Progressive failure analysis of composite structure based on micro- and macro-mechanics models

2015 ◽  
Vol 22 (8) ◽  
pp. 2980-2988 ◽  
Author(s):  
Zhi-gang Sun ◽  
Shao-ming Ruan ◽  
Lei Chen ◽  
Ying-dong Song
Keyword(s):  
Failure Analysis ◽  
Composite Structure ◽  
Progressive Failure ◽  
Progressive Failure Analysis

Progressive Failure Analysis of Thin Walled Composite Tubes Under Low Energy Impact

2007 ◽  
Author(s):  
Chian-Fong Yen ◽  
Thomas Cassin ◽  
Joel Patterson ◽  
Matt Triplett
Keyword(s):  
Failure Analysis ◽  
Progressive Failure ◽  
Low Energy ◽  
Composite Tubes ◽  
Energy Impact ◽  
Progressive Failure Analysis ◽  
Thin Walled

Progressive failure analysis of thin-walled composite structures

2013 ◽  
Vol 95 ◽  
pp. 53-62 ◽  
Author(s):  
Diego Cárdenas ◽  
Hugo Elizalde ◽  
Piergiovanni Marzocca ◽  
Frank Abdi ◽  
Levon Minnetyan ◽  
...  
Keyword(s):  
Failure Analysis ◽  
Composite Structures ◽  
Progressive Failure ◽  
Progressive Failure Analysis ◽  
Thin Walled

Progressive Failure Analysis of Thermoplastic PE/PE Composites: Labeling of Clustered AE Signals

2013 ◽  
Vol 821-822 ◽  
pp. 1479-1483
Author(s):  
Bi Ling Yang ◽  
Sen Liu ◽  
Xiao Xia He ◽  
Shao Qiong Zheng
Keyword(s):  
Failure Analysis ◽  
Progressive Failure ◽  
Tensile Load ◽  
Matrix Cracking ◽  
Thermoplastic Composites ◽  
Damage Mechanisms ◽  
Progressive Failure Analysis ◽  
Fast Fourier Transform Analysis ◽  
Static Tensile ◽  
Ae Signals

Thermoplastic self-reinforced polyethylene (PE/PE) composites were tested under quasi-static tensile load and the failure processes weremonitored by Acoustic Emission (AE) technique. The AE signals were collected and clustered by Unsupervised Pattern Recognition (UPR) scheme. The initiation and progression of the damage mechanisms in the composites can then be reviewed by the cumulative AE hits of each cluster versus strain curves. But the labeling of each cluster is crucial to the failure analysis. The paper focuses on this correlating between the obtained clusters and their specific damage modes. This was carried out by waveform visualization and Fast Fourier Transform analysis. Pure resin and fiber bundles were tested to assist in the labeling of signal classes in the composites (90°, 0° and [±45°] specimens). Typical waveforms of matrix cracking, fiber-matrix debonding, fiber fracture and fiber pullout were indentified respectively. The evolution process of various damage mechanisms in the composites revealed that the correlating method was effective. An objective and repeatable analytical procedure is established for the investigation of progressive failure mechanisms in the thermoplastic composites.

scholarly journals Progressive Failure Analysis in Open-Hole Tensile Composite Laminates of Airplane Stringers Based on Tests and Simulations

2020 ◽  
Vol 11 (1) ◽  
pp. 185
Author(s):  
Jian Shi ◽  
Mingbo Tong ◽  
Chuwei Zhou ◽  
Congjie Ye ◽  
Xindong Wang
Keyword(s):  
Failure Analysis ◽  
Composite Laminates ◽  
Progressive Failure ◽  
Tensile Load ◽  
Fiber Failure ◽  
Stress Criterion ◽  
Progressive Failure Analysis ◽  
Analysis Technique ◽  
Open Hole ◽  
Failure Types

The failure types and ultimate loads for eight carbon-epoxy laminate specimens with a central circular hole subjected to tensile load were tested experimentally and simulated using two different progressive failure analysis (PFA) methodologies. The first model used a lamina level modeling based on the Hashin criterion and the Camanho stiffness degradation theory to predict the damage of the fiber and matrix. The second model implemented a micromechanical analysis technique coined the generalized method of cells (GMC), where the 3D Tsai–Hill failure criterion was used to govern matrix failure, and the fiber failure was dictated by the maximum stress criterion. The progressive failure methodology was implemented using the UMAT subroutine within the ABAQUS/implicit solver. Results of load versus displacement and failure types from the two different models were compared against experimental data for the open hole laminates subjected to tensile displacement load. The results obtained from the numerical simulation and experiments showed good agreement. Failure paths and accurate damage contours for the tested specimens were also predicted.

Sign in / Sign up

Export Citation Format

Share Document