A study of the effective elastic modulus of a lattice truss panel structure by experimental and theoretical analysis

被引:13
作者
Zhang, Qian [1 ]
Jiang, Wenchun [1 ]
Zhao, Bing [2 ]
Luo, Yun [1 ]
Tu, Shan-Tung [3 ]
机构
[1] China Univ Petr East China, Coll Chem Engn, State Key Lab Heavy Oil Proc, Qingdao 266580, Peoples R China
[2] Beijing Aeronaut Mfg Technol Res Inst, Beijing 100024, Peoples R China
[3] East China Univ Sci & Technol, Sch Mech & Power Engn, Key Lab Pressure Syst & Safety MOE, Shanghai 200237, Peoples R China
基金
中国国家自然科学基金;
关键词
Lattice truss panel structure; Effective elastic modulus; Analytical model; SANDWICH PANEL; MECHANICAL-PROPERTIES; BENDING BEHAVIOR; PERFORMANCE; COMPRESSION; CREEP; SHEAR; FOAM;
D O I
10.1016/j.compstruct.2017.01.012
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Lattice truss panel structures (LTPS) have been widely used in engineering structures because of their high strength/density ratios. It is very essential to propose a precise method to calculate the effective elastic modulus (EEM). This paper presented a stretching model and a stretching-bending model to calculate the EEM, which have been compared with experimental results. The stretching-bending model considers the effects of seven geometrical parameters and it shows a good agreement with the experimental results, while the stretching model overestimates the results by approximately two orders of magnitudes. It has been also proved that the stretching-bending model is superior to the models expressed by the relative density. The EEM is strongly dependent on the geometrical parameters rather than the relative density only. At the same relative density, the dip angle, included angle and truss length have more considerable influences on the EEM, followed by truss thickness, truss width and node length successively. (C) 2017 Elsevier Ltd. All rights reserved.
引用
收藏
页码:130 / 137
页数:8
相关论文
共 34 条
[1]  
[Anonymous], 2005, GB T 1456
[2]   Mechanical property of lattice truss material in sandwich panel including strut flexural deformation [J].
Chen, Hailong ;
Zheng, Qing ;
Zhao, Long ;
Zhang, Yu ;
Fan, Hualin .
COMPOSITE STRUCTURES, 2012, 94 (12) :3448-3456
[3]  
Deshpande VS, 2011, ACTA MAT, V49, P1035
[4]   Multiscale structural design of columns made of regular octet-truss lattice material [J].
Elsayed, Mostafa S. A. ;
Pasini, Damiano .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2010, 47 (14-15) :1764-1774
[5]   Mechanics of advanced fiber reinforced lattice composites [J].
Fan, Hua-Lin ;
Zeng, Tao ;
Fang, Dai-Ning ;
Yang, Wei .
ACTA MECHANICA SINICA, 2010, 26 (06) :825-835
[6]   Manufacturing and testing of a CFRC sandwich cylinder with Kagome cores [J].
Fan, Hualin ;
Fang, Daining ;
Chen, Liming ;
Dai, Zheng ;
Yang, Wei .
COMPOSITES SCIENCE AND TECHNOLOGY, 2009, 69 (15-16) :2695-2700
[7]   The optimum layer number of multi-layer pyramidal core sandwich columns under in-plane compression [J].
Feng, Li-Jia ;
Wu, Lin-Zhi ;
Yu, Guo-Cai .
THEORETICAL AND APPLIED MECHANICS LETTERS, 2016, 6 (02) :65-68
[8]  
Finnegan K, 2007, INT J MATER RES, V98, P1264, DOI 10.3139/146.101594
[9]   Mechanical behaviours of composite sandwich panel with strengthened pyramidal truss cores [J].
Gao, Liang ;
Sun, Yuguo ;
Cong, Lixin ;
Chen, Peng .
COMPOSITE STRUCTURES, 2013, 105 :149-152
[10]   Failure prediction on advanced grid stiffened composite cylinder under axial compression [J].
He Jingxuan ;
Ren Mingfa ;
Sun Shiyong ;
Huang Qizhong ;
Sun Xiannian .
COMPOSITE STRUCTURES, 2011, 93 (07) :1939-1946