Finite element modeling of impact shear resistance of double skin composite wall

被引:30
作者
Hossain, Khandaker M. A. [1 ]
Rafiei, Shahryar [1 ]
Lachemi, Mohamed [1 ]
Behdinan, Kamran [2 ]
Anwar, Muhammed S. [3 ]
机构
[1] Ryerson Univ, Dept Civil Engn, 350 Victoria St, Toronto, ON M5B 2K3, Canada
[2] Univ Toronto, Dept Mech & Ind Engn, 5 Kings Coll Rd, Toronto, ON, Canada
[3] Univ Toronto, Dept Engn Sci, 5 Kings Coll Rd, Toronto, ON, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
Impact loading; Profiled double skin composite wall; Finite element modeling; Experimentation; Parametric studies; STEEL SANDWICH PANELS; NUMERICAL-SIMULATION; CONCRETE STRUCTURES; PERFORMANCE; BEHAVIOR; COMPRESSION; TENSION; TESTS;
D O I
10.1016/j.tws.2016.06.002
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
This paper presents the finite element (FE) modeling of a new form of composite walling system consisting of two skins of profiled steel sheeting and an infill of concrete subjected to in-plane impact loading. Composite wall specimen tested under impact shear loading in two phases, namely Phase I and Phase II was used to develop the FE model. In Phase I, the impact test was performed repeatedly keeping the impact energy of the projectile low intentionally to capture dynamic characteristics of the wall. In Phase II, the impact test was performed once with high impact energy (using maximum projectile speed the apparatus could produce). The developed FE model was used to simulate acceleration/displacement at the top of the wall during impact, impact energy dissipation, fundamental period, stress-strain development/concentration, shear strain/rate evolution, impact duration and bounce back impact time. The FE model predicted values/responses were found to be in good agreement with those obtained from experiments. Extensive parametric studies were conducted to study the influence of varying geometric, material and sheet-concrete interface parameters governing the composite wall performance under impact loading using the developed FE model. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:101 / 118
页数:18
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