    Tsuruta, Y.
    JOURNAL OF SOUND AND VIBRATION, 2008, 315 (03) : 607 - 625
  • [6] Development of shock-absorbing insert for honeycomb sandwich panel
    Park, Hyun-Su
    Hwang, Dae-Hyun
    Han, Jae-Hung
    Yang, Jinkyu
    AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 104
  • [7] Local facesheet pulse buckling in a curved, composite sandwich panel
    Gao, Yifei
    Fatt, Michelle S. Hoo
    COMPOSITE STRUCTURES, 2013, 104 : 249 - 260
  • [8] Development of the hybrid insert for composite sandwich satellite structures
    Lim, Jun Woo
    Lee, Dai Gil
    COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2011, 42 (08) : 1040 - 1048
  • [9] AN ENGINEERING APPROACH TO MODELLING PROCESS-INDUCED DEFORMATIONS OF DOUBLE-CURVED COMPOSITE ELEMENTS
    Osmeda, Anna
    COMPOSITES THEORY AND PRACTICE, 2015, 15 (02): : 66 - 71
  • [10] Compensation of process-induced deformations of double-curved carbon-epoxy composite elements
    Galinska, Anna
    POLYMER COMPOSITES, 2019, 40 (09) : 3666 - 3677