Abstract

Increasing applications of laminated composite structures necessitate the development of equivalent single layer (ESL) models that can achieve similar accuracy but are more computationally efficient than 3D or layer-wise models. Most ESL displacement-based models do not guarantee interfacial continuity of shear stresses within laminates. A possible remedy is the enforcement of interlaminar equilibrium in variational formulations, for example, in the framework of the Hellinger-Reissner variational principle, leading to a mixed force/displacement model. In this paper, the governing equations for bending and stretching of laminated beams, comprising only seven stress resultants and two displacement functionals, are obtained using global fifth-order and a local linear zigzag kinematics. As a strong-form solution technique, the differential quadrature method (DQM) is an efficient tool which can provide excellent convergence with relatively few number of grid points. However, in dealing with high-order differential equations, the conventional DQM can incur considerable errors due to the nature of numerical differentiation. Therefore, a mixed inverse differential quadrature method (iDQM) is proposed herein to solve the governing fourth-order differential equations for bending and stretching of laminated beams. This approach involves approximating the first derivatives of functional unknowns, thereby reducing the order of differentiation being performed. Using a non-uniform Chebychev-Gauss-Lobatto grid point profile, numerical results show that the accuracy of stress predictions is improved by using iDQM compared to DQM. In addition, the Cauchy’s equilibrium condition is satisfied more accurately by iDQM, especially in the vicinity of boundaries.

Highlights

  • The design of multi-layered composite structures requires accurate prediction of stress to guarantee safe design of primary loadbearing components

  • Based on a third-order zigzag displacement field and a Hellinger-Reissner (HR) mixed strain energy formulation developed previously, the governing equations and boundary conditions are rewritten in a new form which takes the first derivatives of stress resultants and displacements as primary functional unknowns

  • Fifth-order linear zigzag kinematics are added to investigate the effect of a higher-order displacement assumption on different layup configurations

Read more

Summary

Introduction

The design of multi-layered composite structures requires accurate prediction of stress to guarantee safe design of primary loadbearing components. In combination with a higher-order global displacement field (Groh and Weaver, 2015), the results from models based on zigzag kinematics match well with those from Pagano’s exact solutions or 3D finite element analysis for generally laminated beams except for discrepancies observed in the immediate vicinity of boundaries. The paper proposes a mixed iDQM to obtain the solution of the Hellinger-Reissner mixed variational formulation based on fifthorder global and linear zigzag kinematics for static analysis of both constant- and variable-stiffness laminated beams.

Higher-order zigzag displacement theory
Derivation of shear stress and transverse normal stress
Hellinger-Reissner based variational formulation for laminated beams
F F q T xx
G23 Gð1h2Þ
Numerical results and discussions
Constant stiffness laminated beams
Clamped and cantilevered beams with constant stiffness composites
Findings
Conclusions
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call