State-of-the-art review on honeycomb sandwich composite structures with an emphasis on filler materials

被引:57
作者
Chandrasekaran, Navin Kumar [1 ]
Arunachalam, Vasanthanathan [1 ]
机构
[1] MEPCO SCHLENK Engn Coll, Dept Mech Engn, Sivakasi 626005, Tamil Nadu, India
关键词
compression; filler material; finite element analysis; honeycomb sandwich; low-velocity impact; quasi-static; AXIAL CRUSH PERFORMANCE; ALUMINUM HONEYCOMBS; COMPRESSIVE RESPONSE; ENERGY-ABSORPTION; FINITE-ELEMENT; IMPACT BEHAVIOR; PART II; FOAM; INPLANE; SHEAR;
D O I
10.1002/pc.26252
中图分类号
TB33 [复合材料];
学科分类号
摘要
Honeycomb sandwich composites are suitable for making structural materials that are mainly characterized by their lightweight and high stiffness strength. The honeycomb structures filled with foam materials or granular materials concerning to the applications enhance the strength and the damping properties. In this paper, an emphasis has been provided for the comprehensive review of response of honeycomb sandwich structures in different conditions, namely, static, dynamic, and damping behaviors with and without filler material from an experimental and finite element simulation perspective. Various applications of honeycomb sandwich composites in different fields are also reviewed in this paper. Potential new directions in honeycomb sandwich composites are also identified in this paper in addition to the current practices. Conclusions and recommendations from different technical papers are reviewed by considering the honeycomb sandwich composites with filler materials. The given area of research seeks more scientific analysis, modeling, and experiments in future structural applications.
引用
收藏
页码:5011 / 5020
页数:10
相关论文
共 69 条
[1]   Modeling and experimental study of a honeycomb beam filled with damping particles [J].
Ahmad, Nazeer ;
Ranganath, R. ;
Ghosal, Ashitava .
JOURNAL OF SOUND AND VIBRATION, 2017, 391 :20-34
[2]   Quasi-static axial crushing of extruded polystyrene foam-filled thin-walled aluminum tubes:: Experimental and numerical analysis [J].
Aktay, L ;
Toksoy, AK ;
Güden, M .
MATERIALS & DESIGN, 2006, 27 (07) :556-565
[3]   Numerical modelling of honeycomb core crush behaviour [J].
Aktay, Levent ;
Johnson, Alastair F. ;
Kroeplin, Bernd-H. .
ENGINEERING FRACTURE MECHANICS, 2008, 75 (09) :2616-2630
[4]   Theoretical and finite element study of a compact energy absorber [J].
Ali, M. ;
Qamhiyah, A. ;
Flugrad, D. ;
Shakoor, M. .
ADVANCES IN ENGINEERING SOFTWARE, 2008, 39 (02) :95-106
[5]   Application of aluminium honeycomb sandwich panel as an energy absorber of high-speed train nose [J].
Amraei, M. ;
Shahravi, M. ;
Noori, Z. ;
Lenjani, A. .
JOURNAL OF COMPOSITE MATERIALS, 2014, 48 (09) :1027-1037
[6]  
Annamalai K., 2017, INT J AUTOMOT ENG, V7, P2583, DOI [10.22068/ijae.7.4.2583, DOI 10.22068/IJAE.7.4.2583]
[7]   EFFECT OF CORE THICKNESS AND INTERMEDIATE LAYERS ON MECHANICAL PROPERTIES OF POLYPROPYLENE HONEYCOMB MULTI-LAYER SANDWICH STRUCTURES [J].
Arbaoui, J. ;
Schmitt, Y. ;
Pierrot, J. -L. ;
Royer, F. -X. .
ARCHIVES OF METALLURGY AND MATERIALS, 2014, 59 (01) :11-16
[8]   Quasi-static and dynamic experiments of aluminum honeycombs under combined compression-shear loading [J].
Ashab, A. S. M. ;
Ruan, Dong ;
Lu, Guoxing ;
Wong, Yat Choy .
MATERIALS & DESIGN, 2016, 97 :183-194
[9]   Experimental investigation of the mechanical behavior of aluminum honeycombs under quasi-static and dynamic indentation [J].
Ashab, A. S. M. ;
Ruan, Dong ;
Lu, Guoxing ;
Xu, Shanqing ;
Wen, Cuie .
MATERIALS & DESIGN, 2015, 74 :138-149
[10]   Finite Element Analysis of Aluminum Honeycombs Subjected to Dynamic Indentation and Compression Loads [J].
Ashab, A. S. M. Ayman ;
Ruan, Dong ;
Lu, Guoxing ;
Bhuiyan, Arafat A. .
MATERIALS, 2016, 9 (03)