The failure behavior of the syntactic foams is investigated based on a three-dimensional (3D) micromechanical finite element (FE) model, by varying the volume fraction, the wall thickness of the hollow particles, and the interfacial strength. The maximum principal stress criterion is adopted to determine the state (damaged or undamaged) for both interface and matrix. Material property degradation is used to describe the mechanical behavior of those damaged elements. The current model can reasonably predict the tensile strength of the syntactic foams with high volume fractions (40%–60%). The failure mechanism of the syntactic foam under uniaxial tension is captured by analyzing the stress–strain curves and the contours of damaging evolution process. Results from the quantitative simulations demonstrate that the tensile strength of the syntactic foam can be improved effectively by enhancing the interfacial strength.
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February 2015
Research-Article
Strength Analysis of Syntactic Foams Using a Three-Dimensional Continuum Damage Finite Element Model
Yejie Shan,
Yejie Shan
Department of Engineering Mechanics,
Zhejiang University
,Hangzhou 310027
, China
Research Center for Composites and Structures,
School of Aeronautics and Astronautics,
School of Aeronautics and Astronautics,
Zhejiang University
,Hangzhou 310027
, China
Search for other works by this author on:
Guodong Nian,
Guodong Nian
Department of Engineering Mechanics,
Zhejiang University
,Hangzhou 310027
, China
Research Center for Composites and Structures,
School of Aeronautics and Astronautics,
School of Aeronautics and Astronautics,
Zhejiang University
,Hangzhou 310027
, China
Search for other works by this author on:
Qiang Xu,
Qiang Xu
1
Department of Engineering Mechanics,
Zhejiang University
,Hangzhou 310027
, China
Research Center for Composites and Structures,
School of Aeronautics and Astronautics,
School of Aeronautics and Astronautics,
Zhejiang University
,Hangzhou 310027
, China
Key Laboratory of Aerospace Numerical
Simulation and Validation of Ministry
of Education of China,
e-mail: xuqiang@zju.edu.cn
Simulation and Validation of Ministry
of Education of China,
Zhejiang University
,Hangzhou 310027
, China
e-mail: xuqiang@zju.edu.cn
1Corresponding authors.
Search for other works by this author on:
Weiming Tao,
Weiming Tao
Department of Engineering Mechanics,
Zhejiang University
,Hangzhou 310027
, China
Research Center for Composites and Structures,
School of Aeronautics and Astronautics,
School of Aeronautics and Astronautics,
Zhejiang University
,Hangzhou 310027
, China
Key Laboratory of Aerospace Numerical
Simulation and Validation of Ministry
of Education of China,
Simulation and Validation of Ministry
of Education of China,
Zhejiang University
,Hangzhou 310027
, China
Search for other works by this author on:
Shaoxing Qu
Shaoxing Qu
1
Department of Engineering Mechanics,
Zhejiang University
,Hangzhou 310027
, China
Research Center for Composites and Structures,
School of Aeronautics and Astronautics,
School of Aeronautics and Astronautics,
Zhejiang University
,Hangzhou 310027
, China
Key Laboratory of Aerospace Numerical
Simulation and Validation of Ministry
of Education of China,
e-mail: squ@zju.edu.cn
Simulation and Validation of Ministry
of Education of China,
Zhejiang University
,Hangzhou 310027
, China
e-mail: squ@zju.edu.cn
1Corresponding authors.
Search for other works by this author on:
Yejie Shan
Department of Engineering Mechanics,
Zhejiang University
,Hangzhou 310027
, China
Research Center for Composites and Structures,
School of Aeronautics and Astronautics,
School of Aeronautics and Astronautics,
Zhejiang University
,Hangzhou 310027
, China
Guodong Nian
Department of Engineering Mechanics,
Zhejiang University
,Hangzhou 310027
, China
Research Center for Composites and Structures,
School of Aeronautics and Astronautics,
School of Aeronautics and Astronautics,
Zhejiang University
,Hangzhou 310027
, China
Qiang Xu
Department of Engineering Mechanics,
Zhejiang University
,Hangzhou 310027
, China
Research Center for Composites and Structures,
School of Aeronautics and Astronautics,
School of Aeronautics and Astronautics,
Zhejiang University
,Hangzhou 310027
, China
Key Laboratory of Aerospace Numerical
Simulation and Validation of Ministry
of Education of China,
e-mail: xuqiang@zju.edu.cn
Simulation and Validation of Ministry
of Education of China,
Zhejiang University
,Hangzhou 310027
, China
e-mail: xuqiang@zju.edu.cn
Weiming Tao
Department of Engineering Mechanics,
Zhejiang University
,Hangzhou 310027
, China
Research Center for Composites and Structures,
School of Aeronautics and Astronautics,
School of Aeronautics and Astronautics,
Zhejiang University
,Hangzhou 310027
, China
Key Laboratory of Aerospace Numerical
Simulation and Validation of Ministry
of Education of China,
Simulation and Validation of Ministry
of Education of China,
Zhejiang University
,Hangzhou 310027
, China
Shaoxing Qu
Department of Engineering Mechanics,
Zhejiang University
,Hangzhou 310027
, China
Research Center for Composites and Structures,
School of Aeronautics and Astronautics,
School of Aeronautics and Astronautics,
Zhejiang University
,Hangzhou 310027
, China
Key Laboratory of Aerospace Numerical
Simulation and Validation of Ministry
of Education of China,
e-mail: squ@zju.edu.cn
Simulation and Validation of Ministry
of Education of China,
Zhejiang University
,Hangzhou 310027
, China
e-mail: squ@zju.edu.cn
1Corresponding authors.
Contributed by the Applied Mechanics Division of ASME for publication in the JOURNAL OF APPLIED MECHANICS. Manuscript received September 26, 2014; final manuscript received December 11, 2014; accepted manuscript posted December 16, 2014; published online January 7, 2015. Editor: Yonggang Huang.
J. Appl. Mech. Feb 2015, 82(2): 021004 (7 pages)
Published Online: February 1, 2015
Article history
Received:
September 26, 2014
Revision Received:
December 11, 2014
Accepted:
December 16, 2014
Online:
January 7, 2015
Citation
Shan, Y., Nian, G., Xu, Q., Tao, W., and Qu, S. (February 1, 2015). "Strength Analysis of Syntactic Foams Using a Three-Dimensional Continuum Damage Finite Element Model." ASME. J. Appl. Mech. February 2015; 82(2): 021004. https://doi.org/10.1115/1.4029387
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