Proceedings of the 3rd Annual International Conference on Mechanics and Mechanical Engineering (MME 2016)

Fracture Behavior Investigation of the Propellant Material Using the Extended Finite Element Method

Authors
Li Zhang, Jin-Zhao Huang, Zhi Lv
Corresponding Author
Li Zhang
Available Online December 2016.
DOI
10.2991/mme-16.2017.14How to use a DOI?
Keywords
Crack propagation process, Extended Finite Element Method (XFEM), Propellant material.
Abstract

When simulating crack propagation process using the finite element method, we need to create singularity grids at the crack tip. And with the increase in crack length, we need a re-division of grids. This makes the calculation very complicated. The extended finite element method (XFEM) is an effective method for simulating crack extension. And the crack is independent of the grids. Because there is no complicated grid at the crack tip in the XFEM model, the computation efficiency can be increased greatly. This paper investigated the fracture behavior of the propellant material with an initial crack using XFEM. By comparing with existing experimental results, this paper shows that XFEM can be used to simulate fracture characteristic of the propellant material efficiently.

Copyright
© 2017, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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Volume Title
Proceedings of the 3rd Annual International Conference on Mechanics and Mechanical Engineering (MME 2016)
Series
Advances in Engineering Research
Publication Date
December 2016
ISBN
10.2991/mme-16.2017.14
ISSN
2352-5401
DOI
10.2991/mme-16.2017.14How to use a DOI?
Copyright
© 2017, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

Cite this article

TY  - CONF
AU  - Li Zhang
AU  - Jin-Zhao Huang
AU  - Zhi Lv
PY  - 2016/12
DA  - 2016/12
TI  - Fracture Behavior Investigation of the Propellant Material Using the Extended Finite Element Method
BT  - Proceedings of the 3rd Annual International Conference on Mechanics and Mechanical Engineering (MME 2016)
PB  - Atlantis Press
SP  - 110
EP  - 115
SN  - 2352-5401
UR  - https://doi.org/10.2991/mme-16.2017.14
DO  - 10.2991/mme-16.2017.14
ID  - Zhang2016/12
ER  -