Parameterized mesh generation method for unidirectional composite material mesoscopic finite element model

A composite material and grid division technology, which is applied in the fields of electrical digital data processing, design optimization/simulation, special data processing applications, etc., can solve the problem of large differences in regional grid density and shape, difficulty in selecting grid size, finite element network, etc. In order to achieve the effect of ensuring accuracy, improving calculation stability, and high adjustment efficiency

Pending Publication Date: 2020-11-24
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

However, the shape and density of the finite element mesh can have a large impact on the calculation results
This effect is greater for the mesoscopic model of composite materials, because there are obvious differences in the shape and size of each part in the mesoscopic structure of composite materials. The shape varies greatly, it is difficult to ensure the orderly change of the grid in each area, and it is difficult to choose the appropriate grid size

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  • Parameterized mesh generation method for unidirectional composite material mesoscopic finite element model
  • Parameterized mesh generation method for unidirectional composite material mesoscopic finite element model
  • Parameterized mesh generation method for unidirectional composite material mesoscopic finite element model

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Embodiment Construction

[0070] In order to clarify the technical scheme and working principle of the present invention, the present invention will be further introduced below in conjunction with the accompanying drawings and specific embodiments.

[0071] A parametric meshing method for a mesoscopic finite element model of a unidirectional composite material, comprising the following steps:

[0072] Step 1: Establish a mesoscopic geometric model of the unidirectional composite material including the matrix 1, the interface layer and the fiber monofilament, such as figure 1 shown.

[0073] Step 2: Divide the mesoscopic geometric model established in Step 1 into the outer matrix area 101 and the inner square block area 4, and the specific process is as follows:

[0074] On the cross-section of the meso-geometric model, with each fiber monofilament (cross-section) as the center of a grid unit, the internal area of ​​the model is divided into a plurality of spliced ​​together, and internal square blocks...

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Abstract

The invention discloses a parameterized mesh generation method for a unidirectional composite material mesoscopic finite element model. The method is characterized by comprising the following steps of: establishing the unidirectional composite material mesoscopic geometric model comprising a matrix, an interface layer and fiber monofilaments; dividing the mesoscopic geometric model into an external matrix area and an internal square block area; segmenting the internal square block body area; and defining a division parameter represented by the number of segments as a reference of the mesh division density of the model so as to control the overall mesh density and the like of the model. According to the method, the divided grids are regular in shape and approximate in size, so that the accuracy of a finite element calculation result can be ensured; orderly change of grids in each region is guaranteed through introduced division constraints, the situation of grid change imbalance is avoided, and the calculation stability can be improved; meanwhile, the unified control of the overall grid density of the model is realized by taking a shared division parameter as a reference, and the adjustment efficiency of the grid density of the model is high.

Description

technical field [0001] The invention belongs to the technical field of composite material modeling, and in particular relates to a parametric grid division method for a unidirectional composite material mesoscopic finite element model. Background technique [0002] The mechanical behavior of composite materials is closely related to its mesostructure, so it is of great significance to study the influence of mesostructure on its mechanical behavior. Due to the complexity of the mesoscopic structure inside the composite material, the cost and workload of studying the influence of the mesoscopic structure on its mechanical behavior through the experimental method are relatively high, and because it is difficult to prepare a test sample with a specific mesoscopic structure, it is impossible to obtain a comparative analysis. Comprehensive analysis results. [0003] In the prior art, the above problems are generally solved by numerical analysis methods. Firstly, mesoscopic finite...

Claims

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Application Information

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IPC IPC(8): G06F30/23G06F113/26G06F119/14
CPCG06F30/23G06F2113/26G06F2119/14
Inventor 宋迎东于国强高希光贾蕴发杜金康董洪年
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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