- •TABLE OF CONTENTS
- •Chapter 1 INTRODUCTION
- •The es-ice Environment
- •es-ice Meshing Capabilities
- •Tutorial Structure
- •Trimming Tutorial Overview
- •Required Files
- •Trimming Tutorial files
- •Automatic 2D Tutorial files
- •Wall Temperature Tutorial files
- •Mesh Replacement Tutorial files
- •Multiple Cylinder Tutorial files
- •Closed-Cycle Tutorial files
- •Sector Tutorial files
- •Two-Stroke Tutorial files
- •Mapping Tutorial files
- •ELSA Tutorial files
- •Chapter 2 SURFACE PREPARATION IN STAR-CCM+
- •Importing and Scaling the Geometry
- •Creating Features
- •Defining Surfaces
- •Remeshing and Exporting the Geometry
- •Chapter 3 GEOMETRY IMPORT AND VALVE WORK
- •Importing the Surfaces
- •Modelling the Valves
- •Saving the Model
- •Chapter 4 MESHING WITH THE TRIMMING METHOD
- •Modifying Special Cell Sets in the Geometry
- •Defining Flow Boundaries
- •Creating the 2D Base Template
- •Creating the 3D Template
- •Trimming the 3D Template to the Geometry
- •Improving cell connectivity
- •Assembling the Trimmed Template
- •Running Star Setup
- •Saving the Model
- •Chapter 5 CREATING AND CHECKING THE MESH
- •Chapter 6 STAR SET-UP in es-ice
- •Load Model
- •Analysis Set-up
- •Valve Lifts
- •Assembly
- •Combustion
- •Initialization
- •Cylinder
- •Port 1 and Port 2
- •Boundary Conditions
- •Cylinder
- •Port and Valve 1
- •Port and Valve 2
- •Global settings
- •Post Set-up
- •Cylinder
- •Port 1 and Port 2
- •Global settings
- •Time Step Control
- •Write Data
- •Saving the Model
- •Chapter 7 STAR SET-UP in pro-STAR
- •Using the es-ice Panel
- •Setting Solution and Output Controls
- •File Writing
- •Chapter 8 RUNNING THE STAR SOLVER
- •Running in Serial Mode
- •Running in Parallel Mode
- •Running in Parallel on Multiple Nodes
- •Running in Batch
- •Restarting the Analysis
- •Chapter 9 POST-PROCESSING: GENERAL TECHNIQUES
- •Creating Plots with the es-ice Graph Tool
- •Calculating Apparent Heat Release
- •Plotting an Indicator Diagram
- •Calculating Global Engine Quantities
- •Creating a Velocity Vector Display
- •Creating an Animation of Fuel Concentration
- •Creating an Animation of Temperature Isosurfaces
- •Chapter 10 USING THE AUTOMATIC 2D TEMPLATE
- •Importing the Geometry Surface
- •Defining Special Cell Sets in the Geometry
- •Modelling the Valves
- •Creating the Automatic 2D Template
- •Refining the 2D Template Around the Injector
- •Adding Features to the Automatic 2D Template
- •Using Detailed Automatic 2D Template Parameters
- •Saving the es-ice Model File
- •Chapter 11 MULTIPLE-CYCLE ANALYSIS
- •Setting Up Multiple Cycles in es-ice
- •Setting Up Multiple Cycles in pro-STAR
- •Chapter 12 HEAT TRANSFER ANALYSIS
- •Resuming the es-ice Model File
- •Mapping Wall Temperature
- •Exporting Wall Heat Transfer Data
- •Saving the es-ice Model File
- •Cycle-averaging Wall Heat Transfer Data
- •Post-processing Wall Heat Transfer Data in pro-STAR
- •Plotting average wall boundary temperatures
- •Plotting average heat transfer coefficients
- •Plotting average near-wall gas temperature at Y-plus=100
- •Mapping Heat Transfer Data to an Abaqus Model via STAR-CCM+
- •Chapter 13 MESH REPLACEMENT
- •Preparing the File Structure
- •Rebuilding the Dense Mesh
- •Creating Ahead Files for the Dense Mesh
- •Defining Mesh Replacements
- •Setting Up Mesh Replacement in pro-STAR
- •Setting up the coarse model
- •Setting up the dense model
- •Chapter 14 MULTIPLE CYLINDERS
- •Resuming the es-ice Model File
- •Making, Cutting and Assembling the Template
- •Setting Up Multiple Cylinders
- •Checking the Computational Mesh
- •STAR Set-Up in es-ice
- •Analysis set-up
- •Assembly
- •Combustion
- •Initialization
- •Boundary Conditions
- •Post Setup
- •Time Step Control
- •Write Data
- •Saving the es-ice Model File
- •Importing the Geometry
- •Generating the Closed-Cycle Polyhedral Mesh
- •Assigning shells to geometry cell sets
- •Specifying General, Events and Cylinder parameters
- •Creating a spray-optimised mesh zone
- •Importing a user intermediate surface
- •Checking the spray-optimised zone
- •Creating the closed-cycle polyhedral mesh
- •Running Star Setup
- •Creating and checking the computational mesh
- •Saving the Model File
- •Chapter 16 DIESEL ENGINE: SECTOR MODEL
- •Importing the Bowl Geometry
- •Defining the Bowl Shape
- •Defining the Fuel Injector
- •Creating the 2D Template
- •Creating the Sector Mesh
- •Creating and Checking the Mesh
- •Saving the Model
- •Chapter 17 DIESEL ENGINE: STAR SET-UP IN es-ice and pro-STAR
- •STAR Set-up in es-ice
- •Load model
- •Analysis setup
- •Assembly
- •Combustion
- •Initialization
- •Boundary conditions
- •Post setup
- •Time step control
- •Write data
- •Saving the Model File
- •STAR Set-up in pro-STAR
- •Using the es-ice Panel
- •Selecting Lagrangian and Liquid Film Modelling
- •Setting up the Fuel Injection Model
- •Setting up the Liquid Film Model
- •Setting up Analysis Controls
- •Writing the Geometry and Problem Files and Saving the Model
- •Chapter 18 DIESEL ENGINE: POST-PROCESSING
- •Creating a Scatter Plot
- •Creating a Spray Droplet Animation
- •Chapter 19 TWO-STROKE ENGINES
- •Importing the Geometry
- •Meshing with the Trimming Method
- •Assigning shells to geometry cell sets
- •Creating the 2D template
- •Creating the 3D template
- •Trimming the 3D template to the geometry
- •Assembling the trimmed template
- •Running Star Setup
- •Checking the mesh
- •STAR Set-up in es-ice
- •Analysis setup
- •Assembly
- •Combustion
- •Initialization
- •Boundary conditions
- •Post setup
- •Time step control
- •Write data
- •Saving the es-ice Model File
- •Chapter 20 MESHING WITH THE MAPPING METHOD
- •Creating the Stub Surface in the Geometry
- •Creating the 2D Base Template
- •Creating the 3D Template
- •General Notes About Edges and Splines
- •Creating Edges and Splines Near the Valve Seat
- •Creating the Remaining Edges and Splines
- •Creating Patches
- •The Mapping Process
- •Chapter 21 IMPROVING THE MAPPED MESH QUALITY
- •Creating Plastered Cells
- •Chapter 22 PISTON MODELING
- •Meshing the Piston with the Shape Piston Method
- •Chapter 23 ELSA SPRAY MODELLING
- •Importing the Bowl Geometry
- •Defining the Bowl Shape
- •Setting the Events and Cylinder Parameters
- •Creating the Spray Zone
- •Creating the Sector Mesh
- •STAR Set-up in es-ice
- •Load model
- •Analysis setup
- •Assembly
- •Combustion
- •Initialization
- •Boundary Conditions
- •Time step control
- •Write data
- •Saving the Model File
- •STAR Set-up in pro-STAR
- •Using the es-ice panel
- •Activating the Lagrangian model
- •Defining the ELSA scalars
- •Setting up the Lagrangian droplets
- •Defining boundary regions and boundary conditions
- •Setting up analysis controls
- •Adding extended data for the ELSA model
- •Writing the Geometry and Problem Files and Saving the Model
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Boundary Conditions
The Boundary conditions view sets the boundary type and boundary conditions for the cylinder, intake and exhaust ports, and intake and exhaust valves. As with initial conditions, boundaries for each domain are defined separately. For more details on Boundary Conditions see Chapter 8, “Boundary Conditions” in the User Guide.
Cylinder
The relevant boundaries for the Cylinder are Piston crown, Cylinder wall, Combustion dome and Symmetry plane. For each boundary, you can specify a Fixed or Mapped temperature or an Adiabatic condition. In addition, you can specify different temperatures at different heights of the Cylinder wall by using the Zone boundary type.
In this tutorial, you will specify Fixed temperatures at all cylinder boundaries.
•Click Boundary conditions on the left of the Star Controls panel (see Figure 6-14)
•Check that Cylinder is selected from the domain drop-down menu
•Set Combustion dome regions to Fixed from the drop-down menu
•Set Temperature to 450 K
•Set Piston crown regions to Fixed from the drop-down menu
•Set Temperature to 550 K
•Set Cylinder wall regions to Fixed from the drop-down menu
•Set Temperature to 500 K
In addition, set up an Extra region to define the spark plug.
•Select the Extra region toggle button
•Set Name to Spark Plug
•Click the Define button next to the Regions box
•In the Boundary Tool, click Display all to show all Cylinder surface shells
•Click Keep picked and pick the patches that define the spark plug in the Controls Workspace window, as shown in Figure 6-13:
Figure 6-13 Spark Plug patches
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•Press q to exit from the pick mode
•In the Boundary Tool, click Define to define the generated patches as the
Extra region
•Select Fixed wall from the drop-down menu and set Temperature to 600 K
Figure 6-14 Star Controls panel: Boundary conditions view
Port and Valve 1
For Port and Valve 1, the relevant boundaries are Valve stem, Valve face and Port wall. For each boundary, you can specify a Fixed or Mapped temperature or an Adiabatic condition. In addition, you can specify an Extra region to define the intake flow boundary.
In this tutorial, you will specify Adiabatic conditions for all Port and Valve 1 boundaries.
•Select Port and Valve 1 from the domain drop-down menu
•Ensure that the Valve stem regions, Valve face regions and Port wall regions are set to Adiabatic
As the intake and exhaust manifolds are external meshes added during the Assembly process, es-ice assumes that all their boundaries are solid walls. Note that the Extra regions > Regions box is empty, which means that flow boundary conditions have not been assigned yet.
To define the intake flow boundary shells:
•Under Extra regions, set Name to Intake Flow Boundary
•Click the Define button next to the Regions box
•In the Boundary Tool, click Display all to show all Port 1 surface shells, as shown in Figure 6-15
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•Click Keep picked and pick the Intake Flow Boundary patch in the Controls Workspace window, as shown in Figure 6-15
Intake Flow Boundary
Figure 6-15 Redefining wall boundary condition for Port 1
•Press q to exit from the pick mode
•In the Boundary Tool, click Define to define the generated patch as the
Extra region
•Click Close tool to close the Boundary Tool panel
In this example, a value of 132 appears in the Regions box. This value represents the region ID for the intake boundary faces. Alternatively, if you know the region ID, you can manually enter its value into the box. In this case, you will also need to ensure that region ID 132 is removed from Port wall regions to avoid multiple boundary assignments. Note that if you use the Boundary Tool, es-ice automatically prevents multiple assignments.
To set the Intake Flow Boundary conditions shown in Figure 6-16:
•Set Absolute pressure to Environmental from the drop-down menu
•For Absolute pressure and Temperature values, follow similar steps to those for the Initialization process to import relevant data from the intake-3600.dat image file
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Figure 6-16 Star Controls panel: Boundary conditions view of Port 1
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