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Calculation method for predicting elastic behavior of compressible-incompressible composite material

A technology of composite materials and calculation methods, which is applied in the calculation field of predicting the elastic behavior of compressible-incompressible composite materials, can solve problems such as shear self-locking problems, non-physical stress oscillations, and elastic problems of double-layer composite structures that cannot be calculated. Achieve the effect of stable calculation results and simple program implementation

Active Publication Date: 2022-04-12
CALCULATION AERODYNAMICS INST CHINA AERODYNAMICS RES & DEV CENT
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, the research on the linear elasticity of incompressible materials mostly uses analytical methods, finite element (FEM), and lattice-type / lattice-type finite volume methods (CC-FVM / CV-FVM) for calculation, mainly for isotropic homogeneous The existing problems of mass / functional gradient incompressible materials mainly include: 1. When FEM calculates the elastic problems of composite materials or incompressible materials, there will be non-physical oscillation of the stress along the thickness direction near the material interface or the self-locking problem of unit shear ;2. The analytical method is only suitable for simple structure distribution and material distribution, and the real material structure cannot be calculated; 3. When CC-FVM calculates the elastic problem of composite materials, false stress jumps appear at the material interface
Compared with the above methods, CV-FEM shows better calculation performance in calculating functional materials and compressible materials, which can effectively avoid false stress and shear self-locking phenomenon. However, this method is currently suitable for calculating compressible or compressible materials. Elasticity problems with incompressible material distributions cannot yet be calculated for elastic problems with compressible-incompressible (or compressible-nearly incompressible) bilayer composite structures (see figure 1 )

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  • Calculation method for predicting elastic behavior of compressible-incompressible composite material

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Embodiment 1

[0071] Example 1: A computational method for predicting the elastic behavior of compressible-incompressible composite materials comprising:

[0072] Step 1, labeling of unit material properties and assignment of unit variables to be solved;

[0073] Step 2, obtaining the discrete form of the elastic equation of the compressible-incompressible bilayer composite material;

[0074] Step 3, obtain the element central stress.

Embodiment 2

[0075] Embodiment 2: On the basis of Embodiment 1, in step 1, include the sub-step: S1, given the way of laying the composite material, and using the multi-grid method to store it in the center of the unit, storing the hydrostatic pressure to be solved At the element center, mark whether the discrete element is a composite interface element or an internal element.

Embodiment 3

[0076] Embodiment 3: On the basis of Embodiment 1, in step 2, include the sub-step: S2, based on the governing equation of the lattice-type FVM discrete elastic problem, use the intrinsic relationship of compressible material or incompressible material for the internal control body Introduce, when controlling the volume line integral of the discrete element at the interface, the material intrinsic relationship is introduced segmentally according to the element attribute mark, and the discrete equation is solved to obtain the displacement at the element node and the hydrostatic pressure distribution at the element center.

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Abstract

The invention discloses a calculation method for predicting the elastic behavior of a compressible-incompressible composite material, and belongs to the field of composite material calculation, and the method comprises the steps: 1, marking the attributes of a unit material, and distributing the to-be-solved variables of the unit; 2, obtaining a discrete format of an elastic equation of the compressible-incompressible double-layer composite material; and step 3, obtaining the central stress of the unit. According to the method, the problems of shear self-locking occurring when the FEM is used for solving the incompressible material problem and false stress concentration occurring when the FEM is used for solving the composite material can be avoided, the elastic behavior prediction of the incompressible-compressible double-layer composite material can be realized, the elastic distribution of different material domains can be directly obtained, iterative calculation is not needed, the calculation result is stable, the program implementation is simple, and the method is suitable for popularization and application. And a functional incompressible-compressible material can be directly solved.

Description

technical field [0001] The invention relates to the field of composite material calculation, and more specifically, to a calculation method for predicting the elastic behavior of compressible-incompressible composite materials. Background technique [0002] With the continuous development of rubber-like materials (polymers, living tissues, functional materials) in engineering and biomedical fields, and incompressible materials may exhibit completely different mechanical properties from compressible materials, the problem of linear elasticity of incompressible materials The research has become a hot issue concerned by scholars from all walks of life. Incompressibility means that the volume of an object remains unchanged under any stress state (isovolumetric deformation). Poisson's ratio for an isotropic incompressible elastic body with a finite modulus ν Equal to 0.5, the expression form is that the bulk modulus of the elastic body is infinite, and only volume deformation c...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/20G16C60/00G16C10/00G06F113/26G06F119/14
CPCY02T90/00
Inventor 刘琦刘磊杜雁霞邱芷葳杨肖峰魏东
Owner CALCULATION AERODYNAMICS INST CHINA AERODYNAMICS RES & DEV CENT