Study on shear postbuckling failure of composite sandwich plates by a quasi-conforming finite element method
Source abstract
Abstract
Abstract A quasi-conforming triangular sandwich plate element with 7 degrees of freedom (DOF) per node is established based on a simplified Zig-Zag model and a transverse shear deformation theory. The accuracy of the proposed element has been validated to be equivalent to the element based on the complete Zig-Zag model (11 DOF per note). The path-following method, proposed by Huang and Atluri, is improved and applied to follow complex postbuckling paths with secondary bifurcation points and progressive failure. A finite element (FE) modeling is completed to study the shear postbuckling behavior and failure of composite sandwich plates, based on the energy criterion of stability and the strength criterion of each layer. The basic characteristics of the shear postbuckling and failure are illustrated. The complexity and computation difficulty caused by secondary bifurcations and multi-paths are discussed. Numerical examples show that the proposed method is efficient in improving the convergence of iterations.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Structural Analysis and Optimization · Structural Load-Bearing Analysis
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (20)
Show source-provided references
1. Reddy · 2004
2. Buckling and postbuckling of composite structures10.1016/0010-4361(95)91382-F ↗
3. Insight into the shear behaviour of composite sandwich panels with foam core10.1016/j.matdes.2013.03.016 ↗
4. Experimental and numerical evaluation of the mechanical behaviour of GFRP sandwich panels10.1016/j.compstruct.2006.10.007 ↗
5. Finite element modeling strategies for sandwich composite laminates under compressive loading10.1016/j.oceaneng.2013.01.031 ↗
6. Buckling and postbuckling of stiff lamellae in a compliant matrix10.1016/j.compscitech.2014.05.015 ↗
7. Recent developments in finite element analysis for laminated composite plates10.1016/j.compstruct.2008.02.014 ↗
8. Predicting the buckling load of anisotropic sandwich panels: an approach including shear deformation of the faces10.1016/S0263-8223(98)00067-1 ↗
9. Postbuckling behavior of face/core debonded composite sandwich plate considering matrix crack and contact effect10.1016/S0263-8223(02)00098-3 ↗
10. A new trigonometric zigzag theory for buckling and free vibration analysis of laminated composite and sandwich plates10.1016/j.compstruct.2014.05.002 ↗
11. A simple method for the calculation of postcritical branches10.1108/eb023727 ↗
12. A general procedure for the direct computation of turning and bifurcation points10.1002/nme.1620300110 ↗
13. Nonlinear elastic buckling and postbuckling analysis of cylindrical panels10.1016/j.finel.2014.12.001 ↗
14. A simple method to follow post-buckling paths in finite element analysis10.1016/0045-7949(94)00623-B ↗
15. A quasi-conforming triangular laminated composite shell element based on a refined first-order theory10.1007/BF00350231 ↗
16. On the propagation of flexural waves in an orthotropic laminated plate and its response to an impulsive load10.1177/002199837100500302 ↗
17. Shear correction factor for orthotropic laminates under static load10.1115/1.3422950 ↗
18. Experimental and numerical evaluation of the mechanical behaviour of GFRP sandwich panels10.1016/j.compstruct.2006.10.007 ↗
19. Current trends in the theory of buckling
20. Bai · 2002