Stochastic progressive failure analysis of laminated composite plates using Puck's failure criteria

2016 ◽  
Vol 23 (7) ◽  
pp. 739-757 ◽  
Author(s):  
Appaso M. Gadade ◽  
Achchhe Lal ◽  
B. N. Singh
Keyword(s):  
Failure Analysis ◽  
Progressive Failure ◽  
Laminated Composite ◽  
Composite Plates ◽  
Failure Criteria ◽  
Laminated Composite Plates ◽  
Progressive Failure Analysis

scholarly journals Progressive failure analysis of laminated composite plates

2021 ◽  
Vol 1051 (1) ◽  
pp. 012041
Author(s):  
S S N Mohd Sabee ◽  
N Yusof ◽  
Z A Rasid ◽  
H Yahaya ◽  
F Yakub ◽  
...  
Keyword(s):  
Failure Analysis ◽  
Progressive Failure ◽  
Laminated Composite ◽  
Composite Plates ◽  
Laminated Composite Plates ◽  
Progressive Failure Analysis

Progressive failure analysis of fiber-reinforced laminated composites containing a hole

2017 ◽  
Vol 27 (7) ◽  
pp. 963-978 ◽  
Author(s):  
Hadi Bakhshan ◽  
Ali Afrouzian ◽  
Hamed Ahmadi ◽  
Mehrnoosh Taghavimehr
Keyword(s):  
Failure Analysis ◽  
Failure Modes ◽  
Progressive Failure ◽  
Composite Plates ◽  
Failure Criteria ◽  
Element Analysis ◽  
Progressive Failure Analysis ◽  
Numerical Predictions ◽  
Open Hole ◽  
Failure Loads

The present work aims to obtain failure loads for open-hole unidirectional composite plates under tensile loading. For this purpose, a user-defined material model in the finite element analysis package, ABAQUS, was developed to predict the failure load of the open-hole composite laminates using progressive failure analysis. Hashin and modified Yamanda-Sun’s failure criteria with complete and Camanho’s material degradation model are studied. In order to achieve the most accurate predictions, the influence of failure criteria and property degradation rules are investigated and failure loads and failure modes of the composites are compared with the same experimental test results from literature. A good agreement between experimental results and numerical predictions was observed.

Progressive Failure Analysis of Unidirectional-Fabric Laminated Composite Joints under Pin-Loading

2007 ◽  
Vol 334-335 ◽  
pp. 1-4
Author(s):  
Jin Hwe Kweon ◽  
Hee Jin Son ◽  
Ji Young Choi ◽  
So Young Shin ◽  
Jin Ho Choi ◽  
...  
Keyword(s):  
Finite Element ◽  
Failure Analysis ◽  
Progressive Failure ◽  
Laminated Composite ◽  
Shell Element ◽  
Failure Criteria ◽  
Composite Joints ◽  
Element Analysis ◽  
Progressive Failure Analysis ◽  
Failure Loads

A two-dimensional progressive failure analysis is conducted to predict the failure loads and modes of carbon-epoxy composite joints under pin-loading. An eight-node laminated shell element is used for the finite element modeling. Post-failure stiffness is evaluated based on the complete unloading model combined with various failure criteria. The comparison of finite element and experimental results shows that the finite element analysis based on the combined maximum stress and Yamada-Sun criteria most accurately predicts the failure loads of the composite laminated joints.

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