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Surface Chemistry Tutorial Using the Plasma Module
Introduction
Surface chemistry is often the most important and most overlooked aspect of reacting flow modeling. Surface rate expressions can be hard to find or not even exist at all. Often it is preferable to use sticking coefficients to describe surface reactions because they can be estimated intuitively.
Model Definition
The tutorial model simulates outgassing from a wafer during a chemical vapor deposition (CVD) process. Careful attention is paid to the overall mass balance in the system and the difference between the mass averaged velocity and diffusion velocity is explored.
The same physical problem is investigated first with a global (volume-averaged) model and after with a space dependent model. An initial study of a problem with a global model is a good approach when there is limited knowledge about the system. One reason is that the global model has reduced computational times, allowing for fast sweeps over parametric spaces. The fast computational time of global models is also a great advantage to investigate models with complex chemistries.
In some cases a volume–averaged model might even be good enough to extract the desired information from the model. If, however, space dependent information is necessary, a space dependent model can be implemented in a subsequent study.
The geometry and operating principle for the model is shown in Figure 1. Initially the closed container is full of 99.9% silicon hydride and 0.1% hydrogen (measured by molar content).
Figure 1: Geometry and basic operating principle for the surface chemistry tutorial model.
A surface reaction begins to occur on the wafer which consumes the silicon hydride, releases hydrogen into the domain, alters the composition of the absorbed species on the wafer surface and deposits bulk silicon. The following reactions are considered on the surface of the wafer:
The (s) here denotes “surface species” which means that the species only exists on the surfaces where the reaction is occurring. To indicate that a species is bulk, append (b) to the end of the species. Since bulk species cannot participate in surface reactions, they must only be products and not reactants in a surface reaction. The net result of these two competing reactions is SiH4=>Si(b)+2H2, which means it is expected that the silane is replaced by hydrogen inside the reactor, and layers of silicon deposited on the wafer surface.
model equations — surface reactions and surface species
The surface reaction rate for reaction i is given by:
where ck is the molar concentration of species k. The rate constant kf can be given by
where Γtot is the total surface site concentration (SI unit: mol/m2), m is the reaction order minus 1, T is the surface temperature, R is the gas constant, Mk is the molecular weight, and γi is the sticking coefficient. When defining a surface reaction that contains no gas-phase reactants consider specifying the reaction using a rate coefficient. Otherwise, if using the equation above the mean gas-phase molecular weight is used.
For the surface species the following equations are solved:
where Zk is the site fraction (dimensionless), Rsurf,k is the surface rate expression (SI unit: mol/m2). The quantity Zk is the surface equivalent of the mole fraction on the volumetric level. That is, the sum of the site fractions must always equal one:
.
Empty sites are not accounted for in reaction rate coefficients, so all species which can occupy a surface must be included in the model. The surface site concentration is given by:
.
For each of the bulk surface species, the following equation is solved for the deposition height:
where hk is the total growth height (SI unit: m), Mk is the molecular weight (SI unit: kg/mol), and ρ is the density of the bulk species (SI unit: kg/m3).
domain equations
Inside the domain, the Navier-Stokes equations are solved for the fluid velocity. The mass fraction of hydrogen is computed by solving:
where w is the mass fraction of hydrogen. For detailed information on the transport of the non-electron species see Theory for the Heavy Species Transport Interface in the Plasma Module User’s Guide. The mass fraction of silane is not directly computed. Its value comes from the fact that the sum of the mass fractions must equal one. The gas temperature is computed by solving the energy equation.
boundary conditions
Fluid Flow
The following boundary conditions are used. The mass averaged velocity is constrained using:
where Mf is the inward (or outward in this example) mass flux which is defined, from the surface chemistry as:
where sk is the surface rate expression for each species which comes from summing the surface reaction rates multiplied by their stoichiometric coefficients over all surface reactions:
Hydrogen Mass Fraction
The flux of hydrogen at the surface of the wafer comes from the surface reactions:
Energy Equation
For the energy equation, the following boundary condition is used:
where hi is the molar enthalpy change due to reaction i.
Global model Equations
The global model used in this work considers that the spatial information of the different quantities in the plasma reactor can be treated as uniform. Without the spatial derivatives the numerical solution of the equation set becomes considerably simpler and the computational time is reduced. For detailed information on the global model see Theory for the Heavy Species Transport Interface in the Plasma Module User’s Guide. For heavy species, the following equation is solved for the mass fraction:
where ρ is the mass density (SI unit: kg/m3), wk is the mass fraction, and Rk is the rate expression (SI unit: kg/(m3.s)). The fourth term on the right hand side accounts for surface losses and creation, where Al is the surface area, hl is a dimensionless correction, V is the reactor volume, Mk is the species molar mass (SI unit: kg/mol) and Rsurf,k,l is the surface rate expression (SI unit: mol/(m2.s)) at a surface l. The last term on the right-hand side is introduced because the species mass balance equations are written in the nonconservative form and it used the mass-continuity equation to replace for the mass density time derivative. In the last term, Mf,l is the inward mass flux of surface l (SI unit: kg/(m2·s)). The sum in the last two terms is over all surfaces where there are surface reactions.
To take into account possible variations of the system total mass or pressure, the mass-continuity equation is also solved:
.
The gas temperature is set to a constant value. The model for the surface chemistry is exactly the same.
Results and Discussion
In this section, both space-dependent and global model results are presented and discussed. For this particular physical system, the results from the global model and the space dependent model are in a very good agreement.
The y-component of the mass-averaged velocity is plotted in Figure 2. The mass-averaged velocity is negative at the surface of the wafer. This means that overall, mass is leaving the system. This is to be expected since silane is being consumed, which has a molecular weight of 0.032 kg/mol and replacing it with hydrogen, which has a lower molecular weight of 0.002 kg/mol.
Figure 2: Plot of the mass averaged velocity field after 5 seconds.
The surface reactions begin to consume the silane, which results in concentration gradients within the reactor. The outward mass flux at the wafer surface leads to a mass-averaged velocity everywhere inside the reactor. The combination of concentration gradients and convection due to the mass-averaged velocity tends to draw silane toward the wafer. The first surface reaction is exothermic while the second surface reaction is endothermic. The amount of heat released by the exothermic reaction dominates, so the temperature begins to increase. The temperature is plotted in Figure 3 and is highest on the wafer surface.
Figure 3: Plot of the change in gas temperature after 5 seconds. The higher temperature is observed at the wafer surface due to the heat released in the surface reactions.
From the net reaction SiH4=>Si(b)+2H2 there should be a molar inflow of hydrogen at twice the rate that silane is leaving. Although this condition is not applied explicitly, it is implicit from the equations solved in the Heavy Species transport interface. Despite the fact that there is a negative mass-averaged velocity, there is a positive diffusion velocity for the hydrogen at the wafer surface. The y-component of the diffusion velocity for hydrogen is plotted in Figure 4.
Figure 4: Plot of the y-component of the diffusion velocity for hydrogen after 5 seconds. Even though the mass-averaged velocity is negative, the diffusion velocity is positive, indicating an inflow of hydrogen and a net outflow of total mass.
Figure 5 plots the integrated pressure in the reactor divided by the initial average pressure in the reactor. Once the problem reaches steady state, the average pressure in the reactor has increased by a factor of 2. This is expected since every mole of silane is being replaced by two moles of hydrogen. The silane in the reactor is completely consumed after around 200 seconds.
Figure 5: Plot of the ratio of the average pressure by the average initial pressure computed with the global model (blue) and the space dependent model (green).
In Figure 6, the total mass initially present in the reactor divided by the total mass in the reactor is plotted. The total mass in the reactor drops by a factor of 8, which is expected since the silane with molecular mass 0.032 kg/mol is replaced with two moles of hydrogen, which has a molecular weight of 2·0.002=0.004 kg/mol.
Figure 6: Plot of the ratio of the total mass by the total mass computed with the global model (blue) and the space dependent model (green).
Another way of verifying the correctness of the model is to compare the mass lost inside the reactor to the mass accumulated on the wafer surface. The two quantities should be equal. The total gain in mass from surface and bulk species is compared to the total loss in mass from the reactor in Figure 7. The two curves agree very well, indicating that the total mass in the entire system is conserved.
Figure 7: Plot of the total mass lost in the domain (blue: global model, and red: space dependent model) and the total mass gained due to Silicon deposition on the wafer surface (green: global model and cyan: space dependent model).
The ultimate goal of most CVD models is to determine the total growth height and growth rate on the surface of the wafer. The total growth height is plotted in Figure 8 and saturates at about 159 angstroms. The total growth rate saturates because all the silane in the reactor is consumed after around 200 seconds. The accumulated growth height is also very uniform across the surface of the wafer. The global model and space dependent model results for the total growth height agrees very well (not shown).
Figure 8: Plot of the growth height (surface and z-axis) vs. the wafer arc length (x-axis) and time (y-axis). The final height of deposited silicon is 158 Å.
Reference
1. R.J. Kee, M.E. Coltrin, and P. Glarborg, Chemically Reacting Flow Theory and Practice, John Wiley & Sons, 2003.
Application Library path: Plasma_Module/Chemical_Vapor_Deposition/surface_chemistry_tutorial
Modeling Instructions
From the File menu, choose New.
New
In the New window, click  Model Wizard.
Model Wizard
1
In the Model Wizard window, click  2D.
2
In the Select Physics tree, select Plasma>Species Transport>Heavy Species Transport (hs).
3
Click Add.
4
Click  Study.
5
In the Select Study tree, select General Studies>Time Dependent.
6
Geometry 1
Square 1 (sq1)
1
In the Geometry toolbar, click  Square.
2
In the Settings window for Square, locate the Size section.
3
In the Side length text field, type 0.1.
Polygon 1 (pol1)
1
In the Geometry toolbar, click  Polygon.
2
In the Settings window for Polygon, locate the Coordinates section.
3
Definitions
Variables 1
1
In the Model Builder window, under Component 1 (comp1) right-click Definitions and choose Variables.
2
In the Settings window for Variables, locate the Variables section.
3
Click  Load from File.
4
Integration 1 (intop1)
1
In the Definitions toolbar, click  Nonlocal Couplings and choose Integration.
2
Integration 2 (intop2)
1
In the Definitions toolbar, click  Nonlocal Couplings and choose Integration.
2
In the Settings window for Integration, locate the Source Selection section.
3
From the Geometric entity level list, choose Boundary.
4
Heavy Species Transport (hs)
1
In the Model Builder window, under Component 1 (comp1) click Heavy Species Transport (hs).
2
In the Settings window for Heavy Species Transport, locate the Diffusion Model section.
3
From the Diffusion model list, choose Global.
Surface Reaction 1
1
In the Physics toolbar, click  Boundaries and choose Surface Reaction.
2
In the Settings window for Surface Reaction, locate the Reaction Formula section.
3
In the Formula text field, type SiH4+2Si(s)=>Si(b)+2SiH(s)+H2.
4
5
Locate the Reaction Parameters section. In the γf text field, type 2e-4.
Surface Reaction 2
1
In the Physics toolbar, click  Boundaries and choose Surface Reaction.
2
In the Settings window for Surface Reaction, locate the Reaction Formula section.
3
In the Formula text field, type SiH(s)=>Si(s)+0.5H2.
4
5
From the Specify reaction using list, choose Rate coefficient.
6
Locate the Reaction Parameters section. In the ksf text field, type 3.
Species: SiH4
1
In the Model Builder window, click Species: SiH4.
2
In the Settings window for Species, locate the Species Formula section.
3
Select the From mass constraint check box.
4
Locate the General Parameters section. From the Preset species data list, choose SiH4.
Species: H2
1
In the Model Builder window, click Species: H2.
2
In the Settings window for Species, locate the General Parameters section.
3
From the Preset species data list, choose H2.
4
In the x0 text field, type 1E-3.
Species: Si(s)
1
In the Model Builder window, click Species: Si(s).
2
In the Settings window for Surface Species, locate the General Parameters section.
3
From the Preset species data list, choose Si.
4
Locate the Surface Species Parameters section. In the Zk,0 text field, type 0.995.
Species: Si(b)
1
In the Model Builder window, click Species: Si(b).
2
In the Settings window for Surface Species, locate the General Parameters section.
3
From the Preset species data list, choose Si.
Species: SiH(s)
1
In the Model Builder window, click Species: SiH(s).
2
In the Settings window for Surface Species, locate the General Parameters section.
3
From the Preset species data list, choose SiH.
4
Locate the Surface Species Parameters section. In the Zk,0 text field, type 0.005.
Heavy Species Model 1
1
In the Model Builder window, click Heavy Species Model 1.
2
In the Settings window for Heavy Species Model, locate the Model Inputs section.
3
In the p0 text field, type 13.3.
Global model
1
In the Model Builder window, click Study 1.
2
In the Settings window for Study, type Global model in the Label text field.
3
Locate the Study Settings section. Clear the Generate default plots check box.
4
Clear the Generate convergence plots check box.
Step 1: Time Dependent
1
In the Model Builder window, under Global model click Step 1: Time Dependent.
2
In the Settings window for Time Dependent, locate the Study Settings section.
3
In the Output times text field, type range(0,5,300).
4
In the Home toolbar, click  Compute.
Results
Average Pressure Divided by Average Initial Pressure
1
In the Home toolbar, click  Add Plot Group and choose 1D Plot Group.
2
In the Settings window for 1D Plot Group, type Average Pressure Divided by Average Initial Pressure in the Label text field.
3
Locate the Legend section. From the Position list, choose Lower right.
Global model
1
Right-click Average Pressure Divided by Average Initial Pressure and choose Global.
2
In the Settings window for Global, type Global model in the Label text field.
3
Locate the Data section. From the Dataset list, choose Global model/Solution 1 (sol1).
4
Locate the y-Axis Data section. In the table, enter the following settings:
5
Click to expand the Legends section. From the Legends list, choose Manual.
6
7
In the Average Pressure Divided by Average Initial Pressure toolbar, click  Plot.
Density ratio
1
In the Home toolbar, click  Add Plot Group and choose 1D Plot Group.
2
In the Settings window for 1D Plot Group, type Density ratio in the Label text field.
3
Locate the Legend section. From the Position list, choose Lower right.
Global model
1
Right-click Density ratio and choose Global.
2
In the Settings window for Global, type Global model in the Label text field.
3
Locate the Data section. From the Dataset list, choose Global model/Solution 1 (sol1).
4
Locate the y-Axis Data section. In the table, enter the following settings:
5
Locate the Legends section. From the Legends list, choose Manual.
6
7
In the Density ratio toolbar, click  Plot.
Total Reactor Mass
1
In the Home toolbar, click  Add Plot Group and choose 1D Plot Group.
2
In the Settings window for 1D Plot Group, type Total Reactor Mass in the Label text field.
3
Locate the Legend section. From the Position list, choose Lower right.
Global model
1
Right-click Total Reactor Mass and choose Global.
2
In the Settings window for Global, type Global model in the Label text field.
3
Locate the Data section. From the Dataset list, choose Global model/Solution 1 (sol1).
4
Locate the y-Axis Data section. In the table, enter the following settings:
5
Locate the Legends section. From the Legends list, choose Manual.
6
7
In the Total Reactor Mass toolbar, click  Plot.
Edge 2D 1
1
In the Model Builder window, expand the Results>Datasets node.
2
Right-click Results>Datasets and choose Edge 2D.
3
Parametric Extrusion 1D 1
In the Results toolbar, click  More Datasets and choose Parametric Extrusion 1D.
Parametric Extrusion 1D 1 - Global model
1
In the Results toolbar, click  2D Plot Group.
2
In the Settings window for 2D Plot Group, type Parametric Extrusion 1D 1 - Global model in the Label text field.
3
Locate the Data section. From the Dataset list, choose Parametric Extrusion 1D 1.
Surface 1
1
Right-click Parametric Extrusion 1D 1 - Global model and choose Surface.
2
In the Settings window for Surface, locate the Expression section.
3
In the Expression text field, type Hk_Si_bulk.
4
From the Unit list, choose Å.
Height Expression 1
1
Right-click Surface 1 and choose Height Expression.
Add the physics interfaces necessary for the space-dependent simulations.
Add Physics
1
In the Home toolbar, click  Add Physics to open the Add Physics window.
2
Go to the Add Physics window.
3
In the tree, select Fluid Flow>Single-Phase Flow>Laminar Flow (spf).
4
Find the Physics interfaces in study subsection. In the table, clear the Solve check box for Global model.
5
Click Add to Component 1 in the window toolbar.
6
In the tree, select Heat Transfer>Heat Transfer in Fluids (ht).
7
In the table, clear the Solve check box for Global model.
8
Click Add to Component 1 in the window toolbar.
9
In the Home toolbar, click  Add Physics to close the Add Physics window.
Heavy Species Transport (hs)
Change the Diffusion Model to Mixture-averaged for the space dependent simulations.
1
In the Model Builder window, under Component 1 (comp1) click Heavy Species Transport (hs).
2
In the Settings window for Heavy Species Transport, locate the Diffusion Model section.
3
From the Diffusion model list, choose Mixture-averaged.
4
Locate the Transport Settings section. Find the Include subsection. Select the Calculate thermodynamic properties check box.
5
Clear the Migration in electric field check box.
6
Select the Convection check box.
2: SiH(s)=>Si(s)+0.5H2
1
In the Model Builder window, under Component 1 (comp1)>Heavy Species Transport (hs) click 2: SiH(s)=>Si(s)+0.5H2.
2
In the Settings window for Surface Reaction, locate the Reaction Formula section.
3
From the Specify reaction using list, choose Rate coefficient.
Heavy Species Model 1
1
In the Model Builder window, click Heavy Species Model 1.
2
In the Settings window for Heavy Species Model, locate the Model Inputs section.
3
From the T list, choose Temperature (ht).
4
From the pA list, choose Absolute pressure (spf).
5
From the u list, choose Velocity field (spf).
Laminar Flow (spf)
Since the density variation is not small, the flow cannot be regarded as incompressible. Therefore set the flow to be compressible.
1
In the Model Builder window, under Component 1 (comp1) click Laminar Flow (spf).
2
In the Settings window for Laminar Flow, locate the Physical Model section.
3
From the Compressibility list, choose Compressible flow (Ma<0.3).
Define the pressure reference level in the interface properties.
4
In the pref text field, type 13.3[Pa].
5
Click the  Show More Options button in the Model Builder toolbar.
6
In the Show More Options dialog box, in the tree, select the check box for the node Physics>Stabilization.
7
In the tree, select the check box for the node Physics>Advanced Physics Options.
8
9
In the Model Builder window, click Laminar Flow (spf).
10
In the Settings window for Laminar Flow, click to expand the Consistent Stabilization section.
11
Find the Navier-Stokes equations subsection. Clear the Crosswind diffusion check box.
12
Click to expand the Discretization section. From the Discretization of fluids list, choose P2+P1.
Fluid Properties 1
1
In the Model Builder window, under Component 1 (comp1)>Laminar Flow (spf) click Fluid Properties 1.
2
In the Settings window for Fluid Properties, locate the Fluid Properties section.
3
From the ρ list, choose Density (hs/cdm1).
4
From the μ list, choose Dynamic viscosity (hs/cdm1).
Inlet 1
1
In the Physics toolbar, click  Boundaries and choose Inlet.
2
3
In the Settings window for Inlet, locate the Boundary Condition section.
4
5
Locate the Mass Flow section. From the Mass flow type list, choose Pointwise mass flux.
6
From the Mf list, choose Inward mass flux (hs).
Reaction forces must apply to the velocities only in order to avoid undesired couplings to the surface reactions, so use a unidirectional constraint.
7
Click to expand the Constraint Settings section. From the Apply reaction terms on list, choose Individual dependent variables.
Heat Transfer in Fluids (ht)
Fluid 1
1
In the Model Builder window, under Component 1 (comp1)>Heat Transfer in Fluids (ht) click Fluid 1.
2
In the Settings window for Fluid, locate the Heat Convection section.
3
From the u list, choose Velocity field (spf).
4
Locate the Heat Conduction, Fluid section. From the k list, choose Thermal conductivity (hs/cdm1).
5
Locate the Thermodynamics, Fluid section. From the Fluid type list, choose Ideal gas.
6
From the Gas constant type list, choose Mean molar mass.
7
From the Mn list, choose Mean molar mass (hs/cdm1).
8
From the Cp list, choose Heat capacity at constant pressure (hs/cdm1).
Temperature 1
1
In the Physics toolbar, click  Boundaries and choose Temperature.
2
In the Settings window for Temperature, locate the Temperature section.
3
In the T0 text field, type 300.
4
Initial Values 1
1
In the Model Builder window, click Initial Values 1.
2
In the Settings window for Initial Values, locate the Initial Values section.
3
In the T text field, type 300.
Boundary Heat Source 1
1
In the Physics toolbar, click  Boundaries and choose Boundary Heat Source.
2
3
In the Settings window for Boundary Heat Source, locate the Boundary Heat Source section.
4
From the Qb list, choose Total surface heat source of reaction (hs).
Mesh 1
Size 1
1
In the Model Builder window, under Component 1 (comp1) right-click Mesh 1 and choose Size.
2
In the Settings window for Size, locate the Geometric Entity Selection section.
3
From the Geometric entity level list, choose Point.
4
5
Locate the Element Size section. From the Predefined list, choose Extremely fine.
6
Click the Custom button.
7
Locate the Element Size Parameters section. Select the Maximum element size check box.
8
Edge 1
1
In the Mesh toolbar, click  Edge.
2
Size 1
1
Right-click Edge 1 and choose Size.
2
In the Settings window for Size, locate the Element Size section.
3
From the Predefined list, choose Extremely fine.
Free Triangular 1
1
In the Mesh toolbar, click  Free Triangular.
2
In the Settings window for Free Triangular, click  Build All.
Add Study
1
In the Home toolbar, click  Add Study to open the Add Study window.
2
Go to the Add Study window.
Add a new study to perform the space dependent simulations.
3
Find the Studies subsection. In the Select Study tree, select General Studies>Time Dependent.
4
Click Add Study in the window toolbar.
5
In the Home toolbar, click  Add Study to close the Add Study window.
Study 2
Step 1: Time Dependent
1
In the Settings window for Time Dependent, locate the Study Settings section.
2
In the Output times text field, type range(0,5,300).
3
In the Model Builder window, click Study 2.
4
In the Settings window for Study, type Space dependent model in the Label text field.
Solution 2 (sol2)
1
In the Study toolbar, click  Show Default Solver.
2
In the Model Builder window, expand the Solution 2 (sol2) node.
3
In the Model Builder window, under Space dependent model>Solver Configurations>Solution 2 (sol2) click Time-Dependent Solver 1.
4
In the Settings window for Time-Dependent Solver, click to expand the Absolute Tolerance section.
5
From the Global method list, choose Unscaled.
6
Click to expand the Time Stepping section. In the Initial step text field, type 0.001.
7
Click  Compute.
Results
Velocity (spf)
1
In the Settings window for 2D Plot Group, locate the Data section.
2
From the Time (s) list, choose 5.
Surface
1
In the Model Builder window, expand the Velocity (spf) node, then click Surface.
2
In the Settings window for Surface, locate the Expression section.
3
In the Expression text field, type v.
4
In the Velocity (spf) toolbar, click  Plot.
Temperature (ht)
1
In the Model Builder window, under Results click Temperature (ht).
2
In the Settings window for 2D Plot Group, locate the Data section.
3
From the Time (s) list, choose 5.
Surface
1
In the Model Builder window, expand the Temperature (ht) node, then click Surface.
2
In the Settings window for Surface, locate the Expression section.
3
In the Expression text field, type T-300[K].
4
In the Temperature (ht) toolbar, click  Plot.
Diffusion Velocity, Hydrogen
1
In the Home toolbar, click  Add Plot Group and choose 2D Plot Group.
2
In the Settings window for 2D Plot Group, type Diffusion Velocity, Hydrogen in the Label text field.
3
Locate the Data section. From the Time (s) list, choose 5.
4
From the Dataset list, choose Space dependent model/Solution 2 (sol2).
Surface 1
1
Right-click Diffusion Velocity, Hydrogen and choose Surface.
2
In the Settings window for Surface, locate the Expression section.
3
In the Expression text field, type hs.Vdy_wH2.
4
In the Diffusion Velocity, Hydrogen toolbar, click  Plot.
Plot the global model and space dependent simulation together.
Average Pressure Divided by Average Initial Pressure
1
In the Model Builder window, under Results click Average Pressure Divided by Average Initial Pressure.
2
In the Settings window for 1D Plot Group, click to expand the Title section.
3
From the Title type list, choose None.
4
Locate the Plot Settings section. Select the y-axis label check box.
5
In the associated text field, type Average pressure divided by average initial pressure.
Space dependent model
1
Right-click Average Pressure Divided by Average Initial Pressure and choose Global.
2
In the Settings window for Global, type Space dependent model in the Label text field.
3
Locate the Data section. From the Dataset list, choose Space dependent model/Solution 2 (sol2).
4
Locate the y-Axis Data section. In the table, enter the following settings:
5
Locate the Legends section. From the Legends list, choose Manual.
6
7
In the Average Pressure Divided by Average Initial Pressure toolbar, click  Plot.
Density ratio
1
In the Model Builder window, under Results click Density ratio.
2
In the Settings window for 1D Plot Group, locate the Title section.
3
From the Title type list, choose None.
4
Locate the Plot Settings section. Select the y-axis label check box.
5
In the associated text field, type Initial mass divided by the mass in the reactor.
Space dependent model
1
Right-click Density ratio and choose Global.
2
In the Settings window for Global, type Space dependent model in the Label text field.
3
Locate the Data section. From the Dataset list, choose Space dependent model/Solution 2 (sol2).
4
Locate the y-Axis Data section. In the table, enter the following settings:
5
Locate the Legends section. From the Legends list, choose Manual.
6
7
In the Density ratio toolbar, click  Plot.
Total Reactor Mass
1
In the Model Builder window, under Results click Total Reactor Mass.
2
In the Settings window for 1D Plot Group, locate the Title section.
3
From the Title type list, choose None.
4
Locate the Plot Settings section. Select the y-axis label check box.
5
Space dependent model
1
Right-click Total Reactor Mass and choose Global.
2
In the Settings window for Global, type Space dependent model in the Label text field.
3
Locate the Data section. From the Dataset list, choose Space dependent model/Solution 2 (sol2).
4
Locate the y-Axis Data section. In the table, enter the following settings:
5
Locate the Legends section. From the Legends list, choose Manual.
6
7
In the Total Reactor Mass toolbar, click  Plot.
Plot the Si growth height computed with the space dependent model.
Edge 2D 2
1
In the Results toolbar, click  More Datasets and choose Edge 2D.
2
In the Settings window for Edge 2D, locate the Data section.
3
From the Dataset list, choose Space dependent model/Solution 2 (sol2).
4
Parametric Extrusion 1D 2
1
In the Results toolbar, click  More Datasets and choose Parametric Extrusion 1D.
2
In the Settings window for Parametric Extrusion 1D, locate the Data section.
3
From the Dataset list, choose Edge 2D 2.
Parametric Extrusion 1D 1 - Space dependent model
1
In the Model Builder window, right-click Parametric Extrusion 1D 1 - Global model and choose Duplicate.
2
In the Settings window for 2D Plot Group, type Parametric Extrusion 1D 1 - Space dependent model in the Label text field.
3
Locate the Data section. From the Dataset list, choose Parametric Extrusion 1D 2.
4
In the Parametric Extrusion 1D 1 - Space dependent model toolbar, click  Plot.
5
Click the  Zoom Extents button in the Graphics toolbar.