journal article·2001-02

Modelling of perfectly and weakly bonded laminated plates and shallow shells

Kostas P. Soldatos, Xiaoping Shu

Composites Science and Technology· Volume 61· Issue 2
Publisher page

Abstract

An model suitable for the accurate stress analysis of laminated plates and shallow shells with perfectly or weakly bonded layers is developed within the framework of the theory of elasticity. A six-degrees-of-freedom displacement field is employed and both the transverse deformation and the interfacial bonding conditions are accounted for by means of a set of three shape functions of the transverse co-ordinate parameter. These are determined on the basis of three-dimensional elasticity considerations and account for the weak interfacial bonding conditions. The model makes use of only six equations of equilibrium which are obtained variationally. Upon assuming that linearized interfacial constitutive relations describe quite adequately the initial stages of delamination, closed-form solutions are obtained for simply supported rectangular plates and shell panels made of specially orthotropic layers. The effects of opening delamination and shear slip are discussed and some interesting observatons are made through the numerical results obtained.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Composite Structure Analysis and Optimization · Mechanical Behavior of Composites · Structural Load-Bearing Analysis

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (23)

Show source-provided references
1. Layered beam system with interlayer slip10.1061/JSDEAG.0002116 ↗
2. Shear-deformable two-layer plate theory with interlayer slip
3. Interlayer shear slip theory for cross-ply laminates with nonrigid interfaces10.2514/3.11028 ↗
4. Theory for multilayered anisotropic plates with weakened interfaces10.1115/1.2787221 ↗
5. Effect of interfacial imperfection on buckling and bending behavior of composite laminates10.2514/3.13443 ↗
6. Modelling of weakly bonded laminated composite plates at large deflections10.1016/S0020-7683(96)00192-8 ↗
7. Nonlinear theory for composite laminated shells with interfacial damage10.1115/1.2789115 ↗
8. A geometrically nonlinear theory of multilayered plate with interlayer slips10.2514/2.23 ↗
9. On the modelling of laminated composite structures featuring interlaminae imperfections10.1016/S0922-5382(97)80041-4 ↗
10. Effects of interfacial damage on the global and local static response of cross-ply laminates10.1023/A:1018649824301 ↗
11. Stress analysis of imperfect composite laminates with an interlaminar bonding theory10.1002/nme.1620371608 ↗
12. A general theory for laminated plates with delaminations10.1016/S0020-7683(96)00131-X ↗
13. A generalized multilength scale nonlinear composite plate theory with delamination10.1016/S0020-7683(98)00138-3 ↗
14. A method for improving the stress analysis performance of one- and two-dimensional theories for laminated composites10.1007/BF01178408 ↗
15. A general four-degrees-of-freedom theory suitable for the accurate stress analysis of homogeneous and laminated composite beams10.1016/S0020-7683(96)00170-9 ↗
16. Accurate stress analysis of laminated plates combining a two- dimensional theory with the exact three-dimensional solution for simply supported edges10.1177/108128659700200405 ↗
17. On the stress analysis of cross-ply laminated plates and shallow shell panels10.1016/S0263-8223(99)00061-6 ↗
18. Cylindrical bending of angle-ply laminates subjected to different sets of edge boundary conditions10.1016/S0020-7683(99)00144-4 ↗
19. A continuum model for void nucleation by inclusion debonding10.1115/1.3173064 ↗
20. An analysis of decohesion along an imperfect interface10.1007/BF00018611 ↗
21. Formulation, identification, and use of interface models in the numerical analysis of composite delamination10.1016/0020-7683(93)90154-Y ↗
22. Bending, vibration and buckling of simply supported thick orthotropic rectangular plates and laminates10.1016/0020-7683(70)90076-4 ↗
23. Pagano · J. Comp. Mater. · 1970 · 4 · 2010.1177/002199837000400102 ↗