CN110750933B - An Accurate Interface Tracking Processing Method Coupling Lagrange Particles and Euler's Method - Google Patents

An Accurate Interface Tracking Processing Method Coupling Lagrange Particles and Euler's Method Download PDF

Info

Publication number
CN110750933B
CN110750933B CN201911010698.4A CN201911010698A CN110750933B CN 110750933 B CN110750933 B CN 110750933B CN 201911010698 A CN201911010698 A CN 201911010698A CN 110750933 B CN110750933 B CN 110750933B
Authority
CN
China
Prior art keywords
grid
particle
pressure
stress
calculate
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201911010698.4A
Other languages
Chinese (zh)
Other versions
CN110750933A (en
Inventor
许香照
宁建国
马天宝
李健
任会兰
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Beijing Institute of Technology BIT
Original Assignee
Beijing Institute of Technology BIT
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Beijing Institute of Technology BIT filed Critical Beijing Institute of Technology BIT
Priority to CN201911010698.4A priority Critical patent/CN110750933B/en
Publication of CN110750933A publication Critical patent/CN110750933A/en
Application granted granted Critical
Publication of CN110750933B publication Critical patent/CN110750933B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)

Abstract

本发明涉及一种耦合Lagrange质点和Euler方法的精确界面追踪处理方法,属于计算爆炸力学领域。该方法包括1、针对所需要分析的创建仿真模型,并对所创建的仿真模型进行初始化设置;2、在所设定的每一个时间步内,计算网格的人工粘性值、应力张量及网格速度更新量。3、确定网格与质点之间的拓扑关系以实现网格物理量映射至质点;4、确定质点移动的位置;5、确定移动后质点与网格之间的拓扑关系以实现质点物理量映射至网格;6、计算仿真模型所对应的状态方程以及控制方程;7、更新所述仿真模型在计算域边界处的网格和质点物理量。本发明很好地处理了材料大变形及动态破坏过程,有效地实现了爆炸与冲击问题的精确数值模拟计算。

Figure 201911010698

The invention relates to an accurate interface tracking processing method coupling Lagrange particle and Euler method, and belongs to the field of computational explosion mechanics. The method includes 1. creating a simulation model for the required analysis, and initializing the created simulation model; 2. calculating the artificial viscosity value, stress tensor and Mesh velocity update amount. 3. Determine the topological relationship between the grid and the particle to realize the mapping of the physical quantity of the grid to the particle; 4. Determine the position where the particle moves; 5. Determine the topological relationship between the moving particle and the grid to realize the mapping of the physical quantity of the particle to the grid 6. Calculate the state equation and control equation corresponding to the simulation model; 7. Update the grid and particle physical quantities of the simulation model at the boundary of the computational domain. The invention handles the large deformation and dynamic failure process of the material well, and effectively realizes the accurate numerical simulation calculation of explosion and impact problems.

Figure 201911010698

Description

Accurate interface tracking processing method for coupling Lagrange particles and Euler method
Technical Field
The invention relates to an accurate interface tracking processing method for coupling Lagrange particles and a Euler method, and belongs to the field of computational explosion mechanics.
Background
Computer numerical simulation has gradually become an important means to solve complex problems in engineering applications and scientific computing. The computer numerical simulation test technology has the advantages of safety, confidentiality, flexible design, good repeatability, controllable environment and process, high cost effectiveness ratio and the like, has important functions and significance for understanding the nature of problems and establishing theoretical models, and is an effective means for improving the research and development of weapons and ammunition and the prevention and rescue level of explosion disasters in the future. In addition, the numerical simulation is not restricted by external environment and conditions, the change rule of each physical quantity under different conditions can be researched, and the limitation of experiment and theoretical research can be broken through. With the continuous improvement of computer hardware performance and the development of parallel technology, the scale and efficiency of solving problems by using a numerical simulation method are greatly improved, and the method is more and more widely applied to the research of explosion problems.
The explosion and impact problems are transient dynamics problems related to extreme conditions such as high strain rate, high temperature, high pressure, phase change, mutual coupling and even mixing among various media such as gas, liquid and solid, severe deformation and even breakage of materials and the like. Under these extreme conditions, numerical simulation of explosion and shock problems becomes very difficult, requiring the handling of large deformations of the material, interfaces of various substances and various strong discontinuities, much more complex than the usual fluid, aerodynamic and structural dynamics problems. The Euler method is a preferred method for solving the problems, and the core idea is that a fixed space coordinate system is adopted, materials flow in and out through a grid boundary, and the large deformation of the materials does not directly influence numerical calculation, so that the large deformation problem can be naturally processed, but the problem of interface processing among multiple materials is accompanied, and the precision of the method on tracking the material interface is not higher than that of the Lagrange method.
Later, a coupling algorithm combining the advantages of the Euler method and the Lagrange method, namely an ale (arbitrary Lagrangian eulerian) method, has appeared, the idea of which is mainly based on the Lagrange method, a large deformation problem of a Euler grid processing grid is locally introduced, but the Euler grid processing grid can only process a local area, and a lot of difficulties are still faced to solve transient problems with large deformation, such as explosive shock waves and deep penetration. In recent years, various high-precision algorithms have appeared, which can better deal with the material interface problem and effectively improve the material interface resolution, representative examples of which are tvd (total Variation digital), ENO (essential Non-oscillotory), weno (weighted ENO), and the like, but the solution of the algorithms is more complicated and the calculation time is increased rapidly; meanwhile, various non-grid methods mainly including an SPH smooth particle fluid dynamics method, a unitless Galerkin method, a Material Point Method (MPM), and the like, are also gradually becoming hot points for research in the fields of computational fluid dynamics and computational explosion dynamics, and the non-grid method has advantages in tracking material flow, but for large-scale scientific problems, an increase in computational scale causes a rapid increase in computational load, and under certain hardware conditions, a program is deadlocked and has a long computational duration.
Disclosure of Invention
The invention aims to solve the problem that the Euler method is difficult to clearly track the motion history of a multi-material interface, and provides an accurate interface tracking processing method for coupling Lagrange particles with the Euler method.
The method has the advantages that the Euler method is easy to handle the problem of large deformation and the Lagrange method is easy to track the deformation process of the material, overcomes the numerical fluctuation of the particle method caused by the limited number of particles, and realizes the accurate numerical simulation calculation of the explosion and impact problems.
The purpose of the invention is realized by the following technical scheme.
A method of precision interface tracking processing coupling Lagrange particles and Euler methods, comprising the steps of:
step 1: aiming at a simulation model to be analyzed, initializing the created simulation model, wherein the initialization comprises the steps of determining the size of a calculation domain, position information and geometric dimension information of various materials in the calculation domain, grid step length and coordinates, grid medium identification, particle arrangement, material properties and parameters, setting of simulation conditions, initial calculation control parameters and the like;
step 2: and calculating the artificial viscosity value, the stress tensor and the grid speed updating amount of the grid in each set time step. Wherein the artificial viscosity value is determined by the velocity gradient change of the adjacent grids, the density of the material and the artificial viscosity coefficient; circularly obtaining the strain rate, rotation rate and stress of each grid, and determining the stress tensor of the current grid based on a stress rate formula; further, considering the gradient effect of the stress tensor, determining the speed updating amount of the material in the grid;
and step 3: the topological relationship between the mesh and the particles is determined to achieve mapping of the mesh physical quantity to the particles.
Wherein the grid physical quantity is updated after a set time step is carried out after the step 2. Based on the topological relation between the grids and the particle influence domains, the volume share of the particle influence domains in each grid is obtained through solving, all the particle influence domain volumes in the grids are added and summed to obtain the sum of the influence domain volumes of the grids, and the physical quantities of the grids are mapped to the particles according to the volume share ratio, wherein the physical quantities comprise mass, momentum, volume, energy and the like.
And 4, step 4: the location of the particle movement is determined.
And 2, updating the physical quantity of the particles, and further obtaining the velocity of the particles through a volume weighting formula. After the velocity is obtained, the position coordinate of the particle at the next moment can be obtained by multiplying the velocity by the time step length.
And 5: determining a topological relationship between the moved particles and the grid to achieve mapping of the particle physical quantities to the grid.
Based on the topological relation between the moved particle influence domains and the grids, the volume share of the moved particle influence domains in each grid is obtained through solving, the volume ratio of the volume share in the particle influence domains is calculated, and the physical quantities of the particles are mapped to the grids according to the ratio, wherein the physical quantities comprise mass, momentum, volume, energy and the like.
Step 6: and calculating a state equation and a control equation corresponding to the simulation model.
After step 5, each physical quantity in the grid changes, and the state of each material needs to be updated and calculated, that is, the state equation and the control equation are solved. Wherein the calculation of the state equations includes determining the pressure of each material within each grid, with different materials corresponding to different state equations. The calculation of the control equation comprises solving conservation equations of mass, momentum and energy, and updating the mass, momentum and energy of each material medium in the grid.
And 7: and updating the grid and particle physical quantities of the simulation model at the boundary of the computational domain.
After the step 6, whether each material medium in the calculation domain flows to the boundary or not needs to be judged and corresponding processing is carried out, and if the material medium does not flow to the boundary, the material medium does not need to be processed; when the material medium flows to the boundary, it is necessary to perform boundary condition calculation, that is, to update the physical quantities of the boundary mesh and the particles in accordance with the set boundary conditions when the material medium flows to the boundary.
And 8: and outputting a corresponding simulation result based on the set termination condition, wherein the simulation result comprises the merged output of all the simulation data and the output of the restart file.
The eight steps are adopted to realize accurate numerical simulation calculation of explosion and impact problems.
Advantageous effects
According to the method, the particles with a certain influence domain are introduced into the background grid of the Euler method to track the substances in the grid, the hexahedron influence domain is used for carrying out interpolation mapping on the particles and the grid physical quantity, numerical value fluctuation of the particle method due to limited particle quantity is overcome, the accurate interface tracking processing method for coupling the Lagrange particles and the Euler method has more excellent calculation performance, and the fixed grid is added, so that embedding cannot occur between different substances due to the single value of mapping. The accurate interface tracking processing method for coupling the Lagrange particles and the Euler method has the advantages that the Euler method is easy to process the large deformation problem and the Lagrange method is easy to track the deformation process of the material, solves the problem that the Euler method is difficult to clearly track the movement process of the multi-material interface, and effectively realizes accurate numerical simulation calculation of the explosion and impact problems.
Drawings
FIG. 1 is a flowchart showing the steps of a method for accurate interface tracking of a coupled Lagrange particle and Euler method according to the present invention;
FIG. 2 is a schematic diagram of a two-dimensional mapping of grid physical quantities to particles according to the present invention;
FIG. 3 is a schematic diagram of the present invention showing the influence domain of particles falling completely on the current grid;
FIG. 4 is a diagram illustrating the influence domain of a particle divided by two adjacent grids according to the present invention;
FIG. 5 is a diagram illustrating an influence domain of particles divided by four grids according to the present invention;
FIG. 6 is a schematic diagram of an influence domain of a particle divided by eight grids according to the present invention;
FIG. 7 is a schematic diagram of a two-dimensional mapping of particle physical quantities to a grid according to the present invention;
FIG. 8 is a comparison of the results of numerical simulations of the process of the present invention for penetration of a steel sheet with real experiments;
FIG. 9 is a comparison of the numerical results of the residual velocity of a projectile penetrating a steel sheet in accordance with the present invention with real experimental data;
figure 10 is a comparison of shaped charge form figure results according to the present invention with experimental results.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention clearer, the technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all embodiments of the present invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
As shown in fig. 1, the method for processing an accurate interface tracking by coupling Lagrange particles with a Euler method according to the present invention includes the following steps:
(1) creating a simulation model aiming at the problem to be analyzed, and carrying out initialization setting on the created simulation model; determining the size of a calculation domain, position information and geometric dimension information of various materials in the calculation domain, grid step length and coordinates, grid medium identification, arrangement of particles, material properties and parameters, setting of simulation conditions, initial calculation control parameters and the like;
specifically, as a preferred example of the present invention, the step 1 includes:
step 101, creating a simulation model aiming at a problem to be analyzed, and setting the size of an area needing calculation, namely calculation area intervals in three directions; in the calculation domain, constructing a geometric model of each material of a problem to be simulated;
step 102, setting grid step lengths in three directions to realize grid division, obtaining information of the divided grids and storing the information into grid data, wherein the grid information comprises grid serial numbers, grid coordinates and material medium identifications represented by the grids;
and 103, combining the material medium marks represented by the grids, selecting the grids needing to accurately track the deformation process of the material, and distributing Lagrange particles in each direction according to actual requirements. Determining the step length of the influence domain of Lagrange particles based on the principle that Lagrange particle influence areas are closely connected and completely cover all media in a calculation domain, and calculating the coordinate information of each Lagrange particle;
step 104, setting the properties and model parameters of the materials, and determining the data of density, yield strength, internal energy of melt ratio, Young modulus, Poisson ratio, type and parameters of the material model and the like of each material related to the simulation model;
step 105, setting boundary conditions, and determining the boundary conditions of the simulation model, wherein the boundary conditions comprise a solid wall boundary condition, a continuous boundary condition, a symmetric boundary condition and the like;
106, setting initial calculation control parameters; the calculation control parameters comprise information such as total calculation steps, initial time step length, step interval of stored results and the like.
(2) Calculating the artificial viscosity value, the stress tensor and the grid speed updating amount of the grid in each set time step; (ii) a Specifically, as a preferred example of the present invention, the step 2 includes:
step 21, calculating the current grid speed uiAnd next mesh velocity ui+1Definition of u ═ ui+1-uiThen the artificial viscosity can be determined by
Figure BDA0002244120330000051
Calculated, where ρ is the density of the material in the grid, anAnd bnSecond and first order artificial viscosity coefficients, c being a constant associated with the material;
step 22, calculating a stress tensor of the grid, circularly obtaining a strain rate, a rotation rate and a stress of each grid, calculating the stress tensor of the current grid based on a stress rate formula, obtaining a temporary updated stress through the stress of the grid and the stress tensor, judging whether the stress is greater than the corresponding material yield strength, obtaining the stress after yielding by using a radial return method if yielding occurs, and not processing if yielding does not occur;
and step 23, updating the grid speed. The gradient effect of the stress tensor is considered, the speed and the specific internal energy of the material in the grid are obtained, and the momentum and the energy of the material in the grid are further calculated; specifically, the velocity and specific energy content of the material can be calculated from the following equations
Figure BDA0002244120330000061
Figure BDA0002244120330000062
Wherein u is the grid velocity, t is the time parameter, e is the internal energy of the grid ratio, I is the volume stress tensor, S is the bias stress tensor,
Figure BDA0002244120330000063
for the strain rate tensor, P is the hydrostatic pressure.
(3) Determining the topological relation between the grids and the particles in each set time step to realize the mapping of the grid physical quantity to the particles; fig. 2 shows a schematic diagram of the mapping of grid physical quantities to particles in a two-dimensional case. In the three-dimensional numerical calculation, 27 positional relationships are counted in the case where there are 4 topological relationships affected by grids and particles, as shown in fig. 3 to 6. FIG. 3 shows a case where the influence domain of the particles falls completely in the current mesh, and only one topological relationship exists; FIG. 4 shows a case where the influence domain of a particle is divided by two adjacent grids, and 6 topological relations are included; FIG. 5 shows a case where the influence domain of a particle is divided by four grids, and 12 topological relations are included; FIG. 6 shows a case where the influence domain of a particle is divided by eight grids, and 8 topological relations are included. Based on the topological relation between the grids and the particle influence domains, the volume share of the particle influence domains in each grid is obtained through solving, all the particle influence domain volumes in the grids are added and summed to obtain the sum of the influence domain volumes of the grids, and the physical quantities of the grids are mapped to the particles according to the volume share ratio, wherein the physical quantities comprise mass, momentum, volume, energy and the like.
(4) Determining the position of particle movement after a set time step; similar to the mapping of grid physical quantities to particles, the velocity of particles can be obtained by a volume weighting formula. After the velocity is obtained, the position coordinate of the particle at the next moment can be obtained by multiplying the velocity by the time step length.
(5) Determining the topological relation between the moved mass points and the grid in each set time step to realize the mapping of the mass point physical quantity to the grid; FIG. 7 is a schematic diagram showing the mapping of particle physical quantities to a grid in a two-dimensional case. Similarly, in the three-dimensional numerical calculation, there are 27 kinds of positional relationships in total in the case of 4 topological relationships between the moved particle influence domain and the mesh, and the schematic diagrams thereof can be shown in fig. 3 to 6. Based on the topological relation between the moved particle influence domains and the grids, the volume share of the moved particle influence domains in each grid is obtained through solving, the volume ratio of the volume share in the particle influence domains is calculated, and the physical quantities of the particles are mapped to the grids according to the ratio, wherein the physical quantities comprise mass, momentum, volume, energy and the like.
(6) Calculating a state equation and a control equation corresponding to the simulation model in each set time step; specifically, as a preferred example of the present invention, the step 6 includes:
and step 61, calculating a state equation, and solving the pressure of each substance in each grid, wherein different substances correspond to different state equations. Both the explosion and impact problems are high pressure, high strain rate conditions, in which case the solid material will enter the fluid state instantaneously, its ability to resist deformation can be neglected, only the relation between hydrostatic pressure and volumetric strain, specific internal energy needs to be considered, and the solid material can be treated as a non-viscous compressible fluid. Thermodynamic parameters related to the fluid mechanics equation set are density rho, pressure P, temperature T, internal energy e, thermodynamic entropy s and enthalpy h. According to the thermodynamic theory, only two of the above parameters are mutually independent parameters, and the rest parameters can be derived from other two parameters. The equation of state considered is in the form of pressure as a function of density and internal energy:
P=P(ρ,e) (1)
the pressure determined by equation (1) includes an elastoplastic component, and therefore when determining the hydrostatic pressure, the plastic pressure component must be subtracted, here using the following method:
Figure BDA0002244120330000071
wherein, the plane is a pressure correction coefficient, Y0Is the yield strength of the material.
The numerical simulation of concrete failure under blast and impact loads involves media such as explosives, metals, air, and concrete. For the state equations of the media, variable index multi-party gas state equation, JWL state equation, Grunersen state equation, ideal gas state equation, HJC state equation and the like can be respectively adopted, and the pure grid pressure for a single substance can be directly calculated by the state equations. For the calculation of the mixed grid pressure, the volume fraction weighting method is adopted to calculate the pressure of the mixed grid, and the pressure P of each substance is calculated by the formula (1)αThe pressure of the hybrid grid is calculated by:
Figure BDA0002244120330000072
wherein σαIs the volume fraction of each substance;
and step 62, calculating a control equation, solving a mass, momentum and energy conservation equation, and updating the mass, momentum and energy of each material medium in the grid.
(7) Updating the grid physical quantity of the simulation model at the boundary of the calculation domain within each set time step; specifically, as a preferred example of the present invention, the step 7 includes performing boundary condition calculation to update the physical quantities of the boundary mesh and the particles by processing the material medium flowing to the boundary according to the set boundary conditions. The method specifically comprises the following steps: judging the material flow in the boundary grid, and if the material flow in the grid does not reach the boundary in the time step, normally updating the physical quantities of the grid and the particles; if the material flow in the grid reaches the boundary, processing the grid and the particle physical quantity according to the set boundary condition;
(8) and outputting a corresponding simulation result based on the set termination condition.
Specifically, as a preferred example of the present invention, the step 8 includes: if the currently calculated step number meets the output set condition, merging and outputting all the simulation data and recording the serial number mark of the output file; writing variables and variable names contained in grids and particles into a file; after finishing the data output required by post-processing display, writing the increment information, the material and the calculation control information required by restart into the same file and recording the name of the output file.
Specifically, fig. 8 shows the comparison of the results of numerical simulation of the process of piercing a steel sheet with an elastomer with the real experiment, where (a) is the real experiment data and (b) is the numerical simulation result, and the numerical simulation result is well matched with the real experiment data from the comparison at each time. The simulation was performed on the projectiles at different initial speeds to obtain corresponding residual speed data, and fig. 9 shows the comparison of the numerical results of the residual speeds of the projectiles penetrating through the steel sheet with the real experimental data. The accurate interface tracking processing method coupled with the Larange particle and the Euler method can better track the deformation condition of the target plate in the penetration process of the projectile body, and the residual speed is well matched with real experimental data. Figure 10 shows the comparison of shaped charge shaping values with experimental results, from which it can be seen that the use of a precise interface tracking process coupled with the Larange particle and Euler methods according to the present invention effectively simulates the shaped charge shaping process.
Through the embodiment, the accurate interface tracking processing method for coupling Lagrange particles and the Euler method combines the advantages of the Euler method and the Lagrange method, can well process the large deformation and dynamic damage process of materials, and can be better applied to numerical simulation research of various explosion impact problems.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention, and the scope of the present invention is not limited thereto, and any person skilled in the art can substitute or change the technical solution of the present invention and its inventive concept within the technical scope of the present invention.

Claims (4)

1.一种耦合Lagrange质点和Euler方法的精确界面追踪处理方法,其特征在于包括如下步骤:1. a precise interface tracking processing method of coupling Lagrange particle and Euler method, is characterized in that comprising the steps: 步骤1、针对所需要分析的创建仿真模型,并对所创建的仿真模型进行初始化设置,包括确定计算域的大小,各类材料在计算域中位置信息和几何尺寸信息、网格步长及坐标、网格介质标识、质点的布置、材料属性及参数、模拟条件的设定以及初始计算控制参数;Step 1. Create a simulation model for the required analysis, and initialize the created simulation model, including determining the size of the computational domain, the location information and geometric size information of various materials in the computational domain, grid step size and coordinates , grid medium identification, particle arrangement, material properties and parameters, setting of simulation conditions and initial calculation control parameters; 步骤2、在所设定的每一个时间步内,计算网格的人工粘性值、应力张量及网格速度更新量,其中由相邻网格的速度梯度变化量、材料的密度以及人工粘性系数确定人工粘性值;对每个网格进行循环获得每个网格的应变率、旋转率以及应力,基于应力率公式确定当前网格的应力张量;进一步,考虑应力张量的梯度效应,确定网格内材料的速度更新量;Step 2. In each set time step, calculate the artificial viscosity value, stress tensor and grid velocity update amount of the grid, which are determined by the velocity gradient change of adjacent grids, the density of the material and the artificial viscosity. The coefficient determines the artificial viscosity value; circulates each grid to obtain the strain rate, rotation rate and stress of each grid, and determines the stress tensor of the current grid based on the stress rate formula; further, considering the gradient effect of the stress tensor, Determine the velocity update amount of the material in the mesh; 步骤3、确定网格与质点之间的拓扑关系以实现网格物理量映射至质点,其中网格物理量为经步骤2后经历所设定的一个时间步后更新后的网格物理量,基于网格与质点影响域之间的拓扑关系,求解得到质点影响域在各个网格所占的体积份额,将网格内所有的质点影响域体积相加求和,得到网格的影响域体积之和,由体积份额占比将网格的物理量映射至质点,包括质量、动量、体积、能量物理量;Step 3. Determine the topological relationship between the grid and the particle to realize the mapping of the physical quantity of the grid to the particle, wherein the physical quantity of the grid is the physical quantity of the grid that is updated after going through a set time step after step 2. Based on the grid The topological relationship with the particle influence domain, the volume share of the particle influence domain in each grid is obtained by solving, and the volume of all the particle influence domains in the grid is added and summed to obtain the sum of the influence domain volumes of the grid, The physical quantities of the grid are mapped to the particle points by the volume share ratio, including the physical quantities of mass, momentum, volume, and energy; 步骤4、确定质点移动的位置;步骤2实现了质点物理量的更新,进一步通过体积加权公式,可得到质点的速度;得到速度后,乘以时间步长即可获得质点下一时刻的位置坐标;Step 4. Determine the position where the particle moves; Step 2 realizes the update of the physical quantity of the particle, and further through the volume weighting formula, the speed of the particle can be obtained; after obtaining the speed, multiply the time step to obtain the position coordinate of the particle at the next moment; 步骤5、确定移动后质点与网格之间的拓扑关系以实现质点物理量映射至网格,基于移动后质点影响域与网格之间的拓扑关系,求解得到移动后质点影响域在各个网格所占的体积份额,计算该体积份额占质点影响域体积占比,由该占比将质点物理量映射至网格,包括质量、动量、体积、能量物理量;Step 5. Determine the topological relationship between the moving particle and the grid to realize the mapping of the physical quantity of the particle to the grid. Based on the topological relationship between the particle's influence domain and the grid after the moving, the solution is obtained to obtain the moving particle's influence domain in each grid. The volume share occupied, calculate the volume share of the particle influence domain volume, and map the particle physical quantities to the grid from this ratio, including mass, momentum, volume, and energy physical quantities; 步骤6、计算仿真模型所对应的状态方程以及控制方程;经历步骤5之后,网格内各物理量均发生了变化,需要对各材料的状态进行更新计算,即状态方程和控制方程的求解;其中状态方程的计算包括确定各个网格内各物质的压力,不同物质对应不同的状态方程;控制方程的计算包括求解质量、动量以及能量守恒方程,更新网格内各材料介质的质量、动量以及能量;Step 6: Calculate the state equation and control equation corresponding to the simulation model; after step 5, each physical quantity in the grid has changed, and the state of each material needs to be updated and calculated, that is, the solution of the state equation and the control equation; wherein The calculation of the state equation includes determining the pressure of each substance in each grid, and different substances correspond to different state equations; the calculation of the control equation includes solving the mass, momentum and energy conservation equations, and updating the mass, momentum and energy of each material medium in the grid. ; 步骤7、更新所述仿真模型在计算域边界处的网格和质点物理量;经历步骤6之后,需对计算域内的各材料介质是否流动至边界进行判定并进行相应的处理,若未流动至边界,则无需处理;若流动至边界,则需要进行边界条件计算即根据所设定的边界条件,处理材料介质流动至边界的情况,更新边界网格和质点的物理量;Step 7. Update the grid and particle physical quantities of the simulation model at the boundary of the computational domain; after step 6, it is necessary to determine whether each material medium in the computational domain flows to the boundary and perform corresponding processing. If it does not flow to the boundary , then no processing is required; if it flows to the boundary, it is necessary to calculate the boundary conditions, that is, according to the set boundary conditions, deal with the situation of the material medium flowing to the boundary, and update the physical quantities of the boundary mesh and the particle; 步骤8、基于所设定的终止条件,输出对应的仿真结果,包括所有的仿真数据合并输出以及重启动文件的输出。Step 8. Based on the set termination condition, output the corresponding simulation result, including the combined output of all simulation data and the output of the restart file. 2.根据权利要求1所述的一种耦合Lagrange质点和Euler方法的精确界面追踪处理方法,其特征在于,所述步骤1包括如下步骤:2. the precise interface tracking processing method of a kind of coupling Lagrange particle and Euler method according to claim 1, is characterized in that, described step 1 comprises the steps: 步骤101、针对所需要分析的问题创建仿真模型,设定需要开展计算的区域大小,即三个方向的计算区域区间;在计算域内,构建所需要仿真问题的各材料的几何模型;Step 101: Create a simulation model for the problem to be analyzed, and set the size of the area that needs to be calculated, that is, the calculation area interval in three directions; in the calculation domain, construct the geometric model of each material of the required simulation problem; 步骤102、设定三个方向的网格步长以实现网格划分,获得划分网格的信息并存入网格数据中,所述网格信息包括网格序号、网格坐标、网格所代表的材料介质标识;Step 102: Set the grid step size in three directions to realize grid division, obtain grid information and store it in grid data. The grid information includes grid serial number, grid coordinates, and grid data. Material medium identification; 步骤103、结合网格所代表的材料介质标号,选取需要精确追踪材料变形过程的网格,依据实际需求在每个方向上布撒Lagrange质点,基于Lagrange质点影响区域紧密相连并完全覆盖计算域内所有介质这一原则,确定Lagrange质点的影响域步长,并计算出每个Lagrange质点的坐标信息;Step 103: Select the grid that needs to accurately track the deformation process of the material according to the material medium label represented by the grid, and distribute Lagrange particles in each direction according to the actual requirements. According to the principle of medium, the step size of the influence domain of the Lagrange particle is determined, and the coordinate information of each Lagrange particle is calculated; 步骤104、设定材料的属性和模型参数,确定仿真模型所涉及的每种材料的密度、屈服强度、融化比内能、杨氏模量、泊松比以及材料模型的类型和参数数据;Step 104: Set the properties of the material and model parameters, and determine the density, yield strength, melting ratio internal energy, Young's modulus, Poisson's ratio, and the type and parameter data of each material involved in the simulation model; 步骤105、设定边界条件,确定仿真模型的边界条件,边界条件包括固壁边界条件、连续边界条件和对称边界条件;Step 105, set boundary conditions, determine the boundary conditions of the simulation model, and the boundary conditions include solid wall boundary conditions, continuous boundary conditions and symmetrical boundary conditions; 步骤106、设定初始计算控制参数;所述的计算控制参数包括总体计算步数、初始时间步长、保存结果的步数间隔信息。Step 106 , setting initial calculation control parameters; the calculation control parameters include overall calculation steps, initial time step, and step interval information for saving results. 3.根据权利要求1所述的一种耦合Lagrange质点和Euler方法的精确界面追踪处理方法,其特征在于,所述步骤2包括如下步骤:3. the precise interface tracking processing method of a kind of coupling Lagrange particle and Euler method according to claim 1, is characterized in that, described step 2 comprises the steps: 步骤21、计算当前网格速度ui以及下一个网格速度ui+1,定义速度梯度Δu=ui+1-ui,则人工粘性可由q=ρ(|Δu|-Δu)[an(|Δu|-Δu)+bnc]计算得到,其中ρ为网格内材料的密度,an和bn为二阶和一阶人工粘性系数,c为与材料相关的常数;Step 21: Calculate the current grid velocity ui and the next grid velocity u i+1 , define the velocity gradient Δu=u i+1 -u i , then the artificial viscosity can be calculated by q=ρ(|Δu|-Δu)[a n (|Δu|-Δu)+b n c], where ρ is the density of the material in the grid, an and b n are the second - order and first-order artificial viscosity coefficients, and c is a material-related constant; 步骤22、计算所述网格的应力张量,对每个网格进行循环获得每个网格的应变率、旋转率以及应力,基于应力率公式计算得到当前网格的应力张量,并通过该网格的应力加上应力张量得到临时的更新后的应力,判定是否大于所对应的材料屈服强度,若发生屈服则用径向返回方法获得屈服后的应力,若未发生屈服则不做处理;Step 22: Calculate the stress tensor of the grid, cycle each grid to obtain the strain rate, rotation rate and stress of each grid, calculate the stress tensor of the current grid based on the stress rate formula, and pass The stress of the grid is added to the stress tensor to obtain the temporary updated stress, and it is judged whether it is greater than the corresponding material yield strength. If yield occurs, the radial return method is used to obtain the yield stress. deal with; 步骤23、更新网格的速度,考虑应力张量的梯度效应,获得网格内材料的速度和比内能,进一步计算得到网格内材料的动量和能量;由下列公式计算材料的速度和比内能Step 23. Update the velocity of the grid, consider the gradient effect of the stress tensor, obtain the velocity and specific internal energy of the material in the grid, and further calculate the momentum and energy of the material in the grid; calculate the velocity and specific internal energy of the material by the following formulas
Figure FDA0002779147380000031
Figure FDA0002779147380000031
Figure FDA0002779147380000032
Figure FDA0002779147380000032
其中,u为网格速度,t为时间参量,e为网格比内能,I为体积应力张量,S为偏应力张量,
Figure FDA0002779147380000034
为应变率张量,P为静水压力。
where u is the grid velocity, t is the time parameter, e is the specific internal energy of the grid, I is the volume stress tensor, S is the deviatoric stress tensor,
Figure FDA0002779147380000034
is the strain rate tensor, and P is the hydrostatic pressure.
4.根据权利要求1所述的一种耦合Lagrange质点和Euler方法的精确界面追踪处理方法,其特征在于,所述步骤6包括如下步骤:4. the precise interface tracking processing method of a kind of coupling Lagrange particle and Euler method according to claim 1, is characterized in that, described step 6 comprises the steps: 步骤61、计算状态方程,求解各个网格内各物质的压力,不同物质对应不同的状态方程,爆炸与冲击问题均为高压、高应变率的情况,在该情况下,固体材料将会瞬间进入流体状态,可忽略其抵抗变形的能力,只需要考虑静水压力与体积应变、比内能的关系,固体材料可作为无粘性可压缩的流体处理,流体力学方程组涉及的热力学参量为密度ρ,压力P,温度T,内能e,热力学熵s和焓h;根据热力学理论,上述参量仅有两个参量为相互独立参量,其余参量均可由其他两个参量导出,考虑的状态方程形式为压力是密度和内能的函数:Step 61: Calculate the state equation, and solve the pressure of each substance in each grid. Different substances correspond to different state equations. The explosion and shock problems are both high pressure and high strain rate situations. In this case, the solid material will enter into the grid instantaneously. The fluid state, its ability to resist deformation can be ignored, only the relationship between hydrostatic pressure, volumetric strain and specific internal energy needs to be considered. Solid materials can be treated as inviscid and compressible fluids. The thermodynamic parameters involved in the fluid mechanics equations are density ρ, pressure P, temperature T, internal energy e, thermodynamic entropy s and enthalpy h; according to thermodynamic theory, only two of the above parameters are independent of each other, and the rest of the parameters can be derived from the other two parameters. The considered state equation is in the form of pressure A function of density and internal energy: P=P(ρ,e) (1)P=P(ρ,e) (1) 由式(1)确定的压力包括弹塑性分量,因此在确定静水压力时,必须扣除塑性压力分量,这里采用如下方法处理:The pressure determined by the formula (1) includes the elastic-plastic component, so when determining the hydrostatic pressure, the plastic pressure component must be deducted, and the following method is used here:
Figure FDA0002779147380000033
Figure FDA0002779147380000033
式中,plap为压力修正系数,Y0为材料的屈服强度;In the formula, plap is the pressure correction coefficient, Y 0 is the yield strength of the material; 在爆炸与冲击载荷下混凝土破坏的数值模拟中涉及到炸药、金属、空气以及混凝土介质,对于这些介质的状态方程,分别采用可变指数多方气体状态方程、WL状态方程、Grunerisen状态方程、理想气体状态方程、HJC状态方程,对于单一物质的纯网格压力可由状态方程直接计算得到,对于混合网格压力的计算,采用体积分数加权的方法来计算混合网格的压力,由(1)式计算出各物质的压力Pα,混合网格的压力由下式计算:Explosive, metal, air and concrete media are involved in the numerical simulation of concrete failure under explosion and impact loads. For the state equations of these media, the variable-exponential polytropic gas state equation, WL state equation, Grunerisen state equation, and ideal gas are used respectively. State equation, HJC state equation, the pure grid pressure for a single substance can be directly calculated by the state equation, and for the calculation of the mixed grid pressure, the volume fraction weighting method is used to calculate the pressure of the mixed grid, which is calculated by the formula (1) The pressure P α of each substance is obtained, and the pressure of the mixed mesh is calculated by the following formula:
Figure FDA0002779147380000041
Figure FDA0002779147380000041
其中,σα为各物质的体积分数;Among them, σ α is the volume fraction of each substance; 步骤62、控制方程的计算,求解质量、动量以及能量守恒方程,更新网格内各材料介质的质量、动量以及能量。Step 62 , calculating the control equation, solving the mass, momentum and energy conservation equations, and updating the mass, momentum and energy of each material medium in the grid.
CN201911010698.4A 2019-11-19 2019-11-19 An Accurate Interface Tracking Processing Method Coupling Lagrange Particles and Euler's Method Active CN110750933B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201911010698.4A CN110750933B (en) 2019-11-19 2019-11-19 An Accurate Interface Tracking Processing Method Coupling Lagrange Particles and Euler's Method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201911010698.4A CN110750933B (en) 2019-11-19 2019-11-19 An Accurate Interface Tracking Processing Method Coupling Lagrange Particles and Euler's Method

Publications (2)

Publication Number Publication Date
CN110750933A CN110750933A (en) 2020-02-04
CN110750933B true CN110750933B (en) 2021-01-01

Family

ID=69279516

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201911010698.4A Active CN110750933B (en) 2019-11-19 2019-11-19 An Accurate Interface Tracking Processing Method Coupling Lagrange Particles and Euler's Method

Country Status (1)

Country Link
CN (1) CN110750933B (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111581748B (en) * 2020-05-12 2023-04-18 中国工程物理研究院总体工程研究所 Method for acquiring initial explosion speed of porous material shell
CN113032974B (en) * 2021-03-05 2024-08-09 清华大学 Hexahedral cell finite particle method
CN113591345B (en) * 2021-07-08 2024-01-23 北京理工大学 Explosion reaction flow high-precision prediction method based on generalized Riemann solver
WO2023015528A1 (en) * 2021-08-12 2023-02-16 中国科学院深圳先进技术研究院 Software robot simulation method and apparatus, electronic device, and storage medium
CN113673185B (en) * 2021-08-25 2024-01-30 北京理工大学 Accurate shock wave discontinuities capturing method based on weighted bidirectional mapping
CN114611340B (en) * 2022-03-17 2024-11-22 北京理工大学 A coupled Eulerian-Lagrangian method for accurately capturing the shock wave propagation process
CN114626269B (en) * 2022-03-21 2023-03-24 中国科学院力学研究所 A method and device for analyzing laser ablation effects of multi-material structures
CN114861481B (en) * 2022-03-30 2024-06-21 西北核技术研究所 Calculation method for steady-state effect of movement of explosion source in any configuration
WO2024103241A1 (en) * 2022-11-15 2024-05-23 中国科学院深圳先进技术研究院 Soft robot simulation method based on material point method
CN118862459A (en) * 2024-07-04 2024-10-29 安徽方圆机电股份有限公司 Forming simulation method and system for explosively formed projectiles

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109948275A (en) * 2019-03-28 2019-06-28 湘潭大学 An optimization calculation method of crawler barbed structure based on CFD-DEM coupling simulation

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8060349B2 (en) * 2007-03-16 2011-11-15 Chang Gung University Method of designing a static synchronous compensator based on passivity-based control
CN104268943B (en) * 2014-09-28 2017-05-03 北京航空航天大学 Fluid simulation method based on Eulerian-Lagrangian coupling method
CN107133397B (en) * 2017-04-27 2018-10-19 山东大学 A method of two-way wind-structure interaction is carried out to biovalve based on ALE methods

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109948275A (en) * 2019-03-28 2019-06-28 湘潭大学 An optimization calculation method of crawler barbed structure based on CFD-DEM coupling simulation

Also Published As

Publication number Publication date
CN110750933A (en) 2020-02-04

Similar Documents

Publication Publication Date Title
CN110750933B (en) An Accurate Interface Tracking Processing Method Coupling Lagrange Particles and Euler's Method
Matsson An introduction to ansys fluent 2023
Ferziger et al. Computational methods for fluid dynamics
CN114611340B (en) A coupled Eulerian-Lagrangian method for accurately capturing the shock wave propagation process
Wu et al. A development of the discontinuous deformation analysis for rock fall analysis
CN108763683B (en) New WENO format construction method under trigonometric function framework
CN104991999A (en) Dam bursting flood routing simulation method based on two-dimensional SPH
Smolarkiewicz et al. Towards mesh adaptivity for geophysical turbulence: continuous mapping approach
Dong et al. Smoothed particle hydrodynamics (SPH) simulation of impinging jet flows containing abrasive rigid bodies
CN108701275A (en) Particle simulation device, particle simulation method and particle simulation program
Gan et al. New deformation back analysis method for the creep model parameters using finite element nonlinear method
Hu et al. A multi-mesh adaptive finite element approximation to phase field models
Shi et al. Numerical prediction on erosion damage caused by wind-blown sand movement
CN113673185B (en) Accurate shock wave discontinuities capturing method based on weighted bidirectional mapping
Nguyen Material point method: basics and applications
Duan et al. Modeling the gravitational field of the ore-bearing asteroid by using the CFD-based method
Chung A level set approach for computing solutions to inviscid compressible flow with moving solid boundary using fixed Cartesian grids
Zou et al. Modelling blast movement and muckpile formation with the position-based dynamics method
Zhang et al. Rotation errors in numerical manifold method and a correction based on large deformation theory
CN112668256B (en) Vertical seam type fishway vortex recognition method
Felici et al. Analysis of vortex induced vibration of a thermowell by high fidelity FSI numerical analysis based on RBF structural modes embedding
CN102493800A (en) Euler obtaining method for perforating charge performance parameter
Prokhorov et al. Sintering simulation using GPU-based algorithm for the samples with a large number of grains
CN109271696A (en) Blood clotting analogy method and system based on MPM
Ma et al. A robust and efficient model for the interaction of fluids with deformable solids

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant