Optimization of orthotropic rectangular laminates with weak interfaces under buckling
Source abstract
Abstract
Abstract The buckling of an orthotropic laminate with weak interfaces is investigated. The state-space formulations established directly from the three-dimensional theory of elasticity are employed. The present analysis is effective because the final scale of the resulting equations always keeps the same in spite of the number of layers as well as the number of weak interfaces in the laminate. To maximize the critical buckling stress of laminates with weak interface, the optimal design are performed to find the optimal design of microstructural parameters using ADS (automated design synthesis).
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Mechanical Behavior of Composites · Topology Optimization in Engineering
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References (20)
Show source-provided references
1. Turvey · 1995
2. Thermal buckling analysis of thick anisotropic composite plates by finite strip method10.12989/sem.1999.7.5.473 ↗
3. Free vibration and stability analysis of stiffened sandwich plates10.1016/S0263-8223(03)00139-9 ↗
4. Bending, vibration and buckling of simply supported thick orthotropic rectangular plates and laminates10.1016/0020-7683(70)90076-4 ↗
5. Analysis of natural frequencies of delaminated composite beams based on finite element method10.12989/sem.1996.4.3.243 ↗
6. The fabrication and failure of laminar ceramic composites10.1016/0956-7151(92)90471-P ↗
7. Fabrication and properties of laminated Al2O3/TiC composites10.1016/S0272-8842(01)00007-4 ↗
8. Theory for multilayered anisotropic plates with weakened interfaces10.1115/1.2787221 ↗
9. Effect of interfacial imperfection on buckling and bending behavior of composite laminates10.2514/3.13443 ↗
10. A general linear theory of laminated composite shells featuring interlaminar bonding imperfections10.1016/S0020-7683(00)00263-8 ↗
11. Vibration and bending of antisymmetrically angle-ply laminated plates with perfectly and weakly bonded layers10.1016/S0263-8223(01)00008-3 ↗
12. Buckling of composite plates by global–local plate theory10.1016/S1359-8368(00)00059-7 ↗
13. Assessment of computational models for multilayered composite shells10.1115/1.3119162 ↗
14. A state space approach to elasticity10.1016/0016-0032(75)90082-4 ↗
15. An exact solution for the statics and dynamics of laminated thick plates with orthotropic layer10.1016/0020-7683(90)90036-U ↗
16. Exact solutions of buckling for simply supported thick laminates
17. Free vibration of multi-layered spherically isotropic hollow sphere10.1016/S0020-7403(00)00044-8 ↗
18. Three-dimensional exact analysis of angle-ply laminates in cylindrical bending with interfacial damage via state-space method10.1016/j.compstruct.2003.08.010 ↗
19. Waves at a flexibly bonded interface10.1115/1.3607854 ↗
20. Whitney · 1987