scholarly journals Zeroth-order shear deformation micro-mechanical model for composite plates with in-plane heterogeneity

2013 ◽  
Vol 50 (19) ◽  
pp. 2872-2880 ◽  
Author(s):  
Chang-Yong Lee
Keyword(s):  
Shear Deformation ◽  
Mechanical Model ◽  
Composite Plates ◽  
Zeroth Order

Zeroth-Order Shear Deformation Theory for Laminated Composite Plates

2003 ◽  
Vol 70 (3) ◽  
pp. 374-380 ◽  
Author(s):  
M. C. Ray
Keyword(s):  
Dynamic Analysis ◽  
Shear Deformation ◽  
Deformation Theory ◽  
Shear Deformation Theory ◽  
Laminated Composite ◽  
Composite Plates ◽  
High Accuracy ◽  
Laminated Composite Plates ◽  
Zeroth Order ◽  
Static And Dynamic Analysis

In this paper a zeroth-order shear deformation theory has been derived for static and dynamic analysis of laminated composite plates. The responses obtained by the theory for symmetric and antisymmetric laminates are compared with the existing solutions. The comparison firmly establishes that this new shear deformation theory can be used for both thick and thin laminated composite plates with high accuracy.

Free and forced vibration analysis of flyash/graphene filled laminated composite plates using higher order shear deformation theory

2021 ◽  
pp. 095440622110531
Author(s):  
Sarada P Parida ◽  
Pankaj C Jena
Keyword(s):  
Shear Deformation ◽  
Deformation Theory ◽  
Low Cost ◽  
Shear Deformation Theory ◽  
Laminated Composite ◽  
Composite Plates ◽  
Laminated Composite Plates ◽  
Weight Percentage ◽  
Circular Holes ◽  
Forced Vibration Analysis

The strength of the conventional composite plates can be enhanced by the use of additional fillers. These composite plates are often subjected to dynamic loading conditions which necessitate the study of their static and dynamic behavior. In this study, laminated composite plates (LCP) are fabricated by open layup process with epoxy as a base resin, E-glass fiber as reinforcement, and fillers: flyash and graphene. The fillers are included in order to improve the mechanical properties of the composite. The filler content in the composite is limited to 5% of the total volume. The weight percentage of fiber combined with fillers, treated as reinforcing constituents is limited to 60%. Graphene and flyash are added in different proportions to develop different kinds of LCPs. The free and forced vibrations of LCPs (using simple support end conditions) are measured by an indigenously developed low-cost vibration testing module. The experimental results have been used to validate the results obtained from the mathematical modeling by using fifth-order shear deformation theory and finite element approaches. Additionally, the effect of existing discontinuity in the LCP is studied. Circular holes of different dimensions at different locations are simulated in the numerical model and the consequences on modal frequencies are analyzed.

Zeroth-Order Shear Deformation Theory for Plates

AIAA Journal ◽  
10.2514/2.750 ◽  
1999 ◽  
Vol 37 (4) ◽  
pp. 524-526 ◽  
Author(s):  
Rameshchandra P. Shimpi
Keyword(s):  
Shear Deformation ◽  
Deformation Theory ◽  
Shear Deformation Theory ◽  
Zeroth Order
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