Compressive response and energy absorption of foam-filled aluminum honeycomb composite: experiments and simulation

被引:8
作者
Fathi, Mohammad [1 ]
Sameezadeh, Mahmood [1 ]
Vaseghi, Majid [1 ,2 ]
机构
[1] Shahid Beheshti Univ, Fac Mech & Energy Engn, Dept Mat & Met, Tehran 1983969411, Iran
[2] Univ Alabama, Dept Mech Engn, Tuscaloosa, AL USA
关键词
Aluminum honeycomb; Composite; Polyurethane foam; Compressive behavior; Shear band; Energy absorption; KOREAN TILTING TRAIN; SANDWICH PANEL; BEHAVIOR; INPLANE; DESIGN;
D O I
10.1007/s40430-023-04489-z
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In this study, the effect of foam-filling pattern on the compressive response and energy absorption capacity of the aluminum honeycomb composite has been investigated. An aluminum honeycomb core and a polyurethane foam were used to produce foam-filled honeycomb panels in three patterns with the same volume fraction of the foam. Experimental quasi-static compression tests were performed in the in-plane direction. Numerical analysis based on the conducted tests was also performed by ABAQUS finite element software in similar laboratory conditions to verify the accuracy of the experiments. The results show that the polyurethane-filling pattern is effective in the compressive behavior of the honeycomb core due to the creation and change of the shear bands, the length of the path deflection, and compressive force distribution. At an angle of 30 degrees-35 degrees, the honeycomb materials deform in the in-plane direction, forming shear bands with a greater strain. However, by using the optimized foam pattern-alternating pattern-in addition to enhancing the honeycomb's compressive strength and energy absorption capacity by 490% and 800%, respectively, the foam usage rate can be reduced up to 35% compared to the full foam mode, resulting in lower cost.
引用
收藏
页数:10
相关论文
共 34 条
[1]  
[Anonymous], 2011, Manual of ABAQUS finite element analysis software package, analysis user's guide, explicit dynamic analysis
[2]  
ASTM, 2016, ASTM D1621
[3]  
Baumgart CT., 2018, Science and Technology of Materials, P35
[4]   Design of Replicated Open-Pore Aluminium Cellular Materials with a Non-Stochastic Structure for Sound Absorption Applications [J].
Carbajo, J. ;
Molina, J. M. ;
Kim, S. ;
Maiorano, L. P. ;
Mosanenzadeh, S. Ghaffari ;
Fang, N. X. .
METALS AND MATERIALS INTERNATIONAL, 2023, 29 (04) :1007-1018
[5]   The in-plane, elastic-plastic response of a filled hexagonal honeycomb at finite strain [J].
Carlsson, J. ;
Li, K. ;
Deshpande, V. S. ;
Fleck, N. A. .
JOURNAL OF THE MECHANICS AND PHYSICS OF SOLIDS, 2022, 168
[6]   Honeycomb failure processes under in-plane loading [J].
Cricri, G. ;
Perrella, M. ;
Cali, C. .
COMPOSITES PART B-ENGINEERING, 2013, 45 (01) :1079-1090
[7]   Multi-axial yield behaviour of polymer foams [J].
Deshpande, VS ;
Fleck, NA .
ACTA MATERIALIA, 2001, 49 (10) :1859-1866
[8]   Numerical Investigation into In-Plane Crushing of Tube-Reinforced Damaged 5052 Aerospace Grade Aluminum Alloy Honeycomb Panels [J].
Djemaoune, Younes ;
Krstic, Branimir ;
Rasic, Stefan ;
Radulovic, Daniel ;
Dodic, Marjan .
MATERIALS, 2021, 14 (17)
[9]   Investigation of mechanical behavior of multi-cellular tubes with intermediate walls under lateral quasi-static loading [J].
Guo, Wannan .
JOURNAL OF THE BRAZILIAN SOCIETY OF MECHANICAL SCIENCES AND ENGINEERING, 2022, 44 (08)
[10]   A study on composite honeycomb sandwich panel structure [J].
He, Meifeng ;
Hu, Wenbin .
MATERIALS & DESIGN, 2008, 29 (03) :709-713