Strain rate dependence of damage evolution in syntactic foams

被引:48
作者
Shunmugasamy, Vasanth Chakravarthy [1 ]
Gupta, Nikhil [1 ]
Nguyen, Nguyen Q. [2 ]
Coelho, Paulo G. [3 ]
机构
[1] NYU, Polytech Inst, Mech & Aerosp Engn Dept, Composite Mat & Mech Lab, Brooklyn, NY 11201 USA
[2] Stevens Inst Technol, Dept Mech Engn, Design & Mfg Inst, Hoboken, NJ 07030 USA
[3] NYU, Dept Biomat & Biomimet, New York, NY 10010 USA
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 2010年 / 527卷 / 23期
基金
美国国家科学基金会;
关键词
Mechanical testing; Particulate reinforced composites; Polymer matrix composites; Fracture; High strain rate testing; MICRO-CT; COMPRESSIVE PROPERTIES; BEHAVIOR; DENSITY; FEATURES; MICROTOMOGRAPHY; DEFORMATION; COMPOSITES; STRENGTH;
D O I
10.1016/j.msea.2010.06.021
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The present study focused on determining the effect of high strain rate loading on the deformation and fracture characteristics of syntactic foams and relating them with the initial foam microstructure. The high strain rate testing was carried out using a split-Hopkinson pressure bar system and the damage evaluation was carried out using microCT-scan and scanning electron microscope. The strength was found to be 50-150% higher at high strain rates when compared to quasi-static values for various grades of syntactic foams. Damage evaluation revealed crushing of particles in the surface layer, shear cracking, and propagation of longitudinal cracks as the main fracture modes at different strain rates and material compositions. Wall thickness and volume fraction of hollow particles used in syntactic foams played an important role in determining the failure mechanism. At low strain rates shear cracking of specimens was prominent, whereas at high strain rates longitudinal cracks were the main failure mode. Understanding the strain rate dependence of failure mechanisms is important for aerospace applications of these lightweight composites. (C) 2010 Elsevier B.V. All rights reserved.
引用
收藏
页码:6166 / 6177
页数:12
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