- •ANSYS Fluent Tutorial Guide
- •Table of Contents
- •Using This Manual
- •1. What’s In This Manual
- •2. How To Use This Manual
- •2.1. For the Beginner
- •2.2. For the Experienced User
- •3. Typographical Conventions Used In This Manual
- •Chapter 1: Fluid Flow in an Exhaust Manifold
- •1.1. Introduction
- •1.2. Prerequisites
- •1.3. Problem Description
- •1.4. Setup and Solution
- •1.4.1. Preparation
- •1.4.2. Meshing Workflow
- •1.4.3. General Settings
- •1.4.4. Solver Settings
- •1.4.5. Models
- •1.4.6. Materials
- •1.4.7. Cell Zone Conditions
- •1.4.8. Boundary Conditions
- •1.4.9. Solution
- •1.4.10. Postprocessing
- •1.5. Summary
- •Chapter 2: Fluid Flow and Heat Transfer in a Mixing Elbow
- •2.1. Introduction
- •2.2. Prerequisites
- •2.3. Problem Description
- •2.4. Setup and Solution
- •2.4.1. Preparation
- •2.4.2. Launching ANSYS Fluent
- •2.4.3. Reading the Mesh
- •2.4.4. Setting Up Domain
- •2.4.5. Setting Up Physics
- •2.4.6. Solving
- •2.4.7. Displaying the Preliminary Solution
- •2.4.8. Adapting the Mesh
- •2.5. Summary
- •Chapter 3: Postprocessing
- •3.1. Introduction
- •3.2. Prerequisites
- •3.3. Problem Description
- •3.4. Setup and Solution
- •3.4.1. Preparation
- •3.4.2. Reading the Mesh
- •3.4.3. Manipulating the Mesh in the Viewer
- •3.4.4. Adding Lights
- •3.4.5. Creating Isosurfaces
- •3.4.6. Generating Contours
- •3.4.7. Generating Velocity Vectors
- •3.4.8. Creating an Animation
- •3.4.9. Displaying Pathlines
- •3.4.10. Creating a Scene With Vectors and Contours
- •3.4.11. Advanced Overlay of Pathlines on a Scene
- •3.4.12. Creating Exploded Views
- •3.4.13. Animating the Display of Results in Successive Streamwise Planes
- •3.4.14. Generating XY Plots
- •3.4.15. Creating Annotation
- •3.4.16. Saving Picture Files
- •3.4.17. Generating Volume Integral Reports
- •3.5. Summary
- •Chapter 4: Modeling Periodic Flow and Heat Transfer
- •4.1. Introduction
- •4.2. Prerequisites
- •4.3. Problem Description
- •4.4. Setup and Solution
- •4.4.1. Preparation
- •4.4.2. Mesh
- •4.4.3. General Settings
- •4.4.4. Models
- •4.4.5. Materials
- •4.4.6. Cell Zone Conditions
- •4.4.7. Periodic Conditions
- •4.4.8. Boundary Conditions
- •4.4.9. Solution
- •4.4.10. Postprocessing
- •4.5. Summary
- •4.6. Further Improvements
- •Chapter 5: Modeling External Compressible Flow
- •5.1. Introduction
- •5.2. Prerequisites
- •5.3. Problem Description
- •5.4. Setup and Solution
- •5.4.1. Preparation
- •5.4.2. Mesh
- •5.4.3. Solver
- •5.4.4. Models
- •5.4.5. Materials
- •5.4.6. Boundary Conditions
- •5.4.7. Operating Conditions
- •5.4.8. Solution
- •5.4.9. Postprocessing
- •5.5. Summary
- •5.6. Further Improvements
- •Chapter 6: Modeling Transient Compressible Flow
- •6.1. Introduction
- •6.2. Prerequisites
- •6.3. Problem Description
- •6.4. Setup and Solution
- •6.4.1. Preparation
- •6.4.2. Reading and Checking the Mesh
- •6.4.3. Solver and Analysis Type
- •6.4.4. Models
- •6.4.5. Materials
- •6.4.6. Operating Conditions
- •6.4.7. Boundary Conditions
- •6.4.8. Solution: Steady Flow
- •6.4.9. Enabling Time Dependence and Setting Transient Conditions
- •6.4.10. Specifying Solution Parameters for Transient Flow and Solving
- •6.4.11. Saving and Postprocessing Time-Dependent Data Sets
- •6.5. Summary
- •6.6. Further Improvements
- •Chapter 7: Modeling Flow Through Porous Media
- •7.1. Introduction
- •7.2. Prerequisites
- •7.3. Problem Description
- •7.4. Setup and Solution
- •7.4.1. Preparation
- •7.4.2. Mesh
- •7.4.3. General Settings
- •7.4.4. Models
- •7.4.5. Materials
- •7.4.6. Cell Zone Conditions
- •7.4.7. Boundary Conditions
- •7.4.8. Solution
- •7.4.9. Postprocessing
- •7.5. Summary
- •7.6. Further Improvements
- •Chapter 8: Modeling Radiation and Natural Convection
- •8.1. Introduction
- •8.2. Prerequisites
- •8.3. Problem Description
- •8.4. Setup and Solution
- •8.4.1. Preparation
- •8.4.2. Reading and Checking the Mesh
- •8.4.3. Solver and Analysis Type
- •8.4.4. Models
- •8.4.5. Defining the Materials
- •8.4.6. Operating Conditions
- •8.4.7. Boundary Conditions
- •8.4.8. Obtaining the Solution
- •8.4.9. Postprocessing
- •8.4.10. Comparing the Contour Plots after Varying Radiating Surfaces
- •8.4.11. S2S Definition, Solution, and Postprocessing with Partial Enclosure
- •8.5. Summary
- •8.6. Further Improvements
- •Chapter 9: Using a Single Rotating Reference Frame
- •9.1. Introduction
- •9.2. Prerequisites
- •9.3. Problem Description
- •9.4. Setup and Solution
- •9.4.1. Preparation
- •9.4.2. Mesh
- •9.4.3. General Settings
- •9.4.4. Models
- •9.4.5. Materials
- •9.4.6. Cell Zone Conditions
- •9.4.7. Boundary Conditions
- •9.4.8. Solution Using the Standard k- ε Model
- •9.4.9. Postprocessing for the Standard k- ε Solution
- •9.4.10. Solution Using the RNG k- ε Model
- •9.4.11. Postprocessing for the RNG k- ε Solution
- •9.5. Summary
- •9.6. Further Improvements
- •9.7. References
- •Chapter 10: Using Multiple Reference Frames
- •10.1. Introduction
- •10.2. Prerequisites
- •10.3. Problem Description
- •10.4. Setup and Solution
- •10.4.1. Preparation
- •10.4.2. Mesh
- •10.4.3. Models
- •10.4.4. Materials
- •10.4.5. Cell Zone Conditions
- •10.4.6. Boundary Conditions
- •10.4.7. Solution
- •10.4.8. Postprocessing
- •10.5. Summary
- •10.6. Further Improvements
- •Chapter 11: Using Sliding Meshes
- •11.1. Introduction
- •11.2. Prerequisites
- •11.3. Problem Description
- •11.4. Setup and Solution
- •11.4.1. Preparation
- •11.4.2. Mesh
- •11.4.3. General Settings
- •11.4.4. Models
- •11.4.5. Materials
- •11.4.6. Cell Zone Conditions
- •11.4.7. Boundary Conditions
- •11.4.8. Operating Conditions
- •11.4.9. Mesh Interfaces
- •11.4.10. Solution
- •11.4.11. Postprocessing
- •11.5. Summary
- •11.6. Further Improvements
- •Chapter 12: Using Overset and Dynamic Meshes
- •12.1. Prerequisites
- •12.2. Problem Description
- •12.3. Preparation
- •12.4. Mesh
- •12.5. Overset Interface Creation
- •12.6. Steady-State Case Setup
- •12.6.1. General Settings
- •12.6.2. Models
- •12.6.3. Materials
- •12.6.4. Operating Conditions
- •12.6.5. Boundary Conditions
- •12.6.6. Reference Values
- •12.6.7. Solution
- •12.7. Unsteady Setup
- •12.7.1. General Settings
- •12.7.2. Compile the UDF
- •12.7.3. Dynamic Mesh Settings
- •12.7.4. Report Generation for Unsteady Case
- •12.7.5. Run Calculations for Unsteady Case
- •12.7.6. Overset Solution Checking
- •12.7.7. Postprocessing
- •12.7.8. Diagnosing an Overset Case
- •12.8. Summary
- •Chapter 13: Modeling Species Transport and Gaseous Combustion
- •13.1. Introduction
- •13.2. Prerequisites
- •13.3. Problem Description
- •13.4. Background
- •13.5. Setup and Solution
- •13.5.1. Preparation
- •13.5.2. Mesh
- •13.5.3. General Settings
- •13.5.4. Models
- •13.5.5. Materials
- •13.5.6. Boundary Conditions
- •13.5.7. Initial Reaction Solution
- •13.5.8. Postprocessing
- •13.5.9. NOx Prediction
- •13.6. Summary
- •13.7. Further Improvements
- •Chapter 14: Using the Eddy Dissipation and Steady Diffusion Flamelet Combustion Models
- •14.1. Introduction
- •14.2. Prerequisites
- •14.3. Problem Description
- •14.4. Setup and Solution
- •14.4.1. Preparation
- •14.4.2. Mesh
- •14.4.3. Solver Settings
- •14.4.4. Models
- •14.4.5. Boundary Conditions
- •14.4.6. Solution
- •14.4.7. Postprocessing for the Eddy-Dissipation Solution
- •14.5. Steady Diffusion Flamelet Model Setup and Solution
- •14.5.1. Models
- •14.5.2. Boundary Conditions
- •14.5.3. Solution
- •14.5.4. Postprocessing for the Steady Diffusion Flamelet Solution
- •14.6. Summary
- •Chapter 15: Modeling Surface Chemistry
- •15.1. Introduction
- •15.2. Prerequisites
- •15.3. Problem Description
- •15.4. Setup and Solution
- •15.4.1. Preparation
- •15.4.2. Reading and Checking the Mesh
- •15.4.3. Solver and Analysis Type
- •15.4.4. Specifying the Models
- •15.4.5. Defining Materials and Properties
- •15.4.6. Specifying Boundary Conditions
- •15.4.7. Setting the Operating Conditions
- •15.4.8. Simulating Non-Reacting Flow
- •15.4.9. Simulating Reacting Flow
- •15.4.10. Postprocessing the Solution Results
- •15.5. Summary
- •15.6. Further Improvements
- •Chapter 16: Modeling Evaporating Liquid Spray
- •16.1. Introduction
- •16.2. Prerequisites
- •16.3. Problem Description
- •16.4. Setup and Solution
- •16.4.1. Preparation
- •16.4.2. Mesh
- •16.4.3. Solver
- •16.4.4. Models
- •16.4.5. Materials
- •16.4.6. Boundary Conditions
- •16.4.7. Initial Solution Without Droplets
- •16.4.8. Creating a Spray Injection
- •16.4.9. Solution
- •16.4.10. Postprocessing
- •16.5. Summary
- •16.6. Further Improvements
- •Chapter 17: Using the VOF Model
- •17.1. Introduction
- •17.2. Prerequisites
- •17.3. Problem Description
- •17.4. Setup and Solution
- •17.4.1. Preparation
- •17.4.2. Reading and Manipulating the Mesh
- •17.4.3. General Settings
- •17.4.4. Models
- •17.4.5. Materials
- •17.4.6. Phases
- •17.4.7. Operating Conditions
- •17.4.8. User-Defined Function (UDF)
- •17.4.9. Boundary Conditions
- •17.4.10. Solution
- •17.4.11. Postprocessing
- •17.5. Summary
- •17.6. Further Improvements
- •Chapter 18: Modeling Cavitation
- •18.1. Introduction
- •18.2. Prerequisites
- •18.3. Problem Description
- •18.4. Setup and Solution
- •18.4.1. Preparation
- •18.4.2. Reading and Checking the Mesh
- •18.4.3. Solver Settings
- •18.4.4. Models
- •18.4.5. Materials
- •18.4.6. Phases
- •18.4.7. Boundary Conditions
- •18.4.8. Operating Conditions
- •18.4.9. Solution
- •18.4.10. Postprocessing
- •18.5. Summary
- •18.6. Further Improvements
- •Chapter 19: Using the Multiphase Models
- •19.1. Introduction
- •19.2. Prerequisites
- •19.3. Problem Description
- •19.4. Setup and Solution
- •19.4.1. Preparation
- •19.4.2. Mesh
- •19.4.3. Solver Settings
- •19.4.4. Models
- •19.4.5. Materials
- •19.4.6. Phases
- •19.4.7. Cell Zone Conditions
- •19.4.8. Boundary Conditions
- •19.4.9. Solution
- •19.4.10. Postprocessing
- •19.5. Summary
- •Chapter 20: Modeling Solidification
- •20.1. Introduction
- •20.2. Prerequisites
- •20.3. Problem Description
- •20.4. Setup and Solution
- •20.4.1. Preparation
- •20.4.2. Reading and Checking the Mesh
- •20.4.3. Specifying Solver and Analysis Type
- •20.4.4. Specifying the Models
- •20.4.5. Defining Materials
- •20.4.6. Setting the Cell Zone Conditions
- •20.4.7. Setting the Boundary Conditions
- •20.4.8. Solution: Steady Conduction
- •20.5. Summary
- •20.6. Further Improvements
- •Chapter 21: Using the Eulerian Granular Multiphase Model with Heat Transfer
- •21.1. Introduction
- •21.2. Prerequisites
- •21.3. Problem Description
- •21.4. Setup and Solution
- •21.4.1. Preparation
- •21.4.2. Mesh
- •21.4.3. Solver Settings
- •21.4.4. Models
- •21.4.6. Materials
- •21.4.7. Phases
- •21.4.8. Boundary Conditions
- •21.4.9. Solution
- •21.4.10. Postprocessing
- •21.5. Summary
- •21.6. Further Improvements
- •21.7. References
- •22.1. Introduction
- •22.2. Prerequisites
- •22.3. Problem Description
- •22.4. Setup and Solution
- •22.4.1. Preparation
- •22.4.2. Structural Model
- •22.4.3. Materials
- •22.4.4. Cell Zone Conditions
- •22.4.5. Boundary Conditions
- •22.4.6. Solution
- •22.4.7. Postprocessing
- •22.5. Summary
- •23.1. Introduction
- •23.2. Prerequisites
- •23.3. Problem Description
- •23.4. Setup and Solution
- •23.4.1. Preparation
- •23.4.2. Solver and Analysis Type
- •23.4.3. Structural Model
- •23.4.4. Materials
- •23.4.5. Cell Zone Conditions
- •23.4.6. Boundary Conditions
- •23.4.7. Dynamic Mesh Zones
- •23.4.8. Solution Animations
- •23.4.9. Solution
- •23.4.10. Postprocessing
- •23.5. Summary
- •Chapter 24: Using the Adjoint Solver – 2D Laminar Flow Past a Cylinder
- •24.1. Introduction
- •24.2. Prerequisites
- •24.3. Problem Description
- •24.4. Setup and Solution
- •24.4.1. Step 1: Preparation
- •24.4.2. Step 2: Define Observables
- •24.4.3. Step 3: Compute the Drag Sensitivity
- •24.4.4. Step 4: Postprocess and Export Drag Sensitivity
- •24.4.4.1. Boundary Condition Sensitivity
- •24.4.4.2. Momentum Source Sensitivity
- •24.4.4.3. Shape Sensitivity
- •24.4.4.4. Exporting Drag Sensitivity Data
- •24.4.5. Step 5: Compute Lift Sensitivity
- •24.4.6. Step 6: Modify the Shape
- •24.5. Summary
- •25.1. Introduction
- •25.2. Prerequisites
- •25.3. Problem Description
- •25.4. Setup and Solution
- •25.4.1. Preparation
- •25.4.2. Reading and Scaling the Mesh
- •25.4.3. Loading the MSMD battery Add-on
- •25.4.4. NTGK Battery Model Setup
- •25.4.4.1. Specifying Solver and Models
- •25.4.4.2. Defining New Materials for Cell and Tabs
- •25.4.4.3. Defining Cell Zone Conditions
- •25.4.4.4. Defining Boundary Conditions
- •25.4.4.5. Specifying Solution Settings
- •25.4.4.6. Obtaining Solution
- •25.4.5. Postprocessing
- •25.4.6. Simulating the Battery Pulse Discharge Using the ECM Model
- •25.4.7. Using the Reduced Order Method (ROM)
- •25.4.8. External and Internal Short-Circuit Treatment
- •25.4.8.1. Setting up and Solving a Short-Circuit Problem
- •25.4.8.2. Postprocessing
- •25.5. Summary
- •25.6. Appendix
- •25.7. References
- •26.1. Introduction
- •26.2. Prerequisites
- •26.3. Problem Description
- •26.4. Setup and Solution
- •26.4.1. Preparation
- •26.4.2. Reading and Scaling the Mesh
- •26.4.3. Loading the MSMD battery Add-on
- •26.4.4. Battery Model Setup
- •26.4.4.1. Specifying Solver and Models
- •26.4.4.2. Defining New Materials
- •26.4.4.3. Defining Cell Zone Conditions
- •26.4.4.4. Defining Boundary Conditions
- •26.4.4.5. Specifying Solution Settings
- •26.4.4.6. Obtaining Solution
- •26.4.5. Postprocessing
- •26.5. Summary
- •Chapter 27: In-Flight Icing Tutorial Using Fluent Icing
- •27.1. Fluent Airflow on the NACA0012 Airfoil
- •27.2. Flow Solution on the Rough NACA0012 Airfoil
- •27.3. Droplet Impingement on the NACA0012
- •27.3.1. Monodispersed Calculation
- •27.3.2. Langmuir-D Distribution
- •27.3.3. Post-Processing Using Quick-View
- •27.4. Fluent Icing Ice Accretion on the NACA0012
- •27.5. Postprocessing an Ice Accretion Solution Using CFD-Post Macros
- •27.6. Multi-Shot Ice Accretion with Automatic Mesh Displacement
- •27.7. Multi-Shot Ice Accretion with Automatic Mesh Displacement – Postprocessing Using CFD-Post
vk.com/club152685050 | vk.com/id446425943 Steady Diffusion Flamelet Model Setup and Solution
Figure 14.7: Contours of Static Temperature on the Combustor Walls
g.Rotate the contour plot to examine the temperature field of the combusting flow on the canister walls from different angles.
7.Save the case and data files (combustor_edm.cas.gz and combustor_edm.dat.gz).
File → Write → Case & Data...
14.5. Steady Diffusion Flamelet Model Setup and Solution
In the first part of the tutorial, the combustion reaction was modeled using the Eddy Dissipation model. In this part of the tutorial, you will use the Steady Diffusion Flamelet model to simulate a turbulent non-premixed reacting flow. The Steady Diffusion Flamelet model can model local chemical non-equi- librium due to turbulent strain.
In the Steady Diffusion Flamelet model, reactions take place in a thin laminar locally one-dimensional zone, called 'flamelet'. The turbulent flame is represented by an ensemble of such flamelets. Detailed chemical kinetics is used to describe the combustion reaction. The chemistry is assumed to respond rapidly to the turbulent strain, and as the strain relaxes to zero, the chemistry tends to equilibrium. Despite the tendency toward equilibrium, a flamelet solution can often yield more accurate results than an Eddy Dissipation or oneor two-step Finite Rate solution. This is because all the chemistry details
are included, making it possible to capture some of the faster intermediate reactions. To model turbulent mixing, a probability density function (PDF) table is used as a lookup table at run time.
Note
To reduce the solution time for this tutorial, the mesh used is very coarse. This is not a suitable mesh to obtain accurate results, but it is sufficient for demonstration purposes.
To watch a video that demonstrates some steps shown below, go to
• ANSYS Fluent: Describing Non-premixed Combustion using the Steady Flamelet Model
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14.5.1. Models
Specify settings for non-premixed combustion.
Setting Up Physics → Models → Species...
1.In the Model group box, select Non-Premixed Combustion.
2.In the State Reaction group box, select Steady Diffusion Flamelet.
3.Retain the selection of Create Flamelet in the Options group box.
If you are generating a flamelet file yourself, you need to read in the chemical kinetics mechanism and thermodynamic data, which must be in CHEMKIN format.
4.Click Import CHEMKIN Mechanism...
5.In the CHEMKIN Mechanism Import dialog box, in the Kinetics Input File text entry field, enter the following:
path\KINetics\data\grimech30_50spec_mech.inp
where path is the ANSYS Fluent installation directory (for example, C:\Program Files\ANSYS Inc\v193\fluent\fluent19.3.0).
6.Click Import.
Once the reacting data file has been imported, the tab for specifying the fuel and oxidizer compositions, flamelet and PDF table become accessible.
7.In the Boundary tab, specify the fuel (methane) and oxidizer (air) stream compositions in mass fractions.
a.In the Specify Species in group box, make sure that Mass Fraction is selected.
b.Configure the following settings:
Group |
Species |
Mass Fraction |
Fuel |
ch4 |
1.0 |
Oxid |
o2 |
0.233 (default) |
|
n2 |
0.767 (default) |
Tip
Scroll down to see all the species.
Note
All boundary species with a mass or mole fraction of zero will be ignored.
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vk.com/club152685050 | vk.com/id446425943 Steady Diffusion Flamelet Model Setup and Solution
c.In the Temperature group box, retain the default values of 300 K for Fuel and Oxid.
8.In the Control tab, retain the default settings.
9.In the Flamelet tab, retain the default settings and click Calculate Flamelets.
Once the diffusion flamelets are generated, a Question dialog box opens, asking whether you want to save flamelets to a file. Click No.
10.In the Table tab, retain the default settings for the table parameters and click Calculate PDF Table to compute a non-adiabatic probability density function (PDF) table.
11.Click Display PDF Table...
12.In the PDF Table dialog box, retain the selection of Mean Temperature from the Plot Variable drop-down list and all the other default parameters and click Display.
In the graphical display of the 3D look-up table, the Z axis represents the mean temperature of the reacting fluid, and the X and Y axes represent the mean mixture fraction and the scaled variance, respectively.
The maximum and minimum values for mean temperature and the corresponding mean mixture fraction and scale variance are also reported in the console.
The 3D look-up tables are reviewed on a slice-by-slice basis. By default, the slice selected corresponds to the adiabatic enthalpy values. You can also select other slices of constant enthalpy for display.
13.Save the PDF output file (combustor_flamelet.pdf.gz).
File → Write → PDF...
a.Enter combustor_flamelet.pdf.gz for PDF File name.
b.Click OK to write the file.
By default, the file will be saved as formatted (ASCII, or text). To save a binary (unformatted) file, enable the Write Binary Files option in the Select File dialog box.
14.Click Close to close the PDF Table dialog box.
15.Click OK to close the Species Model dialog box.
14.5.2. Boundary Conditions
Specify the boundary condition for the fuel inlet.
Setup → Boundary Conditions → fuelinlet Edit...
1.In the Velocity Inlet dialog box, under the Species tab, enter 1 for Mean Mixture Fraction.
The value of 1 indicates that only pure methane will be entering the fuelinlet boundary.
2.Click OK.
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14.5.3. Solution
1.Edit the output filename for mass-weighted average of co2 at the outlet.
Solution → Monitors → Report Files → co2-out-rfile Edit...
a.Enter co2-out-fl-rfile.out for File Name.
b.Click OK to close the Edit Report File dialog box.
2.Save the case file (combustor_flamelet.cas.gz).
File → Write → Case...
3.Reinitialize the solution.
Solution → Initialization → Initialize
4.In the Run Calculation task page, retain the settings of 5 for Timescale Factor and 500 for Number of Iterations and click Calculate.
Solution → Run Calculation → Advanced...
5.Save the case and data files (combustor_flamelet.cas.gz and combustor_flamelet.dat.gz).
File → Write → Case & Data...
14.5.4. Postprocessing for the Steady Diffusion Flamelet Solution
1.Check the mass flux balance and the total sensible heat flux as described in Postprocessing for the EddyDissipation Solution (p. 489).
2.Display filled contours of mean mixture fraction on the surface plane_xz (Figure 14.8: Contours of Mean Mixture Fraction (p. 499)).
Results → Graphics → Contours → New...
a.Enter mean-mixture-fraction for Contour Name.
b.From the Contours of drop-down lists, select Pdf... and Mean Mixture Fraction.
c.From the Surfaces selection list, deselect all surfaces and select plane_xz.
d.Enable Filled in the Options group box.
e.Clear the Auto Range and Clip to Range options.
f.Enter 0.15 for Max.
g.In the Coloring group box, select Smooth.
h.Click Save/Display.
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Figure 14.8: Contours of Mean Mixture Fraction
3.Display filled contours of CO2 mass fraction in the combustion chamber (Figure 14.9: Contours of CO2 Mass Fraction (p. 499)).
Results → Graphics → Contours → co2-mass-fraction |
Display |
Figure 14.9: Contours of CO2 Mass Fraction
The steady diffusion flamelet simulation yields a significantly different CO2 mass fraction distribution as compared to the eddy dissipation model calculation. The lower CO2 concentration at the base of the flamelet flame is caused by low local temperature in the area, which results in slower combustion. In the eddy dissipation model, chemical kinetics is ignored, and the reaction is controlled by turbulent mixing of the materials. In this case, the CO2 concentration is greater near the base of the flame because the rate of mixing is high in the area (see Figure 14.5: Contours of CO2 Mass Fraction (p. 493)).
4. Display the outlet CO2 concentration profiles for both solutions on a single plot.
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vk.com/club152685050Using the Eddy Dissipation| vkand.com/id446425943Steady Diffusion Flamelet Combustion Models
Results → Plots → File
a.In the File XY Plot dialog box, click the Load... button to open the Select File dialog box.
b.In the Select File dialog box that opens, click once on co2-out-fl-rfile.out and co2-out-rfile.out.
Each of these files will be listed with their folder path in the bottom list to indicate that they have been selected.
Tip
If you select a file by mistake, simply click the file in the bottom list and then click Remove.
c.Click OK to save the files and close the Select File dialog box.
d.In the Plot group box, enter co2-out for Title.
e.From the Curve Information selection list, select co2-out-rfile.out | Iteration | co2-out
f.Enter co2-EDM in the lower-right text-entry box under the Legend Names selection list.
g.Click the Change Legend Entry button.
The item in the Legend Entries list for co2-out-rfile.out | Iteration | co2-out will be changed to co2-EDM. This legend entry will be displayed in the upper-left corner of the XY plot generated in a later step.
h.In a similar manner, change the legend entry for the co2-out-fl-rfile.out | Iteration | co2-out curve to be co2-Flamelet.
i.Click the Axes... button to open the Axes dialog box.
i.From the Axis list, select Y.
ii.Enter 2 for Precision.
iii.Click Apply and close the Axes dialog box.
j.Click the Curves... button to open the Curves dialog box, where you will define a different curve symbol for the CO2 concentration data.
i.Retain 0 for the Curve #.
ii.Select ---- from the Pattern drop-down list.
iii.From the Symbol drop-down list, select the "blank" choice, which is the first item in the Symbol list.
iv.Click Apply.
v.Set Curve # to 1by clicking the up-arrow button.
vi.Modify the settings for Pattern and Symbol in a manner similar to that for the previous curve.
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Release 2019 R1 - © ANSYS,Inc.All rights reserved.- Contains proprietary and confidential information |
500 |
of ANSYS, Inc. and its subsidiaries and affiliates. |