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A Rapid Fatigue Analysis Method of Aluminum Honeycomb Structure with Defects Based on Static Test and Numerical Simulation

Received: 9 November 2019    Accepted:     Published: 3 December 2019
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Abstract

At present, most of the substrates of the multifunctional components are honeycomb sandwich structures. Therefore, the study on the fatigue characteristics of honeycomb sandwich structures with defects is helpful to accelerate the engineering application process of the multifunctional structures.In order to study the fatigue characteristics of multi-functional structure under three conditions of tension, compression and three-point bending, the author of this paper proposes a rapid fatigue analysis method of based on statics experiment and numerical simulation.Firstly, the static experiments of the structure under three mechanical conditions of tension, compression and three-point bending are carried out, and then the static simulation is carried out with ANSYS software under the same conditions, and the finite element model in ANSYS is modified according to the experimental results. Finally, the fatigue of the aluminum honeycomb sandwich structure with defects under three conditions is calculated quickly by the fatigue analysis tool in ANSYS The analytical expression between the fatigue life and the load level of the structure under different load ratios is obtained by using the least square method.The fatigue analysis method avoids the complicated fatigue experiments, solves the problem of obtaining the fatigue characteristics of the honeycomb sandwich structure with defects at low cost and high speed under different mechanical conditions and greatly improves the analysis efficiency of the fatigue characteristics of the complex structure.

Published in Science Discovery (Volume 7, Issue 5)
DOI 10.11648/j.sd.20190705.28
Page(s) 365-372
Creative Commons

This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.

Copyright

Copyright © The Author(s), 2024. Published by Science Publishing Group

Keywords

Aluminum Honeycomb Sandwich Structure, Static Mechanical Test, Fatigue Simulation, Lattice Defect, Fatigue Life Curve

References
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[4] 曹莉,介党阳,熊楚杨,徐嘉. 多功能结构在固体火箭上的应用分析[J].导弹与航天运载技术,2013,(04): 38-42。
[5] Belingardi G, Martella P, Peroni L. Fatigue Analysis of Honeycomb-Composite Sandwich Beams [J]. Composites Part A: Applied Science and Manufacturing, 2007, 38 (4): 1183-1191.
[6] S. Belouettar, A. Abbadi, Z. Azari, R. Belouettar, et al. Experimental investigation of static and fatigue behaviour of composites honeycomb materials using four point bending tests [J]. Composite Structrues, 2009, 87 (3), 265-273.
[7] Soni SM, Gibson RF, Ayorinde EO. The influence of subzero temperatures on fatigue behavior of composite sandwich structures [J]. Composite Science Technology, 2009, 69 (6), 829-838.
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[9] Costantino Menna, Alberto Zinno, Domenico Asprone. Andrea Prota Numerical assessment of the impact behavior of honeycomb sandwich structures [J]. Composite Structures, 2013.106(Complete): 326-339.
[10] Figueroa E, Shafiq B, de la Paz I. Creep to failure and cyclic creep of foam core sandwich composites in seawater [J]. JOURNAL OF SANDWICH STRUCTURES & MATERIALS, 2013, 15 (6): 657-670.
[11] 赵鹏成. 含缺陷复合材料蜂窝夹层结构力学性能研究[D]. 哈尔滨:哈尔滨工程大学,2009: 33。
[12] 柴子龙. 复合材料蜂窝夹芯结构疲劳行为研究[D].哈尔滨:哈尔滨工业大学,2016:66。
[13] 王琦,童国权,陈峰,马振武,杨钦鑫. 缺陷对高温合金蜂窝板弯曲力学性能的影响[J].航空制造技术,2017,(1/2):106-111。
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  • APA Style

    Zhao Qian, Ge Meng, Zhang Shunjia. (2019). A Rapid Fatigue Analysis Method of Aluminum Honeycomb Structure with Defects Based on Static Test and Numerical Simulation. Science Discovery, 7(5), 365-372. https://doi.org/10.11648/j.sd.20190705.28

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    ACS Style

    Zhao Qian; Ge Meng; Zhang Shunjia. A Rapid Fatigue Analysis Method of Aluminum Honeycomb Structure with Defects Based on Static Test and Numerical Simulation. Sci. Discov. 2019, 7(5), 365-372. doi: 10.11648/j.sd.20190705.28

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    AMA Style

    Zhao Qian, Ge Meng, Zhang Shunjia. A Rapid Fatigue Analysis Method of Aluminum Honeycomb Structure with Defects Based on Static Test and Numerical Simulation. Sci Discov. 2019;7(5):365-372. doi: 10.11648/j.sd.20190705.28

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  • @article{10.11648/j.sd.20190705.28,
      author = {Zhao Qian and Ge Meng and Zhang Shunjia},
      title = {A Rapid Fatigue Analysis Method of Aluminum Honeycomb Structure with Defects Based on Static Test and Numerical Simulation},
      journal = {Science Discovery},
      volume = {7},
      number = {5},
      pages = {365-372},
      doi = {10.11648/j.sd.20190705.28},
      url = {https://doi.org/10.11648/j.sd.20190705.28},
      eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.sd.20190705.28},
      abstract = {At present, most of the substrates of the multifunctional components are honeycomb sandwich structures. Therefore, the study on the fatigue characteristics of honeycomb sandwich structures with defects is helpful to accelerate the engineering application process of the multifunctional structures.In order to study the fatigue characteristics of multi-functional structure under three conditions of tension, compression and three-point bending, the author of this paper proposes a rapid fatigue analysis method of based on statics experiment and numerical simulation.Firstly, the static experiments of the structure under three mechanical conditions of tension, compression and three-point bending are carried out, and then the static simulation is carried out with ANSYS software under the same conditions, and the finite element model in ANSYS is modified according to the experimental results. Finally, the fatigue of the aluminum honeycomb sandwich structure with defects under three conditions is calculated quickly by the fatigue analysis tool in ANSYS The analytical expression between the fatigue life and the load level of the structure under different load ratios is obtained by using the least square method.The fatigue analysis method avoids the complicated fatigue experiments, solves the problem of obtaining the fatigue characteristics of the honeycomb sandwich structure with defects at low cost and high speed under different mechanical conditions and greatly improves the analysis efficiency of the fatigue characteristics of the complex structure.},
     year = {2019}
    }
    

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  • TY  - JOUR
    T1  - A Rapid Fatigue Analysis Method of Aluminum Honeycomb Structure with Defects Based on Static Test and Numerical Simulation
    AU  - Zhao Qian
    AU  - Ge Meng
    AU  - Zhang Shunjia
    Y1  - 2019/12/03
    PY  - 2019
    N1  - https://doi.org/10.11648/j.sd.20190705.28
    DO  - 10.11648/j.sd.20190705.28
    T2  - Science Discovery
    JF  - Science Discovery
    JO  - Science Discovery
    SP  - 365
    EP  - 372
    PB  - Science Publishing Group
    SN  - 2331-0650
    UR  - https://doi.org/10.11648/j.sd.20190705.28
    AB  - At present, most of the substrates of the multifunctional components are honeycomb sandwich structures. Therefore, the study on the fatigue characteristics of honeycomb sandwich structures with defects is helpful to accelerate the engineering application process of the multifunctional structures.In order to study the fatigue characteristics of multi-functional structure under three conditions of tension, compression and three-point bending, the author of this paper proposes a rapid fatigue analysis method of based on statics experiment and numerical simulation.Firstly, the static experiments of the structure under three mechanical conditions of tension, compression and three-point bending are carried out, and then the static simulation is carried out with ANSYS software under the same conditions, and the finite element model in ANSYS is modified according to the experimental results. Finally, the fatigue of the aluminum honeycomb sandwich structure with defects under three conditions is calculated quickly by the fatigue analysis tool in ANSYS The analytical expression between the fatigue life and the load level of the structure under different load ratios is obtained by using the least square method.The fatigue analysis method avoids the complicated fatigue experiments, solves the problem of obtaining the fatigue characteristics of the honeycomb sandwich structure with defects at low cost and high speed under different mechanical conditions and greatly improves the analysis efficiency of the fatigue characteristics of the complex structure.
    VL  - 7
    IS  - 5
    ER  - 

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Author Information
  • Shanghai Institute of Mechanical and Electrical Engineering, Shanghai, China

  • Department of Aerospace Engineering, Harbin Institute of Technology, Harbin, China

  • Shanghai Institute of Mechanical and Electrical Engineering, Shanghai, China

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