4.7 Article

Bending and stress responses of the hybrid axisymmetric system via state-space method and 3D-elasticity theory

期刊

ENGINEERING WITH COMPUTERS
卷 38, 期 SUPPL 2, 页码 939-961

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SPRINGER
DOI: 10.1007/s00366-020-01242-1

关键词

Circumferential initially stresses; Linear and torsional gradient elastic foundation; 3D-elasticity theory; Bending; HLNRACP/HLNRAAP

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This research investigates the bending responses of hybrid laminated nanocomposite reinforced axisymmetric circular/annular plates under mechanical loading and various types of initially stresses using three-dimensional elasticity theory. The study utilizes the state-space approach and differential quadrature method to analyze the bending characteristics of the current structure considering different boundary conditions. A parametric study shows that increasing the values of Winkler and Pasternak factors improves the system's static stability and bending behavior.
This research presents bending responses of hybrid laminated nanocomposite reinforced axisymmetric circular/annular plates (HLNRACP/ HLNRAAP) within the framework of non-polynomial under mechanical loading and various type of initially stresses via the three-dimensional elasticity theory. The current structure is on the Pasternak type of elastic foundation and torsional interaction. The state-space approach and differential quadrature method (SS-DQM) are studied to present the bending characteristics of the current structure by considering various boundary conditions. To predict the material properties of the bulk, the role of mixture and Halpin-Tsai equations are studied. For modeling the circular plate, a singular point is studied. Finally, a parametric study investigates the impacts of various types of distribution of laminated layers, stacking sequence on the stress/strain information of the HLNRACP/ HLNRAAP. Results reveal that the system's static stability and bending behavior improve due to increasing the value of Winkler and Pasternak factors, and the stress distribution becomes more uniform.

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