Graded conventional-auxetic Kirigami sandwich structures: Flatwise compression and edgewise loading

被引:201
作者
Hou, Y. [1 ]
Neville, R. [2 ]
Scarpa, F. [2 ]
Remillat, C. [2 ]
Gu, B. [1 ]
Ruzzene, M. [3 ]
机构
[1] Donghua Univ, Coll Text, Key Lab High Performance Fibers & Prod, Minist Educ, Shanghai 201620, Peoples R China
[2] Univ Bristol, Adv Composites Ctr Innovat & Sci, Bristol BS8 1TR, Avon, England
[3] Georgia Inst Technol, D Guggenheim Sch Aerosp Engn, Atlanta, GA 30332 USA
基金
英国工程与自然科学研究理事会;
关键词
Honeycomb; Mechanical properties; Impact behavior; Assembly; WAVE-PROPAGATION; IMPACT RESPONSE; HONEYCOMB; STRENGTH; CORE; BEHAVIOR; FAILURE; BLADES; PANELS; RATIO;
D O I
10.1016/j.compositesb.2013.10.084
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The work describes the manufacturing and testing of graded conventional/auxetic honeycomb cores. The graded honeycombs are manufactured using Kevlar woven fabric/914 epoxy prepreg using Kirigami techniques, which consist in a combination of Origami and ply-cut processes. The cores are used to manufacture sandwich panels for flatwise compression and edgewise loading. The compressive modulus and compressive strength of stabilized (sandwich) honeycombs are found to be higher than those of bare honeycombs, and with density-averaged properties enhanced compared to other sandwich panels offered in the market place. The modulus and strength of graded sandwich panel under quasi-static edgewise loading vary with different failure mode mechanisms, and offer also improvements towards available panels from open literature. Edgewise impact loading shows a strong directionality of the mechanical response. When the indenter impacts the auxetic portion of the graded core, the strong localization of the damage due to the negative Poisson's ratio effect contains significantly the maximum dynamic displacement of the sandwich panel. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:33 / 42
页数:10
相关论文
共 61 条
[1]   Dynamic crushing and energy absorption of regular, irregular and functionally graded cellular structures [J].
Ajdari, Amin ;
Nayeb-Hashemi, Hamid ;
Vaziri, Ashkan .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2011, 48 (3-4) :506-516
[2]   Piezomorphic Materials [J].
Alderson, Andrew ;
Alderson, Kim L. ;
McDonald, Samuel A. ;
Mottershead, Beth ;
Nazare, Shonali ;
Withers, Philip J. ;
Yao, Yong T. .
MACROMOLECULAR MATERIALS AND ENGINEERING, 2013, 298 (03) :318-327
[3]   The low velocity impact response of auxetic carbon fibre laminates [J].
Alderson, K. L. ;
Coenen, V. L. .
PHYSICA STATUS SOLIDI B-BASIC SOLID STATE PHYSICS, 2008, 245 (03) :489-496
[4]   How to make auxetic fibre reinforced composites [J].
Alderson, KL ;
Simkins, VR ;
Coenen, VL ;
Davies, PJ ;
Alderson, A ;
Evans, KE .
PHYSICA STATUS SOLIDI B-BASIC SOLID STATE PHYSICS, 2005, 242 (03) :509-518
[5]  
[Anonymous], 2003, ANN BOOK ASTM STAND, V03.01
[6]  
[Anonymous], SMART MAT STRUCT
[7]  
[Anonymous], J REINF PLAST COMPOS
[8]  
[Anonymous], INT J SOLIDS STRUCT
[9]  
[Anonymous], P 16 INT C COMP STRU
[10]  
[Anonymous], HONEYCOMB FABRICATIO