CN110970095A - Method for calculating stress of forced convection on AlN dendrites in molten steel solidification process in metallurgical field - Google Patents

Method for calculating stress of forced convection on AlN dendrites in molten steel solidification process in metallurgical field Download PDF

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CN110970095A
CN110970095A CN201911036081.XA CN201911036081A CN110970095A CN 110970095 A CN110970095 A CN 110970095A CN 201911036081 A CN201911036081 A CN 201911036081A CN 110970095 A CN110970095 A CN 110970095A
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孟祥宁
崔磊
高晓晗
朱苗勇
张坤
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Northeastern University China
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Abstract

The invention provides a method for calculating the stress of AlN dendrite by forced convection in the process of molten steel solidification in the field of metallurgy, and relates to the field of metallurgy. The method comprises the steps of firstly collecting steel components and solidification conditions, then calculating heat transfer and mass transfer in the solidification process, growth of interface cells in the solidification process and AlN nucleation and growth in the solidification process, and further establishing an AlN precipitation model in the solidification of the Fe-C-Al-N quaternary alloy. And predicting the precipitation rule of the AlN precipitation model according to the continuous casting process conditions such as casting temperature, solute composition, cooling rate and the like, and displaying the precipitation position, size, shape and size of the AlN in an imaging manner by utilizing data analysis and visual processing software data, and quantifying the precipitation amount of the AlN. The method for predicting the AlN inclusion precipitation condition in the molten steel solidification process provides theoretical guidance for optimizing the solidification technology, controlling the size of the AlN inclusion in the steel and improving the quality of casting blanks.

Description

Method for calculating stress of forced convection on AlN dendrites in molten steel solidification process in metallurgical field
Technical Field
The invention belongs to the technical field of ferrous metallurgy, and particularly relates to a method for calculating the stress of AlN dendrites by forced convection in a molten steel solidification process in the field of metallurgy.
Background
The steel industry is an important pillar type basic industry of national economy. In the process of molten steel solidification, the surface layer of a casting blank begins to nucleate and grow to form columnar crystals along with the reduction of temperature, and the solute concentration at the front edge of a solid-liquid interface is serious along with the growth of the columnar crystals. AlN inclusions with different sizes play different roles in the performance of steel. Therefore, the prediction of the precipitation of the inclusions in the molten steel solidification process has important significance for controlling the cracks of the casting blank and improving the quality of the casting blank. In the continuous casting process, molten steel in the casting blank can continuously flow, and certain influence is generated on the growth and the appearance of the microscopic dendritic crystal. At the same time, the flow of molten steel is also made more complex by the presence of dendrites. The traditional flow field numerical simulation is mainly to solve the pressure field iteratively through a Navier-Stokes (N-S) equation. However, the method is complex to solve, large in calculation amount and poor in numerical stability, and a wall function is needed to be used when the dendritic crystal curved edge boundary is processed, so that the solving error is increased. Therefore, accurately describing the flow field distribution is extremely important for dendrite solution. A method for solving a flow field around dendrites by using a lattice Boltzmann method which has been developed in recent years is introduced. The lattice Boltzmann method is derived from the Boltzmann equation. The Boltzmann equation is mainly used for describing the change rule of the system in the nonequilibrium state.
Disclosure of Invention
The invention aims to solve the problem of the prior solidification technology and provides a method for calculating the stress of AlN dendrites by forced convection in the molten steel solidification process. The stress condition of forced convection on the AlN dendrites under the condition of different processes is predicted, and the solidification technology and the theoretical guidance of forced growth of the dendrites under the forced convection are optimized.
In order to solve the technical problems, the technical scheme adopted by the invention is as follows: a method for calculating the stress of AlN dendrite by forced convection in the process of molten steel solidification comprises the following steps:
step 1, collecting steel grade components, thermodynamic and kinetic parameters in a solidification process and flow field boundary conditions;
step 2, based on a metal solidification theory, calculating the interface growth direction, the distribution of a liquid phase solute field and a temperature field and the distribution of a solid phase region solute field by using a cellular automaton model; meanwhile, a classical model D2Q9 model in a lattice Boltzmann method is coupled to calculate the velocity distribution of the flow field;
step 2.1, in order to enable the cellular automaton model to have certain physical significance, introducing a metal solidification theory, and calculating the growth direction and curvature supercooling of an interface by adopting a sharp interface model;
step 2.2, determining a fluid flow boundary, and calculating the velocity distribution of the flow field by adopting a D2Q9 model;
step 2.3, calculating a liquid phase temperature field by adopting a cellular automaton model in combination with the velocity distribution of the flow field;
step 2.4, combining the flow field velocity distribution, and calculating solute distribution of the liquid phase region and the solid phase region by adopting a cellular automaton model;
and 3, for the complex boundary flow, correcting an F-H format by adopting Mei, adding a free boundary condition on the right side along the speed of the complex boundary flow along the x direction, and establishing a stress growth model of the lower dendrite of the Fe-C-Al-N quaternary alloy flow field by combining a lattice Boltzmann method. And displaying the shape, the size and the stress condition of the AlN dendrite by using data and analysis and visual processing software images.
A method for calculating the stress of AlN dendrites by forced convection in the process of molten steel solidification in the field of metallurgy is characterized by comprising the following steps: the specific method of the step 2.1 comprises the following steps:
firstly, supposing that the solid-liquid interface is in a thermodynamic equilibrium state, according to the law of conservation of solute at the interface, the growth direction of the interface
Figure RE-GDA0002361837180000031
Calculated by the following formula:
Figure RE-GDA0002361837180000032
wherein
Figure RE-GDA0002361837180000033
Indicating the direction of interfacial growth, curvature overcoolingK is calculated by the following formula:
Figure RE-GDA0002361837180000034
wherein ,
Figure RE-GDA0002361837180000035
and
Figure RE-GDA0002361837180000036
respectively representing first-order partial derivatives of the solid phase ratio on an x axis and a y axis;
Figure RE-GDA0002361837180000037
firstly, solving the second-order partial derivative of the y axis after solving the partial derivative of the solid phase ratio on the x axis;
Figure RE-GDA0002361837180000038
and
Figure RE-GDA0002361837180000039
respectively is a second order partial derivative of the solid fraction on an x axis and a y axis;
the state of the cells is detected and the fluid flow boundary and its boundary conditions are determined as described in step 2.2. In the two-dimensional numerical simulation calculation, a D2Q9 model is generally used to calculate the flow field distribution, while ignoring the external force, the velocity distribution of the flow field is calculated by the following formula:
Figure RE-GDA00023618371800000310
Figure RE-GDA00023618371800000311
wherein τ is the dimensionless single-step relaxation time, fi(x+ciΔt,t+Δt)、fi(x, t) is a liquid phase fluid particle distribution function,
Figure RE-GDA0002361837180000041
is in equilibrium with liquid phase fluid particlesA distribution function; wherein c isiThe migration velocity of liquid phase fluid particles in the direction of the grid i, and delta t is a time step; due to the adoption of the D2Q9 model, wherein ciThe sum of the calculation formula is the weight coefficient wiCalculated by the following formula:
Figure RE-GDA0002361837180000042
Figure RE-GDA0002361837180000043
Figure RE-GDA0002361837180000044
wherein c and csThe lattice velocity and the lattice sound velocity are respectively; the macroscopic density ρ, the macroscopic velocity u, and the hydrodynamic viscosity v are calculated by the following equations:
Figure RE-GDA0002361837180000045
Figure RE-GDA0002361837180000046
Figure RE-GDA0002361837180000047
wherein fiIs an entrance node distribution function, i (values of 0,1,2,3,4,5,6,7 and 8) is an angular step node ordinal number, and entrance density rhoinOutlet density ρoutThe velocity u of the fluid particles in the x-axis directionxAnd the velocity u of the fluid particles in the y-axis directionyThe calculation formula is calculated by the following formula:
Figure RE-GDA0002361837180000048
Figure RE-GDA0002361837180000049
Figure RE-GDA00023618371800000410
Figure RE-GDA0002361837180000051
Figure RE-GDA0002361837180000052
Figure RE-GDA0002361837180000053
Figure RE-GDA0002361837180000054
Figure RE-GDA0002361837180000055
f1=f3,f2=f4,f8=f6(19)
Figure RE-GDA0002361837180000056
a method for calculating the stress of AlN dendrites by forced convection in the process of molten steel solidification relates to the field of metallurgy, and step 2.3, a cellular automaton model is adopted to calculate a liquid phase temperature field in combination with flow field velocity distribution; the specific method is calculated by the following method:
firstly, the calculation of the liquid phase temperature field is the calculation in the heat transfer process, so the liquid phase region temperature field is calculated by adopting the following formula:
Figure RE-GDA0002361837180000057
wherein T is time, ρ is matrix density, λ is thermal conductivity, T is cell temperature, cpThe specific heat capacity of the matrix, fs the cellular solid phase rate and L the latent heat; q. q.sw,w、qw,e、qw,n、qw,sThe heat flux densities of the left boundary, the right boundary, the upper boundary and the lower boundary in four directions respectively; for the sake of simplifying the calculation, it is assumed that the thermal conductivity λ of the matrix in the x-axis and y-axis directions is equal;
the supercooling degree at the solid-liquid interface consists of component supercooling, curvature supercooling, thermal supercooling and dynamic supercooling degree, and the dynamic supercooling degree is neglected because the dynamic supercooling degree is smaller relative to other supercooling degrees in the solidification process; therefore, the supercooling degree is calculated by the following equation:
ΔT=ΔTc+ΔTr+(Tbulk-TL) (22)
wherein ,ΔTrIs undercooling of curvature, TbulkTemperature of liquid phase, T, at solidification frontLIs the liquidus temperature, Δ TcIs the supercooling of the components; the liquidus temperature, curvature supercooling and composition supercooling are respectively solved by the following formulas:
TL=1535-65[%C]-2.7[%Al]-90[%N](23)
Figure RE-GDA0002361837180000061
Figure RE-GDA0002361837180000062
wherein gamma is a Gibbs-Thomson coefficient; m isL,iIs the liquidus slope of element i; c. CL,iRepresents the liquid phase concentration of element i;
Figure RE-GDA0002361837180000063
the concentration of the solid-liquid interface front edge of the element i;
because the heat transfer density and the mass transfer density are inseparable in the forced convection AlN dendrite stress calculation method, the solute distribution of the liquid phase region and the solid phase region is calculated by adopting a cellular automaton model according to the flow field velocity distribution in the step 2.4; the interaction between solutes on the growth of dendrites is considered in the liquid phase, and the solute transport in the solid phase is smaller than that in the liquid phase by several orders of magnitude, so the solute interaction in the solid phase is ignored, and the solute transport in the solid phase and the solute transport in the liquid phase are respectively calculated by adopting the following formulas:
Figure RE-GDA0002361837180000064
Figure RE-GDA0002361837180000065
wherein ,CL,i、CS,iRespectively representing the concentration of the element i in the liquid phase and the solid phase; cS,iIs the transmission coefficient of the element i in the solid phase matrix; n-1, wherein n is the total number of elements in the molten steel, and the nth element represents a solvent;
Figure RE-GDA0002361837180000066
representing the Darken coefficient matrix in the liquid phase, assuming the directions of the x-axis and the y-axis in the matrix for simplifying the calculation
Figure RE-GDA0002361837180000067
The values are the same, and the following formula is utilized to solve:
Figure RE-GDA0002361837180000071
Figure RE-GDA0002361837180000072
Figure RE-GDA0002361837180000073
wherein R represents a gas constant, akIndicates the activity of the element k, xkDenotes the molar fraction of the element k, xjRepresents the molar fraction of the element j, δkiDenotes the Kronector delta function, when k is i, δkiTake 1, otherwise deltakiTaking 0; mkRepresenting the mobility of the element k in the system, which is solved according to the Einstein formula, e.g.The following equation is shown:
Figure RE-GDA0002361837180000074
wherein ,
Figure RE-GDA0002361837180000075
representing the diffusion coefficient of the tracking element k. Assuming that a solid-liquid interface is in a thermodynamic equilibrium state, the solute distribution law is satisfied at the interface:
Figure RE-GDA0002361837180000076
according to the law of conservation of solute at the interface, the growth speed of interface cells in a thermodynamic equilibrium state is solved according to the following formula:
Figure RE-GDA0002361837180000077
wherein, the right side
Figure RE-GDA0002361837180000078
The solute transport item only considers the influence of the liquid phase solute interaction on the growth of dendrites;
Figure RE-GDA0002361837180000079
representing the growth speed of the interface cell solidification front; by solving the growth speed of the solidification front of the interface cells, the growth of the interface cells in unit time step is calculated by increasing the solid phase rate, and the following formula is shown:
Figure RE-GDA00023618371800000710
Figure RE-GDA00023618371800000711
Figure RE-GDA0002361837180000081
wherein ,
Figure RE-GDA0002361837180000082
and
Figure RE-GDA0002361837180000083
the cell solid phase ratio Δ f of AlN at the previous time and this time, respectivelys,AlNIncrease in solid fraction of (2); Δ t is a unit time step;
Figure RE-GDA0002361837180000084
indicating edge
Figure RE-GDA0002361837180000085
Unit length of direction through the center of the cell; Δ l ═ 1 μm for the grid cell length; theta represents the angle between the dendrite growth direction and the x-axis direction.
A method for calculating the stress of AlN dendrites by forced convection in the process of molten steel solidification in the field of metallurgy is characterized by comprising the following steps:
the specific method of the step 2.4 comprises the following steps: the following assumptions are calculated and simulated for the calculation of the stress of the forced convection on the AlN dendrites: AlN precipitated in the steel does not contain other phases; only AlN precipitation in the liquid phase is considered; neglecting the increase of interface energy in the growth process; neglecting the heat change when AlN is precipitated; based on the above assumptions, the thermodynamic and kinetic conditions for AlN nucleation in steel are first calculated; when the nucleation condition is met, nucleation is carried out in the cell and the surrounding solute field is updated and calculated, as the AlN interface keeps a thermodynamic equilibrium state, the solute is continuously diffused to the interface, forced convection is carried out on the stress calculation simulation of the AlN dendrite according to the thermodynamic equilibrium state, and the solid-liquid interface normal phase and the growth direction function
Figure RE-GDA0002361837180000086
Calculated by the following formula:
Figure RE-GDA0002361837180000087
whereinθ and
Figure RE-GDA0002361837180000088
the included angles between the interface growth normal direction and the preferred growth direction and the positive direction of the x axis are respectively. ε represents the anisotropy parameter, where the angle between the preferential growth direction and the positive x-axis direction
Figure RE-GDA0002361837180000089
Calculated by the following formula:
Figure RE-GDA00023618371800000810
the reaction formula for generating AlN in the solid-liquid two-phase region and the calculation formula for activity and activity coefficient are as follows:
[Al]+[N]=(AlN) (39)
a[M]=[%M]f[M](40)
Figure RE-GDA0002361837180000091
wherein ,a[M]Representing the Henry activity of element M; m represents an element Al or N, [ M ]]Indicates that the element M is dissolved in the steel; [% M]Represents the concentration of the element M based on a mass 1% standard; f. of[Al] and f[N]Activity coefficients of elements Al and N, respectively, based on a mass 1% standard;
Figure RE-GDA0002361837180000094
representing the interaction coefficient of element j to element i; when a certain cell in the calculation region meets the AlN precipitation condition, marking the cell, carrying out 3 x 3 grid refinement division on the cell, and simultaneously calculating the growth of the cell according to dynamic chemical equilibrium, wherein the formula is as follows:
Figure RE-GDA0002361837180000092
MAlNrepresents the relative molecular mass of AlN; Δ x represents the reaction amount;
a method for calculating the stress of AlN dendrites by forced convection in the process of molten steel solidification in the field of metallurgy is characterized in that Mei is adopted to correct the F-H format, the speed in the x direction is added, the free boundary condition is added on the right side, and a stress growth model of the lower dendrite of a Fe-C-Al-N quaternary alloy flow field is established by combining a lattice Boltzmann method.
Therefore, according to the Mei, the F-H format is modified by first aligning the solid phase boundary points xbAssume that it has a virtual state equilibrium distribution function as follows:
Figure RE-GDA0002361837180000093
wherein ufIs xfFluid velocity of (u)bfFor undetermined virtual velocity, to solve for ubfConstructing an interpolation factor α and xwPosition dependent, ubfThe following formula is used to obtain:
Figure RE-GDA0002361837180000101
Figure RE-GDA0002361837180000102
Figure RE-GDA0002361837180000103
wherein β is for calculating xfInterpolation factor, u, of the rebound distribution structurewIs xwThe moving speed of the interface; according to the formula, a virtual state balance distribution function can be solved; therefore, the solute field distribution and the solid phase region solute distribution under the Mei correction F-H format are obtained by the following formulas:
Figure RE-GDA0002361837180000104
Figure RE-GDA0002361837180000105
when the cell growth is calculated according to the dynamic chemical balance, in order to reduce the calculation error caused by the larger time step, the cells are subjected to spatial 3 x 3 refinement time division and time division, and are subjected to refinement time division at the same time, and the growth in a time step is subjected to multiple circulating calculation when the forced convection is calculated and calculated to stress the AlN dendrite for growth, so that the calculation error caused by the time step is reduced; when the volume of AlN in the matrix cell is increased and the matrix cell is contacted with the adjacent liquid-phase cell, the adjacent liquid-phase cell is subdivided into 3 multiplied by 3F-H format lower boundary AlN precipitation cells, and AlN growth is continued. And displaying the shape, the size and the stress condition of the AlN dendrite by using data and analysis and visual processing software images.
Adopt above-mentioned technical scheme to adopt the produced beneficial effect of above-mentioned technical scheme to lie in: the invention provides a method for calculating the stress of AlN dendrite by forced convection in the process of molten steel solidification. Dendritic crystal growth is carried out under the condition of calculating the forced convection, and the calculation precision is improved by refining the time step. Showing the shape, size and stress of the AlN dendrite. The invention optimizes the solidification technology, predicts the stress analysis of the dendrite under the forced convection and provides theoretical guidance for improving the quality of the casting blank.
Drawings
FIG. 1 is a flow chart of a method for calculating the stress on AlN dendrites by forced convection in a molten steel solidification process according to an embodiment of the present invention;
FIG. 2 is a flow chart of the procedure for computing the stress on the AlN dendrite by forced convection according to the embodiment of the present invention;
fig. 3 is a schematic diagram of a general D2Q9 model of a lattice Boltzmann method according to an embodiment of the present invention;
FIG. 4 is a schematic diagram of a Mei modified F-H format according to an embodiment of the present invention;
FIG. 5 is a simulated graph of dendrite morphology evolution and Al solute distribution in a flow field according to an embodiment of the present invention;
Detailed Description
The following detailed description of embodiments of the present invention is provided in connection with the accompanying drawings and examples. The following examples are intended to illustrate the invention but are not intended to limit the scope of the invention.
In the embodiment, ordinary low-carbon steel is taken as an example, and the method for calculating the stress of the forced convection to the AlN dendrite crystal in the molten steel solidification process is adopted to calculate the stress of the forced convection to the AlN dendrite crystal in the molten steel solidification process.
A method for calculating the stress of AlN dendrites by forced convection in the process of molten steel solidification is shown in figure 1 and comprises the following steps:
step 1, collecting steel grade components, solidification conditions and boundary conditions; in this example, 38CrMoAl steel was used. The components are shown in table 1, and the solidification conditions include cooling rate, supercooling degree and casting temperature;
TABLE 1 Steel species main Components
Figure RE-GDA0002361837180000121
Step 2, based on a metal solidification theory, calculating the interface growth direction, the distribution of a liquid phase solute field and a temperature field and the distribution of a solid phase region solute field by using a cellular automaton model; meanwhile, a classical model D2Q9 model in a lattice Boltzmann method is coupled to calculate the velocity distribution of the flow field; the specific method comprises the following steps:
step 2.1, in order to enable the cellular automaton model to have certain physical significance, introducing a metal solidification theory, and calculating the growth direction and curvature supercooling of an interface by adopting a sharp interface model;
firstly, assuming that a solid-liquid interface is in a thermodynamic equilibrium state, and according to the solute conservation law at the interface, the growth direction of the interface is calculated by the following formula:
Figure RE-GDA0002361837180000122
wherein
Figure RE-GDA0002361837180000123
Expressing the interface growth direction, the curvature undercooling K is calculated by the following formula:
Figure RE-GDA0002361837180000124
wherein ,
Figure RE-GDA0002361837180000125
and
Figure RE-GDA0002361837180000126
respectively representing first-order partial derivatives of the solid phase ratio on an x axis and a y axis;
Figure RE-GDA0002361837180000127
firstly, solving the second-order partial derivative of the y axis after solving the partial derivative of the solid phase ratio on the x axis;
Figure RE-GDA0002361837180000128
and
Figure RE-GDA0002361837180000129
respectively is a second order partial derivative of the solid fraction on an x axis and a y axis;
step 2.2, determining a fluid flow boundary, and calculating the velocity distribution of the flow field by adopting a D2Q9 model; the fluid flow boundary and its boundary conditions are determined. In the two-dimensional numerical simulation calculation, a D2Q9 model is generally used to calculate the flow field distribution, while ignoring the external force, and the liquid phase fluid particle calculation expression and the equilibrium state distribution function are calculated by the following formulas:
Figure RE-GDA0002361837180000131
Figure RE-GDA0002361837180000132
wherein τ is the dimensionless single-step relaxation time, fi(x+ciΔt,t+Δt)、fi(x, t) is a liquid phase fluid particle distribution function,
Figure RE-GDA0002361837180000133
is an equilibrium distribution function of liquid phase fluid particles; wherein c isiIs the migration velocity, Δ t, of liquid phase fluid particles in the direction of lattice iIs the time step; due to the adoption of the D2Q9 model, wherein ciThe sum of the calculation formula is the weight coefficient wiCalculated by the following formula:
Figure RE-GDA0002361837180000134
Figure RE-GDA0002361837180000135
Figure RE-GDA0002361837180000136
wherein c and csThe lattice velocity and the lattice sound velocity are respectively; the macroscopic density ρ, the macroscopic velocity u, and the hydrodynamic viscosity v are calculated by the following equations:
Figure RE-GDA0002361837180000137
Figure RE-GDA0002361837180000138
Figure RE-GDA0002361837180000141
wherein fiIs an entrance node distribution function, i (values of 0,1,2,3,4,5,6,7 and 8) is an angular step node ordinal number, and entrance density rhoinOutlet density ρoutThe velocity u of the fluid particles in the x-axis directionxAnd the velocity u of the fluid particles in the y-axis directionyThe calculation formula is calculated by the following formula:
Figure RE-GDA0002361837180000142
Figure RE-GDA0002361837180000143
Figure RE-GDA0002361837180000144
Figure RE-GDA0002361837180000145
Figure RE-GDA0002361837180000146
Figure RE-GDA0002361837180000147
Figure RE-GDA0002361837180000148
Figure RE-GDA0002361837180000149
f1=f3,f2=f4,f8=f6(19)
Figure RE-GDA00023618371800001410
step 2.3, calculating a liquid phase temperature field by adopting a cellular automaton model in combination with the velocity distribution of the flow field; the specific method is calculated by the following method:
firstly, the calculation of the liquid phase temperature field is the calculation in the heat transfer process, so the liquid phase region temperature field is calculated by adopting the following formula:
Figure RE-GDA0002361837180000151
wherein T is time, ρ is matrix density, λ is thermal conductivity, T is cell temperature, cpThe specific heat capacity of the matrix, fs the cellular solid phase rate and L the latent heat; q. q.sw,w、qw,e、qw,n、qw,sLeft, right, upper and lower boundaries, respectivelyThe heat flux density of the boundary in four directions; for the sake of simplifying the calculation, it is assumed that the thermal conductivity λ of the matrix in the x-axis and y-axis directions is equal;
the supercooling degree at the solid-liquid interface consists of component supercooling, curvature supercooling, thermal supercooling and dynamic supercooling degree, and the dynamic supercooling degree is neglected because the dynamic supercooling degree is smaller relative to other supercooling degrees in the solidification process; therefore, the supercooling degree is calculated by the following equation:
ΔT=ΔTc+ΔTr+(Tbulk-TL) (22)
wherein ,ΔTrIs undercooling of curvature, TbulkTemperature of liquid phase, T, at solidification frontLIs the liquidus temperature, Δ TcIs the supercooling of the components; the liquidus temperature, curvature supercooling and composition supercooling are respectively solved by the following formulas:
TL=1535-65[%C]-2.7[%Al]-90[%N](23)
Figure RE-GDA0002361837180000152
Figure RE-GDA0002361837180000153
wherein gamma is a Gibbs-Thomson coefficient; m isL,iIs the liquidus slope of element i; c. CL,iRepresents the liquid phase concentration of element i;
Figure RE-GDA0002361837180000154
the concentration of the solid-liquid interface front edge of the element i;
step 2.4, combining the flow field velocity distribution, and calculating solute distribution of the liquid phase region and the solid phase region by adopting a cellular automaton model; the specific method is as follows:
the interaction between solutes on the growth of dendrites is considered in the liquid phase, and the solute transport in the solid phase is smaller than that in the liquid phase by several orders of magnitude, so the solute interaction in the solid phase is ignored, and the solute transport in the solid phase and the solute transport in the liquid phase are respectively calculated by adopting the following formulas:
Figure RE-GDA0002361837180000161
Figure RE-GDA0002361837180000162
wherein ,CL,i、CS,iRespectively representing the concentration of the element i in the liquid phase and the solid phase; cS,iIs the transmission coefficient of the element i in the solid phase matrix; n-1, wherein n is the total number of elements in the molten steel, and the nth element represents a solvent;
Figure RE-GDA0002361837180000163
representing the Darken coefficient matrix in the liquid phase, assuming the directions of the x-axis and the y-axis in the matrix for simplifying the calculation
Figure RE-GDA0002361837180000164
The values are the same, and the following formula is utilized to solve:
Figure RE-GDA0002361837180000165
Figure RE-GDA0002361837180000166
Figure RE-GDA0002361837180000167
wherein R represents a gas constant, akIndicates the activity of the element k, xkDenotes the molar fraction of the element k, xjRepresents the molar fraction of the element j, δkiDenotes the Kronector delta function, when k is i, δkiTake 1, otherwise deltakiTaking 0; mkRepresents the mobility of the element k in the system, which is solved according to the einstein formula, as shown in the following formula:
Figure RE-GDA0002361837180000168
wherein ,
Figure RE-GDA0002361837180000169
representing the diffusion coefficient of the tracking element k. Assuming that a solid-liquid interface is in a thermodynamic equilibrium state, the solute distribution law is satisfied at the interface:
Figure RE-GDA00023618371800001610
according to the law of conservation of solute at the interface, the growth speed of interface cells in a thermodynamic equilibrium state is solved according to the following formula:
Figure RE-GDA0002361837180000171
wherein, the right side
Figure RE-GDA0002361837180000172
The solute transport item only considers the influence of the liquid phase solute interaction on the growth of dendrites;
Figure RE-GDA0002361837180000173
representing the growth speed of the interface cell solidification front; by solving the growth speed of the solidification front of the interface cells, the growth of the interface cells in unit time step is calculated by increasing the solid phase rate, and the following formula is shown:
Figure RE-GDA0002361837180000174
Figure RE-GDA0002361837180000175
Figure RE-GDA0002361837180000176
wherein ,
Figure RE-GDA0002361837180000177
and
Figure RE-GDA0002361837180000178
the cell solid phase ratio Δ f of AlN at the previous time and this time, respectivelys,AlNIncrease in solid fraction of (2); Δ t is a unit time step;
Figure RE-GDA0002361837180000179
indicating edge
Figure RE-GDA00023618371800001710
Unit length of direction through the center of the cell; Δ l ═ 1 μm for the grid cell length; theta represents the angle between the dendrite growth direction and the x-axis direction.
Function of normal phase and growth direction of solid-liquid interface
Figure RE-GDA00023618371800001711
Calculated by the following formula:
Figure RE-GDA00023618371800001712
wherein, θ and
Figure RE-GDA00023618371800001713
the included angles between the interface growth normal direction and the preferred growth direction and the positive direction of the x axis are respectively. ε represents the anisotropy parameter, where the angle between the preferential growth direction and the positive x-axis direction
Figure RE-GDA00023618371800001714
Calculated by the following formula:
Figure RE-GDA00023618371800001715
the reaction formula for generating AlN in the solid-liquid two-phase region and the calculation formula for activity and activity coefficient are as follows:
[Al]+[N]=(AlN) (39)
a[M]=[%M]f[M](40)
Figure RE-GDA0002361837180000181
wherein ,a[M]Representing the Henry activity of element M; m represents an element Al or N, [ M ]]Indicates that the element M is dissolved in the steel; [% M]Represents the concentration of the element M based on a mass 1% standard; f. of[Al] and f[N]Activity coefficients of elements Al and N, respectively, based on a mass 1% standard;
Figure RE-GDA0002361837180000184
representing the interaction coefficient of element j to element i; (as shown in table 2);
TABLE 2 solute interaction coefficients
Figure RE-GDA0002361837180000182
When a certain cell in the calculation region meets the AlN precipitation condition, marking the cell, carrying out 3 x 3 grid refinement division on the cell, and simultaneously calculating the growth of the cell according to dynamic chemical equilibrium, wherein the formula is as follows:
Figure RE-GDA0002361837180000183
MAlNrepresents the relative molecular mass of AlN; Δ x represents the reaction amount;
and for the complex boundary condition, the method is characterized in that Mei is adopted to correct the F-H format, the speed is increased along the x direction, the free boundary condition is added on the right side, and a lattice Boltzmann method is combined to establish a stress growth model of the lower dendrite of the Fe-C-Al-N quaternary alloy flow field.
Therefore, according to the Mei, the F-H format is modified by first aligning the solid phase boundary points xbAssume that it has a virtual state equilibrium distribution function as follows:
Figure RE-GDA0002361837180000191
wherein ufIs xfFluid velocity of (u)bfFor undetermined virtual velocity, to solve for ubfConstructing an interpolation factor α and xwPosition dependent, ubfThe following formula is used to obtain:
Figure RE-GDA0002361837180000192
Figure RE-GDA0002361837180000193
Figure RE-GDA0002361837180000194
wherein β is for calculating xfInterpolation factor, u, of the rebound distribution structurewIs xwThe moving speed of the interface; according to the formula, a virtual state balance distribution function can be solved; therefore, the solute field distribution and the solid phase region solute distribution under the Mei correction F-H format are obtained by the following formulas:
Figure RE-GDA0002361837180000195
Figure RE-GDA0002361837180000196
when the cell growth is calculated according to the dynamic chemical balance, in order to reduce the calculation error caused by the larger time step, the cells are subjected to spatial 3 x 3 refinement time division and time division, and are subjected to refinement time division at the same time, and the growth in a time step is subjected to multiple circulating calculation when the forced convection is calculated and calculated to stress the AlN dendrite for growth, so that the calculation error caused by the time step is reduced; when the volume of AlN in the matrix cell is increased and the matrix cell is contacted with the adjacent liquid-phase cell, the adjacent liquid-phase cell is subdivided into 3 multiplied by 3F-H format lower boundary AlN precipitation cells, and AlN growth is continued. And displaying the shape, the size and the stress condition of the AlN dendrite by using data and analysis and visual processing software images.
In this embodiment, the model parameter values involved in the calculation process are shown in table 3:
TABLE 3 model parameters in the calculation process
Figure RE-GDA0002361837180000201
Figure RE-GDA0002361837180000211
The embodiment is implemented by writing a numerical simulation program shown in figure 2 on a mathematical model for computing the stress of the forced convection to the AlN dendrites by using a C + + language based on a Visual Studio 2015 platform to obtain a simulation diagram of dendrite morphology evolution and Al solute distribution in a molten steel solidification flow field shown in figure 5; and (3) obtaining a branch crystal growth model under the flow field through numerical simulation, and providing theoretical guidance for optimizing the solidification technology, predicting the stress analysis of the dendritic crystal under the forced convection and improving the casting blank quality.
Finally, it should be noted that: the above examples are only intended to illustrate the technical solution of the present invention, but not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit of the corresponding technical solutions and scope of the present invention as defined in the appended claims.

Claims (5)

1. A method for calculating the stress of AlN dendrites by forced convection in the process of molten steel solidification in the field of metallurgy is characterized by comprising the following steps: the method comprises the following steps:
step 1, collecting steel grade components, thermodynamic and kinetic parameters in a solidification process and flow field boundary conditions;
step 2, based on a metal solidification theory, calculating the interface growth direction, the distribution of a liquid phase solute field and a temperature field and the distribution of a solid phase region solute field by using a cellular automaton model; meanwhile, a classical model D2Q9 model in a lattice Boltzmann method is coupled to calculate the velocity distribution of the flow field;
step 2.1, in order to enable the cellular automaton model to have certain physical significance, introducing a metal solidification theory, and calculating the growth direction and curvature supercooling of an interface by adopting a sharp interface model;
step 2.2, determining a fluid flow boundary, and calculating the velocity distribution of the flow field by adopting a D2Q9 model;
step 2.3, calculating a liquid phase temperature field by adopting a cellular automaton model in combination with the velocity distribution of the flow field;
step 2.4, combining the flow field velocity distribution, and calculating solute distribution of the liquid phase region and the solid phase region by adopting a cellular automaton model;
and 3, for the complex boundary flow, correcting an F-H format by adopting Mei, adding a free boundary condition on the right side along the speed of the complex boundary flow along the x direction, and establishing a stress growth model of the lower dendrite of the Fe-C-Al-N quaternary alloy flow field by combining a lattice Boltzmann method. And displaying the shape, the size and the stress condition of the AlN dendrite by using data and analysis and visual processing software images.
2. The method for calculating the stress of the AlN dendrites by forced convection in the process of molten steel solidification in the field of metallurgy according to claim 1 is characterized in that: the specific method of the step 2.1 comprises the following steps:
firstly, assuming that a solid-liquid interface is in a thermodynamic equilibrium state, and according to the solute conservation law at the interface, the growth direction of the interface is calculated by the following formula:
Figure RE-FDA0002361837170000021
wherein
Figure RE-FDA0002361837170000022
Expressing the interface growth direction, the curvature undercooling K is calculated by the following formula:
Figure RE-FDA0002361837170000023
wherein ,
Figure RE-FDA0002361837170000024
and
Figure RE-FDA0002361837170000025
respectively representing first-order partial derivatives of the solid phase ratio on an x axis and a y axis;
Figure RE-FDA0002361837170000026
firstly, solving the second-order partial derivative of the y axis after solving the partial derivative of the solid phase ratio on the x axis;
Figure RE-FDA0002361837170000027
and
Figure RE-FDA0002361837170000028
respectively is a second order partial derivative of the solid fraction on an x axis and a y axis;
the state of the cells is detected and the fluid flow boundary and its boundary conditions are determined as described in step 2.2. In the two-dimensional numerical simulation calculation, a D2Q9 model is generally used to calculate the flow field distribution, while ignoring the external force, the velocity distribution of the flow field is calculated by the following formula:
Figure RE-FDA0002361837170000029
Figure RE-FDA00023618371700000210
wherein τ is the dimensionless single-step relaxation time, fi(x+ciΔt,t+Δt)、fi(x, t) is the distribution function of the liquid phase fluid particles, fi eq(x, t) is the liquid phase fluid particle equilibrium distribution function; wherein c isiThe migration velocity of liquid phase fluid particles in the direction of the grid i, and delta t is a time step; due to the adoption of the D2Q9 model, wherein ciThe sum of the calculation formula is the weight coefficient wiCalculated by the following formula:
Figure RE-FDA0002361837170000031
Figure RE-FDA0002361837170000032
Figure RE-FDA0002361837170000033
wherein c and csThe lattice velocity and the lattice sound velocity are respectively; the macroscopic density ρ, the macroscopic velocity u, and the hydrodynamic viscosity v are calculated by the following equations:
Figure RE-FDA0002361837170000034
Figure RE-FDA0002361837170000035
Figure RE-FDA0002361837170000036
wherein fiIs an entrance node distribution function, i (values of 0,1,2,3,4,5,6,7 and 8) is an angular step node ordinal number, and entrance density rhoinOutlet density ρoutThe velocity u of the fluid particles in the x-axis directionxAnd the velocity u of the fluid particles in the y-axis directionyThe calculation formula is calculated by the following formula:
Figure RE-FDA0002361837170000037
Figure RE-FDA0002361837170000038
Figure RE-FDA0002361837170000039
Figure RE-FDA00023618371700000310
Figure RE-FDA00023618371700000311
Figure RE-FDA0002361837170000041
Figure RE-FDA0002361837170000042
Figure RE-FDA0002361837170000043
f1=f3,f2=f4,f8=f6(19)
Figure RE-FDA0002361837170000044
3. the method for calculating the stress on the AlN dendrite by the forced convection in the molten steel solidification process in the metallurgical field according to claim 1, wherein in the step 2.3, a cellular automaton model is adopted to calculate a liquid phase temperature field in combination with the velocity distribution of a flow field; the specific method is calculated by the following method:
firstly, the calculation of the liquid phase temperature field is the calculation in the heat transfer process, so the liquid phase region temperature field is calculated by adopting the following formula:
Figure RE-FDA0002361837170000045
wherein T is time, ρ is matrix density, λ is thermal conductivity, T is cell temperature, cpIs the specific heat capacity of the matrix, fs is the cellular solid phase rate,l is latent heat; q. q.sw,w、qw,e、qw,n、qw,sThe heat flux densities of the left boundary, the right boundary, the upper boundary and the lower boundary in four directions respectively; for the sake of simplifying the calculation, it is assumed that the thermal conductivity λ of the matrix in the x-axis and y-axis directions is equal;
the supercooling degree at the solid-liquid interface consists of component supercooling, curvature supercooling, thermal supercooling and dynamic supercooling degree, and the dynamic supercooling degree is neglected because the dynamic supercooling degree is smaller relative to other supercooling degrees in the solidification process; therefore, the supercooling degree is calculated by the following equation:
ΔT=ΔTc+ΔTr+(Tbulk-TL) (22)
wherein ,ΔTrIs undercooling of curvature, TbulkTemperature of liquid phase, T, at solidification frontLIs the liquidus temperature, Δ TcIs the supercooling of the components; the liquidus temperature, curvature supercooling and composition supercooling are respectively solved by the following formulas:
TL=1535-65[%C]-2.7[%Al]-90[%N](23)
Figure RE-FDA0002361837170000051
Figure RE-FDA0002361837170000052
wherein gamma is a Gibbs-Thomson coefficient; m isL,iIs the liquidus slope of element i; c. CL,iRepresents the liquid phase concentration of element i;
Figure RE-FDA0002361837170000053
the concentration of the solid-liquid interface front edge of the element i;
because the heat transfer density and the mass transfer density are inseparable in the forced convection AlN dendrite stress calculation method, the solute distribution of the liquid phase region and the solid phase region is calculated by adopting a cellular automaton model according to the flow field velocity distribution in the step 2.4; the interaction between solutes on the growth of dendrites is considered in the liquid phase, and the solute transport in the solid phase is smaller than that in the liquid phase by several orders of magnitude, so the solute interaction in the solid phase is ignored, and the solute transport in the solid phase and the solute transport in the liquid phase are respectively calculated by adopting the following formulas:
Figure RE-FDA0002361837170000054
Figure RE-FDA0002361837170000055
wherein ,CL,i、CS,iRespectively representing the concentration of the element i in the liquid phase and the solid phase; cS,iIs the transmission coefficient of the element i in the solid phase matrix; n-1, wherein n is the total number of elements in the molten steel, and the nth element represents a solvent;
Figure RE-FDA0002361837170000056
representing the Darken coefficient matrix in the liquid phase, assuming the directions of the x-axis and the y-axis in the matrix for simplifying the calculation
Figure RE-FDA0002361837170000057
The values are the same, and the following formula is utilized to solve:
Figure RE-FDA0002361837170000058
Figure RE-FDA0002361837170000059
Figure RE-FDA0002361837170000061
wherein R represents a gas constant, akIndicates the activity of the element k, xkDenotes the molar fraction of the element k, xjRepresents the molar fraction of the element j, δkiDenotes the Kronector delta function, when k is i, δkiTake 1, otherwise deltakiTaking 0; mkRepresents the element k in the systemIs solved according to the einstein formula, as shown in the following formula:
Figure RE-FDA0002361837170000062
wherein ,
Figure RE-FDA0002361837170000063
representing the diffusion coefficient of the tracking element k. Assuming that a solid-liquid interface is in a thermodynamic equilibrium state, the solute distribution law is satisfied at the interface:
Figure RE-FDA0002361837170000064
according to the law of conservation of solute at the interface, the growth speed of interface cells in a thermodynamic equilibrium state is solved according to the following formula:
Figure RE-FDA0002361837170000065
wherein, the right side
Figure RE-FDA0002361837170000066
The solute transport item only considers the influence of the liquid phase solute interaction on the growth of dendrites;
Figure RE-FDA0002361837170000067
representing the growth speed of the interface cell solidification front; by solving the growth speed of the solidification front of the interface cells, the growth of the interface cells in unit time step is calculated by increasing the solid phase rate, and the following formula is shown:
Figure RE-FDA0002361837170000068
Figure RE-FDA0002361837170000069
Figure RE-FDA00023618371700000613
wherein ,
Figure RE-FDA00023618371700000610
and
Figure RE-FDA00023618371700000611
the cell solid phase ratio Δ f of AlN at the previous time and this time, respectivelys,AlNIncrease in solid fraction of (2); Δ t is a unit time step;
Figure RE-FDA00023618371700000614
indicating edge
Figure RE-FDA00023618371700000612
Unit length of direction through the center of the cell; Δ l ═ 1 μm for the grid cell length; theta represents the angle between the dendrite growth direction and the x-axis direction.
4. The method for calculating the stress of the AlN dendrites by forced convection in the process of molten steel solidification in the field of metallurgy according to claim 3 is characterized in that:
the specific method of the step 2.4 comprises the following steps: the following assumptions are calculated and simulated for the calculation of the stress of the forced convection on the AlN dendrites: AlN precipitated in the steel does not contain other phases; only AlN precipitation in the liquid phase is considered; neglecting the increase of interface energy in the growth process; neglecting the heat change when AlN is precipitated; based on the above assumptions, the thermodynamic and kinetic conditions for AlN nucleation in steel are first calculated; when the nucleation condition is met, nucleation is carried out in the cell and the surrounding solute field is updated and calculated, as the AlN interface keeps a thermodynamic equilibrium state, the solute is continuously diffused to the interface, forced convection is carried out on the stress calculation simulation of the AlN dendrite according to the thermodynamic equilibrium state, and the solid-liquid interface normal phase and the growth direction function
Figure RE-FDA0002361837170000071
Calculated by the following formula:
Figure RE-FDA0002361837170000072
wherein, θ and
Figure RE-FDA0002361837170000073
the included angles between the interface growth normal direction and the preferred growth direction and the positive direction of the x axis are respectively. ε represents the anisotropy parameter, where the angle between the preferential growth direction and the positive x-axis direction
Figure RE-FDA0002361837170000074
Calculated by the following formula:
Figure RE-FDA0002361837170000075
the reaction formula for generating AlN in the solid-liquid two-phase region and the calculation formula for activity and activity coefficient are as follows:
[Al]+[N]=(AlN) (39)
a[M]=[%M]f[M](40)
Figure RE-FDA0002361837170000081
wherein ,a[M]Representing the Henry activity of element M; m represents an element Al or N, [ M ]]Indicates that the element M is dissolved in the steel; [% M]Represents the concentration of the element M based on a mass 1% standard; f. of[Al] and f[N]Activity coefficients of elements Al and N, respectively, based on a mass 1% standard; e.g. of the typei jRepresenting the interaction coefficient of element j to element i; when a certain cell in the calculation region meets the AlN precipitation condition, marking the cell, carrying out 3 x 3 grid refinement division on the cell, and simultaneously calculating the growth of the cell according to dynamic chemical equilibrium, wherein the formula is as follows:
Figure RE-FDA0002361837170000082
MAlNrepresents the relative molecular mass of AlN; Δ x represents the reaction amount.
5. The method for calculating the stress of the AlN dendrites by forced convection in the molten steel solidification process in the metallurgical field according to claim 4 is characterized in that an F-H format is modified by Mei, the speed in the x direction is increased, a free boundary condition is added on the right side, and a stress growth model of the dendrites under the Fe-C-Al-N quaternary alloy flow field is established by combining a lattice Boltzmann method.
Therefore, according to the Mei, the F-H format is modified by first aligning the solid phase boundary points xbAssume that it has a virtual state equilibrium distribution function as follows:
Figure RE-FDA0002361837170000083
wherein ufIs xfFluid velocity of (u)bfFor undetermined virtual velocity, to solve for ubfConstructing an interpolation factor α and xwPosition dependent, ubfThe following formula is used to obtain:
Figure RE-FDA0002361837170000084
Figure RE-FDA0002361837170000091
Figure RE-FDA0002361837170000092
wherein β is for calculating xfInterpolation factor, u, of the rebound distribution structurewIs xwThe moving speed of the interface; according to the formula, a virtual state balance distribution function can be solved; therefore, the solute field distribution and the solid phase region solute distribution under the Mei correction F-H format are solved by the following formulasObtaining:
Figure RE-FDA0002361837170000093
Figure RE-FDA0002361837170000094
when the cell growth is calculated according to the dynamic chemical balance, in order to reduce the calculation error caused by the larger time step, the cells are subjected to spatial 3 x 3 refinement time division and time division, and are subjected to refinement time division at the same time, and the growth in a time step is subjected to multiple circulating calculation when the forced convection is calculated and calculated to stress the AlN dendrite for growth, so that the calculation error caused by the time step is reduced; when the volume of AlN in the matrix cell is increased and the matrix cell is contacted with the adjacent liquid-phase cell, the adjacent liquid-phase cell is subdivided into 3 multiplied by 3F-H format lower boundary AlN precipitation cells, and AlN growth is continued. And displaying the shape, the size and the stress condition of the AlN dendrite by using data and analysis and visual processing software images.
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