journal article·2018-03

Buckling analysis of bilayer beam-columns with an asymmetric delamination

Qinghui Liu, Pizhong Qiao

Publisher page

Abstract

Abstract A general analytical model is developed to evaluate buckling behavior of a bilayer beam-column with a through-the-width asymmetric delamination under simply supported boundary conditions . Both transverse shear deformation and local deformation at delamination tip are taken into account in the model by considering two sublayers in both delaminated and intact regions as two individual shear deformable ones. Interface continuity conditions , which account for effect of interface normal and shear stresses, are also introduced in the intact regions. Furthermore, the present model is capable of dealing with the case of delamination located arbitrary through thickness and along length of beam-columns. In comparisons with the results of classical Euler-Bernoulli beam model, Timoshenko beam model (rigid joint model) and finite element analysis , better agreements are achieved for the present flexible joint model, which captures local deformation at delamination tip due to consideration of interface normal and shear stress components. Parametric studies are conducted to evaluate influences of sublayer thickness ratio , delamination length, delamination location, specimen length, and material parameters on the critical buckling strain with emphasis on transverse shear deformation and local deformation at delamination tip. The developed model can be used with confidence in buckling analysis of layered structures with an arbitrary delamination through the length and thickness.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Mechanical Behavior of Composites · Structural Load-Bearing Analysis · Structural Response to Dynamic Loads

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

References (30)

Show source-provided references
1. Slenderness limit for hybrid FRP-concrete columns10.1061/(ASCE)1090-0268(2001)5:1(26) ↗
2. Cross laminated timber (CLT): overview and development10.1007/s00107-015-0999-5 ↗
3. Numerical analysis of the damage behavior of an aluminum/CFRP hybrid beam under three point bending10.1016/j.compositesb.2013.08.030 ↗
4. Bending, buckling and free vibration of laminated composite and sandwich beams: a critical review of literature10.1016/j.compstruct.2017.03.053 ↗
5. A finite element framework for the interplay between delamination and buckling of rubber-like bi-material systems and stretchable electronics10.1016/j.jeurceramsoc.2016.01.002 ↗
6. Growth from buckling to buckling-driven delamination in a film/substrate system10.1016/j.compstruct.2017.04.062 ↗
7. One dimensional modelling of failure in laminated plates by delamination buckling10.1016/0020-7683(81)90014-7 ↗
8. Effect of delamination of axially loaded homogeneous laminated plates10.2514/3.9104 ↗
9. Delamination buckling and growth of flat, cross-ply laminates10.1016/0263-8223(85)90033-9 ↗
10. Postbuckling behavior of composite plates with through-the-width delaminations10.1016/j.tws.2008.01.005 ↗
11. Buckling analysis of two-layer beams with an asymmetric delamination10.1016/j.engstruct.2004.01.003 ↗
12. Buckling and postbuckling of delaminated composites under compressive loads including transverse shear effects10.2514/3.9894 ↗
13. Shear deformation theory for compressive delamination buckling and growth10.2514/3.10661 ↗
14. Delamination buckling analysis of general laminated composite beams by differential quadrature method10.1016/S1359-8368(99)00011-6 ↗
15. Stability analysis of composite plates with through-the-width delamination10.1061/(ASCE)EM.1943-7889.0000205 ↗
16. Compressional stability behavior of composite plates with through-the-width and embedded delaminations by using first order shear deformation theory10.1016/j.compstruc.2010.10.016 ↗
17. Buckling analysis of delaminated composite plates using a novel layerwise theory10.1016/j.tws.2013.08.008 ↗
18. Closed form solutions of Euler-Bernoulli beams with singularities10.1016/j.ijsolstr.2004.09.048 ↗
19. Energy release rates for the ENF specimen using a beam on an elastic foundation10.1177/002199839502901101 ↗
20. Mode separation of energy release rate for delamination in composite laminates using sublaminates10.1016/S0020-7683(00)00172-4 ↗
21. Interface crack between two shear deformable elastic layers10.1016/S0022-5096(03)00121-2 ↗
22. Mechanics and fracture of crack tip deformable bi-material interface10.1016/j.ijsolstr.2004.06.006 ↗
23. On the calculation of energy release rate and mode mixity in delaminated laminated beams10.1016/j.engfracmech.2016.08.010 ↗
24. The buckling of a delaminated sublaminate on an elastic foundation10.1177/002199838702101202 ↗
25. Buckling of delaminated composites re-examined10.1016/0266-3538(93)90093-V ↗
26. Mechanics of bimaterial interface: shear deformable split bilayer beam theory and fracture10.1115/1.1978920 ↗
27. Local delamination buckling of laminated composite beams using novel joint deformation models10.1061/(ASCE)EM.1943-7889.0000093 ↗
28. Buckling of delaminated bi-layer beam-columns10.1016/j.ijsolstr.2011.04.020 ↗
29. Reddy · 2004
30. Novel beam analysis of end notched flexure specimen for mode-II fracture10.1016/S0013-7944(03)00096-1 ↗