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Finite element numerical model debugging method based on grid structure

A grid structure and numerical model technology, applied in the direction of electrical digital data processing, special data processing applications, instruments, etc., can solve problems such as time-consuming, model errors, errors that need to be eliminated one by one, repeated repeatedly, etc., to achieve Overcoming time-consuming and laborious effects

Inactive Publication Date: 2011-05-18
HOHAI UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the construction of models under complex conditions such as dam abutments, large underground caverns, and complex components, due to the complex geometric conditions of the structures and the influence of the intersecting relationship of the structural plane space, a little carelessness may cause errors in the model, making the calculation The result is distorted and cannot even be calculated
In order to find out the source of the error, the common method is to check from the point-line-surface modeling process, and to traverse in a certain order, such as point-by-point, line-by-line, and surface-by-surface inspection along the coordinate axis of the model ; If there are many errors in the model, it needs to be eliminated one by one, and repeated many times. It is relatively easy for a simple finite element model. If the number of nodes and elements of the finite element model is tens of thousands or even hundreds of thousands or millions, use ordinary models to check for errors The method seems powerless, not only consumes a lot of time, but also reworks many times, causing researchers to lose patience

Method used

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  • Finite element numerical model debugging method based on grid structure
  • Finite element numerical model debugging method based on grid structure
  • Finite element numerical model debugging method based on grid structure

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Experimental program
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Embodiment 1

[0046] Step 2 Number the surface elements in the 2 hexahedral 8-node units, the 6 surface elements of unit 1 are 1 2 3 4; 2 6 7 3; 3 7 8 4; 4 8 5 1; 1 5 6 2; 5 8 7 6; the 6 bins of unit 2 are 2 9 10 3; 9 12 11 10; 10 11 7 3; 3 7 6 2; 2 6 12 9; 6 7 11 12. Panels are numbered sequentially 1-12.

[0047] Among the 12 bins, there is no bin with zero area, n0=0.

[0048] Model left boundary xmin=0; model right boundary xmax=20; model front boundary ymin=0; model rear boundary ymax=10; model upper boundary ymax=10; model lower boundary ymin=0.

[0049] Among the 12 spatial elements, Nos. 1 and 7 are the lower boundary elements, No. 6 and 12 are the upper boundary elements, No. 4 is the left interface element, No. 8 is the right interface element, and No. 5 and 11 are the The front boundary interface, No. 3 and 9 are the rear boundary interface. The total number of boundary surface elements is n1=10, and the remaining surface elements are 2.

[0050] Step 3 Among the 2 remaining ...

Embodiment 2

[0053] (1) Classify the finite element grid information into node information and unit structure information, including the number of nodes and units, node coordinates, unit structure shape, information on building unit structure by node numbers; the total number of nodes is 38954, and the total number of units for 184336.

[0054] (2) Transform tetrahedral elements and triangular prism elements into hexahedral 8-node elements. Split each 6-hedron 8-node unit into 6 space elements, analyze the properties of each surface element, and eliminate the surface elements with obvious characteristics (zero area and boundary surface elements).

[0055] (3) Perform grid self-retrieval. Analyze whether each unit body satisfies the rules of numerical calculation through the surface element correspondence of each unit body. By judging whether each surface element is shared by two or more unit bodies, if a certain surface element is only used by one unit body, it is a Potential error bins ...

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Abstract

The invention relates to a finite element numerical model debugging method based on a grid structure, which comprises the following steps of: dividing a geologic model into a plurality of tetrahedron four-node, pentahedron six-node and hexahedron eight-node grid objects; converting the tetrahedron four-node and pentahedron six-node grid objects into hexahedron eight-node grid objects; classifying unit information by using the hexahedron eight-node grid objects and the hexahedron eight-node grid objects which are obtained by converting the tetrahedron four-node and pentahedron six-node grid objects as units to obtain node and structure information;; numbering the nodes according to the node position and the anticlockwise sequence from bottom to top; numbering plane elements in all the hexahedron eight-node units, i.e. making all nodes point to the inner part of the unit according to the right hand rule; combining the node number in the plane elements to obtain the plane element code; and carrying out area retrieval in 6*ne plane elements and removing zero-area plane elements, left, right, front, back, upper and lower boundaries and public plane elements, wherein the residual plane element is the probable model error position.

Description

technical field [0001] The invention relates to the preprocessing part in the field of engineering numerical analysis such as civil engineering. Background technique [0002] Numerical simulation technology is an important means of mechanical analysis in civil engineering, and geological modeling is the main component of the pre-processing of numerical simulation technology. In the construction of models under complex conditions such as dam abutments, large underground caverns, and complex components, due to the complex geometric conditions of the structures and the influence of the intersecting relationship of the structural plane space, a little carelessness may cause errors in the model, making the calculation The result is distorted and cannot even be calculated. In order to find out the source of the error, the common method is to check from the point-line-surface modeling process, and to traverse in a certain order, such as point-by-point, line-by-line, and surface-by...

Claims

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Application Information

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IPC IPC(8): G06F17/50
Inventor 石崇徐卫亚聂卫平
Owner HOHAI UNIV
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