Misalignment Assembly Effect on the Impact Mechanical Response of Tandem Nomex Honeycomb-Core Sandwich Structures

被引:0
作者
Yin, Yufan [1 ]
Zhang, Xiaojing [1 ]
机构
[1] Shanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai 200240, Peoples R China
关键词
tandem honeycomb; misalignment assembly; mechanical response; finite element model; failure behavior; BEHAVIOR; OPTIMIZATION; DESIGN; PANELS;
D O I
10.3390/ma17164024
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
To optimize the assembly methods of honeycomb structures and enhance their design flexibility, this study investigated the impact mechanical responses of tandem honeycomb-core sandwich structures with varying misalignment assembly lengths. Impact tests were conducted across different energy levels on single-layer and tandem honeycomb-core sandwiches to observe their impact processes and failure behaviors. Our findings indicate that tandem honeycomb cores significantly enhance the impact resistance compared with single-layer configurations, even though a misaligned assembly can deteriorate this property. A finite element model was developed and validated experimentally; the model showed good agreement with the experiments, thereby allowing the simulation and evaluation of the impact responses. Herein, we reveal that specific misalignment lengths can either increase or decrease the impact resistance, providing insights into improving the resilience of tandem honeycomb-core structures. Our results not only contribute to enhancing the impact resistance of honeycomb-core sandwich structures but also offer a valuable basis for their practical applications in engineering.
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页数:27
相关论文
共 48 条
  • [1] Impact performance enhancement of honeycombs through additive manufacturing-enabled geometrical tailoring
    Andrew, J. Jefferson
    Ubaid, Jabir
    Hafeez, Farrukh
    Schiffer, Andreas
    Kumar, S.
    [J]. INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2019, 134
  • [2] [Anonymous], 2018, ASTM International D3763-18, DOI [10.1520/D3763-18, DOI 10.1520/D3763-18]
  • [3] [Anonymous], 2015, ASTM D 7136/7136M-15
  • [4] Prediction of impact-induced delamination in cross-ply composite laminates using cohesive interface elements
    Aymerich, F.
    Dore, F.
    Priolo, P.
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 2008, 68 (12) : 2383 - 2390
  • [5] Bitzer TN, 1997, Honeycomb technology: materials, design, manufacturing, applications and testing, DOI [10.1007/978-94-011-5856-5, DOI 10.1007/978-94-011-5856-5]
  • [6] Study on the Energy Absorption Characteristics of Different Composite Honeycomb Sandwich Structures under Impact Energy
    Chang, Bianhong
    Wang, Zhenning
    Bi, Guangjian
    [J]. APPLIED SCIENCES-BASEL, 2024, 14 (07):
  • [7] Multi-objective optimization for designing a composite sandwich structure under normal and 45° impact loadings
    Chen, Yuan
    Fu, Kunkun
    Hou, Shujuan
    Han, Xu
    Ye, Lin
    [J]. COMPOSITES PART B-ENGINEERING, 2018, 142 : 159 - 170
  • [8] Low-Velocity Impact Resistance of Double-Layer Folded Sandwich Structure
    Duan, Yuechen
    Zhan, Zhiren
    Zou, Ting
    Tie, Ying
    Cui, Zhen
    Wang, Tingting
    [J]. MACHINES, 2022, 10 (08)
  • [9] Predicting low-velocity impact damage on a stiffened composite panel
    Faggiani, A.
    Falzon, B. G.
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2010, 41 (06) : 737 - 749
  • [10] Review of current trends for metal-based sandwich panel: Failure mechanisms and their contribution factors
    Faidzi, M. K.
    Abdullah, S.
    Abdullah, M. F.
    Azman, A. H.
    Hui, D.
    Singh, S. S. K.
    [J]. ENGINEERING FAILURE ANALYSIS, 2021, 123 (123)