Mechanical Property and Failure Mechanism of Composite Laminates Containing a Circular Hole under Tension

ZHU Hao; GUO Zhang-Xin; SONG Lu-Bin; WANG Zhi-Hua; LI Yong-Cun

doi:10.11858/gywlxb.2017.04.004

Volume 31 Issue 4

Aug 2017

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Chinese Journal of High Pressure Physics > 2017 > 31(4): 373-381.

ZHU Hao, GUO Zhang-Xin, SONG Lu-Bin, WANG Zhi-Hua, LI Yong-Cun. Mechanical Property and Failure Mechanism of Composite Laminates Containing a Circular Hole under Tension[J]. Chinese Journal of High Pressure Physics, 2017, 31(4): 373-381. doi: 10.11858/gywlxb.2017.04.004

Citation:

ZHU Hao, GUO Zhang-Xin, SONG Lu-Bin, WANG Zhi-Hua, LI Yong-Cun. Mechanical Property and Failure Mechanism of Composite Laminates Containing a Circular Hole under Tension[J]. Chinese Journal of High Pressure Physics, 2017, 31(4): 373-381. doi: 10.11858/gywlxb.2017.04.004

Citation:

ZHU Hao, GUO Zhang-Xin, SONG Lu-Bin, WANG Zhi-Hua, LI Yong-Cun. Mechanical Property and Failure Mechanism of Composite Laminates Containing a Circular Hole under Tension[J]. Chinese Journal of High Pressure Physics, 2017, 31(4): 373-381. doi: 10.11858/gywlxb.2017.04.004

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Mechanical Property and Failure Mechanism of Composite Laminates Containing a Circular Hole under Tension

doi: 10.11858/gywlxb.2017.04.004

ZHU Hao^{1, 2
,},
GUO Zhang-Xin^{1, 2,*
,
,},
SONG Lu-Bin^{1, 2},
WANG Zhi-Hua¹,
LI Yong-Cun¹

1.
College of Mechanics, Shanxi Key Laboratory of Material Strength & Structural Impact, Taiyuan University of Technology, Taiyuan 030024, China
2.
State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi'an Jiaotong University, Xi'an 710049, China

Received Date: 29 Dec 2016
Rev Recd Date: 27 Feb 2017

Abstract

Abstract

In order to set up a three dimensional damage model for composite laminates with a circular hole, based on the failure criteria proposed by Linde et al., we at first implemented the user-defined material subroutine UMAT in the finite element code ABAQUS using the factors of fiber and matrix to characterize the gradual degradation of material.Then we used the damage model to study the mechanical property and failure mechanism of composite laminates with different ply angels, stacking sequences, hole diameters or positions subjected to uniaxial tension.The results show that the damage factors of the fiber and matrix varied differently for plies with different ply angels.In addition, the hole diameter and ply angle have significant effects on the reaction force of the composite laminates, while the influence of the hole position and stacking sequence of plies are much smaller.Our model can be used to predict qualitatively and quantitatively the progressive failure behavior of composite laminates under tension, thus it can serve as a reference for engineering application and design of composite laminates.
- composite laminates,
- damage mechanics,
- progressive failure analysis,
- numerical simulation,
- UMAT

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References(24)

References

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Mechanical Property and Failure Mechanism of Composite Laminates Containing a Circular Hole under Tension

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