FineTurbo_User_manual User Manual FINETurbo

2013-12-19

• CHAPTER 1: Getting Started
  • 1-1 Overview
  • 1-2 Introduction
    • 1-2.1 Components
    • 1-2.2 Multi-Tasking
    • 1-2.3 Project Management
  • 1-3 How To Use This Manual
    • 1-3.1 Outline
    • 1-3.2 Conventions
  • 1-4 First Time Use
    • 1-4.1 Basic Installation
    • 1-4.2 Expert Graphics Options
      • a) Graphics Driver
      • b) Background Color
  • 1-5 How to start the FINE™/Turbo Interface
  • 1-6 Required Licenses
    • 1-6.1 Standard FINE™/Turbo License
    • 1-6.2 Additional Licenses
• CHAPTER 2: Graphical User Interface
  • 2-1 Overview
  • 2-2 Project Selection
    • 2-2.1 Create New Project
    • 2-2.2 Open Existing Project
    • 2-2.3 Grid Units & Project Configuration
  • 2-3 Main Menu Bar
    • 2-3.1 File Menu
      • 2-3.1.1 New Project
      • 2-3.1.2 Open Project
        • a) Use File/Open Menu
        • b) Select File From the List of Files in File Menu.
      • 2-3.1.3 Save Project
      • 2-3.1.4 Save As Project
      • 2-3.1.5 Save Run Files
      • 2-3.1.6 Preferences
        • a) Project Units
        • b) Global Layout
        • c) Solver Preferences
      • 2-3.1.7 Quit
    • 2-3.2 Mesh Menu
      • 2-3.2.1 View On/Off
      • 2-3.2.2 Repetition
      • 2-3.2.3 Tearoff graphics
      • 2-3.2.4 Unload
      • 2-3.2.5 Properties
    • 2-3.3 Solver Menu
      • 2-3.3.1 Start Flow Solver
      • 2-3.3.2 Save
      • 2-3.3.3 Stop Flow Solver
    • 2-3.4 Modules Menu
  • 2-4 Icon Bar
    • 2-4.1 File Buttons
    • 2-4.2 Grid Selection Bar
    • 2-4.3 Solver Buttons
    • 2-4.4 Module Buttons
    • 2-4.5 User Mode
  • 2-5 Computation Management
  • 2-6 Graphical Area Management
    • 2-6.1 Configuration Management
    • 2-6.2 Parameters Management
    • 2-6.3 View Area
    • 2-6.4 Mesh Information
    • 2-6.5 Parameters Area
    • 2-6.6 Graphics Area
    • 2-6.7 Viewing Buttons
      • 2-6.7.1 X, Y, and Z Projection Buttons
      • 2-6.7.2 Coordinate Axes
      • 2-6.7.3 Scrolling
      • 2-6.7.4 3D Viewing Button
      • 2-6.7.5 Rotate About X, Y or Z Axis
      • 2-6.7.6 Zoom In/Out
      • 2-6.7.7 Region Zoom
      • 2-6.7.8 Fit Button
      • 2-6.7.9 Original Button
      • 2-6.7.10 Cutting Plane
  • 2-7 Profile Management
• CHAPTER 3: Fluid Model
  • 3-1 Overview
  • 3-2 The Fluid Model in the FINE™/Turbo GUI
    • 3-2.1 Properties of Fluid Used in the Project
    • 3-2.2 List of Fluids
    • 3-2.3 Add Fluid
      • 3-2.3.1 Definition of a Perfect Gas
      • 3-2.3.2 Definition of a Real Gas
      • 3-2.3.3 Definition of a Liquid
      • 3-2.3.4 Definition of a Condensable Fluid
        • a) Selection of the Viscosity, Conductivity, and Specific Heat
      • 3-2.3.5 Formula Editor
      • 3-2.3.6 Profile Manager
    • 3-2.4 Delete Fluid from List
    • 3-2.5 Edit Fluid
    • 3-2.6 Show Fluid Properties
    • 3-2.7 Filters
    • 3-2.8 Import Fluid Database
    • 3-2.9 Expert Parameters
• CHAPTER 4: Flow Model
  • 4-1 Overview
  • 4-2 Mathematical Model
    • 4-2.1 Euler
    • 4-2.2 Laminar Navier-Stokes
    • 4-2.3 Turbulent Navier-Stokes
      • a) Boundary Condition
      • b) Initial Condition
    • 4-2.4 Expert Parameters for Turbulence Modelling
      • 4-2.4.1 Interfaced Expert Parameters
      • 4-2.4.2 Non-interfaced Expert Parameters
    • 4-2.5 Best Practice for Turbulence Modelling
      • 4-2.5.1 Introduction to Turbulence
      • 4-2.5.2 First Step: Choosing a Turbulence Model.
      • 4-2.5.3 Second Step: Generating an Appropriate Grid.
        • a) Cell Size
        • b) Things to Look Out For
        • c) General Advice
        • d) Verification of y1+
      • 4-2.5.4 Defining Initial & Boundary Conditions
        • a) Spalart-Allmaras Model
        • b) k-e, k-w, EARSM and v2-f Models
      • 4-2.5.5 Setting Expert Parameters to Procure Convergence
        • a) Cut-off (Clipping) of Minimum k Value
        • b) Minimizing Artificial Dissipation in the Boundary Layer
        • c) Wall Function for the k-e Turbulence Model
        • d) Full Multigrid k-e / Baldwin-Lomax & v2-f / Baldwin-Lomax Switch
        • e) Cut-off (clipping) of Maximum Turbulence Production/Destruction Value
        • f) Cut-off (clipping) of Maximum Turbulent Viscosity Ratio (mt /m)
    • 4-2.6 Laminar-Transition Model
      • 4-2.6.1 Introduction
      • 4-2.6.2 How to model transition on non-turbomachinery cases
    • 4-2.7 Gravity Forces
    • 4-2.8 Low Speed Flow (Preconditioning)
  • 4-3 Characteristic & Reference Values
    • 4-3.1 Reynolds Number Related Information
    • 4-3.2 Reference Values
• CHAPTER 5: Boundary Conditions
  • 5-1 Overview
  • 5-2 Boundary Conditions in the FINE™/Turbo GUI
    • 5-2.1 Inlet Condition
      • 5-2.1.1 Available Types
      • 5-2.1.2 Coupling Temperature with Outlet
      • 5-2.1.3 Imposing Variables as an Interpolation Profile
    • 5-2.2 Outlet Condition
      • 5-2.2.1 Pressure Imposed
      • 5-2.2.2 Mass Flow Imposed
      • 5-2.2.3 Averaged Mach Number
      • 5-2.2.4 Characteristic Imposed
      • 5-2.2.5 From Rotor/Stator
    • 5-2.3 Periodic Condition
    • 5-2.4 Solid Wall Boundary Condition
      • 5-2.4.1 Cylindrical Boundary Condition
        • a) Area Defined Rotation Speed
        • b) Thermal Condition
      • 5-2.4.2 Cartesian Boundary Conditions
      • 5-2.4.3 Force and Torque
      • 5-2.4.4 Properties of Solid for Turbulence
    • 5-2.5 External Condition (Far-field)
  • 5-3 Expert Parameters
    • 5-3.1 Imposing Velocity Angles of Relative Flow
    • 5-3.2 Inlet Mass Flow Boundary Condition
    • 5-3.3 Outlet Mass Flow Boundary Condition
    • 5-3.4 Outlet Averaged Mach Number Boundary Condition
    • 5-3.5 Control of backflows
    • 5-3.6 Torque and Force
    • 5-3.7 Euler or Navier-Stokes Wall for Viscous Flow
    • 5-3.8 Pressure Condition at Solid Wall
  • 5-4 Best Practice for Imposing Boundary Conditions
    • 5-4.1 Compressible Flows
    • 5-4.2 Incompressible or Low Speed Flow
    • 5-4.3 Special Parameters (for Turbomachinery)
• CHAPTER 6: Numerical Scheme
  • 6-1 Overview
  • 6-2 Numerical Model
    • 6-2.1 Introduction
    • 6-2.2 Numerical Model in the FINE™/Turbo GUI
      • 6-2.2.1 CFL Number
      • 6-2.2.2 CPU Booster
      • 6-2.2.3 Multigrid Parameters
      • 6-2.2.4 Preconditioning Parameters
        • a) Hakimi Preconditioning
        • b) Merkle Preconditioning
    • 6-2.3 Expert Parameters
      • 6-2.3.1 Interfaced Expert Parameters
        • a) Multigrid Strategy
        • b) Spatial Discretization
        • c) Temporal Discretization
      • 6-2.3.2 Non-interfaced Expert Parameters
        • a) Multigrid
        • b) Spatial Discretization
        • c) Central Discretization
        • d) Upwind Discretization
        • e) Time Discretization
  • 6-3 Time Configuration
    • 6-3.1 Interface for Unsteady Computation
      • a) Rotating Machinery
      • b) Time Dependent Boundary Conditions
      • c) Phase Lagged
      • d) Control Variables
      • e) Second Order Accurate in Time
    • 6-3.2 Expert Parameters for Unsteady Computations
      • 6-3.2.1 Numerical Model in Expert User Mode
      • 6-3.2.2 List of Non-interfaced Expert Parameters
    • 6-3.3 Best Practice on Time Accurate Computations
      • 6-3.3.1 General Project Set-up for Time Accurate Computations
      • 6-3.3.2 Time Dependent Boundary Conditions
      • 6-3.3.3 Initialisation Procedure
        • a) Start From Steady Solution
        • b) Start From Time Accurate Solution
        • c) Steady State Initialisation in Unsteady Computation
      • 6-3.3.4 Physical Time Step
      • 6-3.3.5 Amount of Output
      • 6-3.3.6 Time Averaged Solution
• CHAPTER 7: Physical Models
  • 7-1 Overview
  • 7-2 Fluid-Particle Interaction
    • 7-2.1 Introduction
      • 7-2.1.1 Lagrangian Approach
      • 7-2.1.2 Algorithm
    • 7-2.2 Fluid-Particle Interaction in the FINE™/Turbo GUI
      • 7-2.2.1 Parameters
      • 7-2.2.2 Boundary Conditions
        • a) Inlet Boundary
        • b) Solid Wall Boundary
      • 7-2.2.3 Outputs
    • 7-2.3 Specific Output
      • 7-2.3.1 Field Quantities (’.cgns’)
      • 7-2.3.2 Particles Traces (’.tr’)
      • 7-2.3.3 Summary File (’.tr.sum’)
    • 7-2.4 Expert Parameters
  • 7-3 Fluid-Structure
    • 7-3.1 Thermal
      • 7-3.1.1 Conjugate Heat Transfer
        • a) Introduction
        • b) Conjugate Heat Transfer in the FINE™/Turbo GUI
      • 7-3.1.2 MpCCI Coupling
        • a) Introduction
        • b) Thermal Coupling with MpCCI
        • c) Expert Parameters
    • 7-3.2 Mechanical
      • 7-3.2.1 Rigid Motion
        • a) Introduction
        • b) Rigid Motion in the FINE™/Turbo GUI
        • c) Adaptive Wall
        • d) Expert Parameters
      • 7-3.2.2 MpCCI Coupling
        • a) Introduction
        • b) Mechanical Coupling with MpCCI
        • c) Expert Parameters
      • 7-3.2.3 Modal Coupling
        • a) Introduction
        • b) The Modal Coupling in the FINE™/Turbo GUI
      • 7-3.2.4 Mesh deformation methods
        • a) Laplacian Smoothing
        • b) Radial Basis Functions
        • c) Expert Parameters
  • 7-4 Passive Tracers
    • 7-4.1 Boundary Conditions
    • 7-4.2 Initial Solution
    • 7-4.3 Outputs
  • 7-5 Porous Media Model
    • 7-5.1 Porous Media Model in the FINE™/Turbo GUI
    • 7-5.2 Experts Parameters
  • 7-6 Cavitation Model
    • 7-6.1 Cavitation Model in the FINE™/Turbo GUI
    • 7-6.2 Experts Parameters
• CHAPTER 8: Dedicated Turbomachinery Models
  • 8-1 Overview
  • 8-2 Rotating Blocks
  • 8-3 Rotor/Stator Interaction
    • 8-3.1 Rotor/Stator Interfaces in the FINE™/Turbo GUI
    • 8-3.2 How to Set-up a Simulation with Rotor/Stator Interfaces?
      • 8-3.2.1 Mixing Plane Approach
        • a) Geometrical Constraints
        • b) Mesh Constraints
        • c) FINE™/Turbo Settings
        • d) Illustrative Example
        • e) Expert Parameters
      • 8-3.2.2 Frozen Rotor
        • a) Mesh Constraints
        • b) FINE™/Turbo Settings
        • c) Illustrative Example
      • 8-3.2.3 Domain Scaling Method
        • a) Mesh Constraints
        • b) FINE™/Turbo Settings
        • c) Illustrative Example
        • d) Expert Parameters
      • 8-3.2.4 Phase Lagged Method
        • a) Mesh Constraints
        • b) FINE™/Turbo Settings
        • c) Output
        • d) Expert Parameters
      • 8-3.2.5 Harmonic Method
        • a) Mesh Constraints
        • b) FINE™/Turbo Settings
        • c) Illustrative Example
      • 8-3.2.6 Control the flux of Eddy viscosity
  • 8-4 Harmonic Method
    • 8-4.1 Introduction
    • 8-4.2 Interface & Best Practice for Harmonic Computations
      • 8-4.2.1 Initial Solution
      • 8-4.2.2 Boundary conditions
      • 8-4.2.3 Outputs
        • a) Harmonic variables output
        • b) Plot3D output
        • c) Reconstruction in Time
      • 8-4.2.4 Control Variables
      • 8-4.2.5 Troubleshooting in Rotor/Stator Interface
    • 8-4.3 Expert Parameters
      • 8-4.3.1 Expert Parameters for the Flow Solver
      • 8-4.3.2 Expert Parameters for Reconstruction in Time
  • 8-5 Clocking
    • 8-5.1 Introduction
    • 8-5.2 Interface Settings
      • 8-5.2.1 Reconstruction in Time
  • 8-6 Cooling/Bleed
    • 8-6.1 Introduction
    • 8-6.2 Cooling/Bleed Model in the FINE™/Turbo GUI
      • 8-6.2.1 Injector Sector Wizard
        • a) Injection Sector Name
        • b) Injection Sector Role
        • c) Injection Sector Geometry
        • d) Injection Sector Positioning
        • e) Injection Sector Geometry/Positioning Parameters
        • f) Flow Parameters
      • 8-6.2.2 Preview/Preview&Check Injector Sector
      • 8-6.2.3 Multiple edit and copy of the injectors
        • a) Multiple select and edit
        • b) Copy and Paste
    • 8-6.3 Expert Parameters
    • 8-6.4 Cooling/Bleed Data File: ’.cooling-holes’
      • 8-6.4.1 Injection file format
        • a) The header
        • b) Multiple injector format
        • c) Injector name
        • d) Injection geometry Type
        • e) Injection physical Type
        • f) Locations patches
        • g) Location patch index
        • h) Anchor point location
        • i) Cooling direction (not for Bleed)
        • j) Anchor point location and cooling direction (for points type only)
        • k) Mass flow
        • l) Number of holes on a line
        • m) Cooling/Bleed size
        • n) Physical Properties
      • 8-6.4.2 Examples
  • 8-7 Rigid Motion
  • 8-8 Aeroacoustics
    • 8-8.1 Aeroacoustics in the FINE™/Turbo GUI
      • 8-8.1.1 The global parameters
      • 8-8.1.2 The observer definition
      • 8-8.1.3 Launch Solver and Post-processing
    • 8-8.2 Expert Parameters for Aeroacoustics
  • 8-9 Laminar-Transition Model
    • 8-9.1 Introduction
    • 8-9.2 Transition Model in the FINE™/Turbo GUI
    • 8-9.3 Expert Parameters
  • 8-10 Performance Curve
    • 8-10.1 Introduction
    • 8-10.2 Performance Curve in the FINE™/Turbo GUI
      • 8-10.2.1 Create and Edit Performance Curve
      • 8-10.2.2 Launch the flow Solver
      • 8-10.2.3 Output
  • 8-11 SubProject Management
    • 8-11.1 Introduction
    • 8-11.2 Set-up of SubProjects in FINE™/Turbo
      • 8-11.2.1 Grid Requirements
      • 8-11.2.2 Create SubProjects
      • 8-11.2.3 Modify & Merge SubProjects
        • a) Modify Geometry
        • b) Merge SubProjects
      • 8-11.2.4 File Structure
• CHAPTER 9: Initial Solution
  • 9-1 Overview
  • 9-2 Block Dependent Initial Solution
    • 9-2.1 How to Define a Block Dependent Initial Solution
    • 9-2.2 Examples for the use of Block Dependent Initial Solution
  • 9-3 Initial Solution Defined by Constant Values
  • 9-4 Initial Solution from File
    • 9-4.1 General Restart Procedure
    • 9-4.2 Restart in Unsteady Computations
    • 9-4.3 Expert Parameters for an Initial Solution from File
  • 9-5 Initial Solution for Turbomachinery
    • 9-5.1 Methodology
    • 9-5.2 Grouping & Parameters
    • 9-5.3 Expert Parameters
  • 9-6 Throughflow-oriented Initial Solution
    • 9-6.1 File Format
    • 9-6.1.1 Solution Definition
    • 9-6.1.2 Hub Definition
    • 9-6.1.3 Shroud Definition
• CHAPTER 10: Output
  • 10-1 Overview
  • 10-2 Output in FINE™/Turbo
    • 10-2.1 Computed Variables
      • 10-2.1.1 Thermodynamics
      • 10-2.1.2 Velocities
      • 10-2.1.3 Vorticities
      • 10-2.1.4 Residuals
      • 10-2.1.5 Solid Data
      • 10-2.1.6 Turbulence
      • 10-2.1.7 Harmonic
      • 10-2.1.8 Deformation
    • 10-2.2 Surface Averaged Variables
    • 10-2.3 Azimuthal Averaged Variables
    • 10-2.4 Template manager
    • 10-2.5 ANSYS
      • 10-2.5.1 ANSYS Pre-Processing
      • 10-2.5.2 Global Parameters
      • 10-2.5.3 Surface Selection
      • 10-2.5.4 Import Results in ANSYS
    • 10-2.6 Global Performance Output
      • 10-2.6.1 Flow Angle
      • 10-2.6.2 Global Performance
        • a) Global Performance Output for Incompressible Fluid
        • b) Global Performance Output for Compressible Fluid
      • 10-2.6.3 Solid Boundary Characteristics
    • 10-2.7 Plot3D Formatted Output
  • 10-3 Expert Parameters
    • 10-3.1 Azimuthal Averaged Variables
    • 10-3.2 Global Performance Output
    • 10-3.3 Solid Data Output
• CHAPTER 11: Task Manager
  • 11-1 Overview
  • 11-2 Getting Started
    • 11-2.1 PVM Daemons
      • 11-2.1.1 What PVM Daemons Do
      • 11-2.1.2 Limitation under Windows
    • 11-2.2 Multiple FINE™/Turbo Sessions
    • 11-2.3 Machine Connections
    • 11-2.4 Remote Copy Features on UNIX/LINUX
    • 11-2.5 Remote Copy Features on Windows
  • 11-3 The Task Manager Interface
    • 11-3.1 Hosts Definition
      • 11-3.1.1 Add Host
      • 11-3.1.2 Remove Host
      • 11-3.1.3 Shutdown
    • 11-3.2 Tasks Definition
      • 11-3.2.1 Task List
      • 11-3.2.2 Task Definition
      • 11-3.2.3 Subtask Arguments
        • a) Definition of Input & Output
        • b) Simultaneous or Sequential Mode
        • c) Remote Copy
        • d) Launching Mode
        • e) Message Window
  • 11-4 Parallel Computations
    • 11-4.1 Introduction
      • 11-4.1.1 Parallel Computation
      • 11-4.1.2 Parallel Partitioned Computation
    • 11-4.2 Management of Inter-Block Communication
    • 11-4.3 How to Run a Parallel Computation
    • 11-4.4 Use an External OpenMPI Library on LINUX/UNIX
    • 11-4.5 Troubleshooting
    • 11-4.6 Limitations
  • 11-5 Task Management in Batch
    • 11-5.1 Launch IGG™ in Batch
      • 11-5.1.1 How to Launch IGG™ on UNIX
      • 11-5.1.2 How to Launch IGG™ on Windows
    • 11-5.2 Launch AutoGrid™ in Batch
      • 11-5.2.1 How to Launch AutoGrid™ 4 on UNIX
      • 11-5.2.2 How to Launch AutoGrid™ on UNIX
      • 11-5.2.3 How to Launch AutoGrid™ 4 on Windows
      • 11-5.2.4 How to Launch AutoGrid™ on Windows
    • 11-5.3 Launch FINE™ in Batch
      • 11-5.3.1 How to Launch FINE™ on UNIX
        • a) Create a ".run" file
        • b) Set-up a parallel computation using MPI
        • c) Set-up a parallel computation using SGE
        • d) Set-up a parallel computation using PBS
        • e) Set-up a parallel computation using LSF
        • f) Set-up a parallel partitioned computation using MPI
        • g) Set-up a parallel partitioned computation using SGE
        • h) Set-up a parallel partitioned computation using PBS
        • i) Set-up a parallel partitioned computation using LSF
      • 11-5.3.2 How to Launch FINE™ on Windows
        • a) Set-up a sequential computation
    • 11-5.4 Launch the flow solver in Sequential Mode in Batch
      • 11-5.4.1 How to Launch the flow solver in Sequential mode on UNIX
      • 11-5.4.2 How to Launch the flow solver in Sequential under Windows
    • 11-5.5 Launch the flow solver in Parallel Mode in Batch
      • 11-5.5.1 How to Launch the flow solver in Parallel using MPI on UNIX
      • 11-5.5.2 How to Launch the flow solver in Parallel using MPI on Windows
      • 11-5.5.3 How to Launch the flow solver in Parallel using SGE on UNIX
      • 11-5.5.4 How to Launch the flow solver in Parallel using PBS on UNIX
      • 11-5.5.5 How to Launch the flow solver in Parallel using LSF on UNIX
    • 11-5.6 Launch CFView™ in Batch
      • 11-5.6.1 How to Launch CFView™ on UNIX
      • 11-5.6.2 How to Launch CFView™ on Windows
      • 11-5.6.3 Command Line Arguments
  • 11-6 Limitations
• CHAPTER 12: Computation Steering & Monitoring
  • 12-1 Overview
  • 12-2 Control Variables
    • 12-2.1 Control Variables in the FINE™/Turbo GUI
    • 12-2.2 Expert Parameters
  • 12-3 Convergence History
    • 12-3.1 Convergence History in the FINE™/Turbo GUI
      • 12-3.1.1 Steering Files Selection & Curves Export
      • 12-3.1.2 Available Quantities Selection
      • 12-3.1.3 New Quantity Parameters Definition
      • 12-3.1.4 Quantity Selection Area
      • 12-3.1.5 Definition of Global Residual
      • 12-3.1.6 The Graphics View
    • 12-3.2 Expert Parameters
  • 12-4 MonitorTurbo
    • 12-4.1 Introduction
    • 12-4.2 The MonitorTurbo GUI
      • 12-4.2.1 The Residual File Box
      • 12-4.2.2 Quantities to Display
        • a) Residuals
        • b) Global Quantities
        • c) Harmonic Quantities
        • d) Display Options
        • e) Zooming Option
  • 12-5 Best Practice for Computation Monitoring
    • 12-5.1 Introduction
    • 12-5.2 Convergence History
    • 12-5.3 MonitorTurbo
    • 12-5.4 Analysis of Residuals
• APPENDIX A: File Formats
  • A-1 Overview
  • A-2 Files Produced by IGG™
    • A-2.1 The Identification File: ’project.igg’
    • A-2.2 The Binary File: ’project.cgns’
    • A-2.3 The Geometry File: ’project.geom’
    • A-2.4 The Boundary Condition File: ’project.bcs’
    • A-2.5 The Configuration File: ’project.config’
  • A-3 Files Produced by the FINE™/Turbo GUI
    • A-3.1 The Project File: ’project.iec’
      • a) File Header
      • b) The Computation Block
    • A-3.2 The Computation File: ’project_computation.run’
  • A-4 Files Produced by the FINE™/Turbo solver
    • A-4.1 The Binary Solution File: ’project_computation.cgns’
      • A-4.1.1 Fluid_solution
      • A-4.1.2 Project3d
      • A-4.1.3 Project3d_solid_data
      • A-4.1.4 Project2d_meridional
      • A-4.1.5 The Size of the ".cgns" File
    • A-4.2 The Global Solution File: ’project_computation.mf’
    • A-4.3 The Global Solution File: ’project_computation.xmf’
    • A-4.4 The Residual File: ’project_computation.res’
    • A-4.5 The LOG File: ’project_computation.log’
    • A-4.6 The STD file: ’project_computation.std’
    • A-4.7 The Wall File: ’project_computation.wall’
    • A-4.8 The AQSI File: ’project_computation.aqsi’
    • A-4.9 The ADF File: ’project.adf’
    • A-4.10 The Plot3D Files
    • A-4.11 The Meridional File: ’project_computation.me.cfv’
  • A-5 Files Used as Data Profile
    • A-5.1 Boundary Conditions Data
    • A-5.2 Fluid Properties
    • A-5.3 Solid Properties
  • A-6 Resource Files
    • A-6.1 Boundary Conditions Resource File: ’euranus_bc.def’
    • A-6.2 Fluids Database File: ’euranus.flb’
    • A-6.3 Units Systems Resource File: ’euranus.uni’
• APPENDIX B: List of Expert Parameters
  • B-1 Overview
  • B-2 List of Integer Expert Parameters
  • B-3 List of Float Expert Parameters
• APPENDIX C: Characteristics of Thermodynamic Tables
  • C-1 Overview
  • C-2 Main Characteristics for Water (Steam)
  • C-3 Main Characteristics for R134a
• APPENDIX D: TabGen
  • D-1 Overview
  • D-2 Graphical User Interface
    • D-2.1 Start Program
      • D-2.1.1 Create New Mixture
      • D-2.1.2 Open Mixture
      • D-2.1.3 Exit
    • D-2.2 Main Window
      • D-2.2.1 Edit Table
        • a) Edit 1D Saturation Table
        • b) Edit PT Table
        • c) Edit 2D Tables
      • D-2.2.2 Generate Tables
      • D-2.2.3 Stop
      • D-2.2.4 Clear Tables
      • D-2.2.5 Mismatch Status / Fix
      • D-2.2.6 Visualization
  • D-3 Launch TabGen in Batch Mode