Exact(1)
In this paper, we employ the slip zone model in composite structure and strength theory to acquire the stress evolution, and then fundamentally and quantitatively explain the interfacial failure behaviors of such flexible electronic devices.
Similar(59)
The work presented in this paper is focused on damage modeling in composite items of aeronautical structures.
Our performance evaluation method is based on executable streaming data application workload model specified as UML activity diagrams and abstract platform performance model specified in composite structure diagrams.
A method based on the Refined Zigzag Theory (RZT) to model delamination in composite laminated beam structures is presented.
A numerical method based on the Refined Zigzag Theory (RZT) to model delamination in composite laminated plate/shell structures is presented.
The static and fatigue experimental results are compared with established models in composites analysis and with the available data in composite databases.
In order to demonstrate the capabilities of the proposed model in optimizing composite floor system designs, two design examples taken from the literature are studied.
In particular, it is widely reported that no efficient guidelines for modelling imperfections in composite structures are available.
The results of the adjusted multivariate GEE linear regression model examining change in composite NEI VFQ-25 score after cataract surgery are presented in Table 4.
Damage modeled in the composite is matrix cracking.
Utilizing the proposed method, the results of extensive computer simulations of conduction in model composite materials, in which the conductance distribution is broad and contains long-range correlations, are reported.
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