Title: ANSYS CFX S3 PreProcess, Solve
1ANSYS CFXS3 Pre-Process, Solve Post-Process
- Maryam Einian
- mae345_at_mail.usask.ca
- CFD lab 1B85
2Numerical Simulation
Pre-Processor
Geometry
Solver
Post-Processor
Meshing
CFX-Pre
3ANSYS Workbench CFX-Pre
- ANSYS Workbench
- Select a Mesh File --gt .cmdb
- Advanced CFD Tasks
- Create CFD Simulation with Mesh
- Examine in CFX-Post
- CFX-Pre
4CEX-Pre Mesh
- Automatically Uploaded
- Import Mesh
- Principal 3-D Regions
- Principal 2-D Regions
- Edit Definition
- Edit Mesh
- Statistics
5CFX-Pre Quick Setups (Gen/Turbo)
- Quick Setup Mode
- Very Simple Problems
- Set Boundary Conditions before-hand
- Turbo Mode
- Pump, Fan, Compressors, Turbines
- Set Boundary Conditions before-hand
- Set Domains and Coordinate Systems before hand
6CFX-Pre General Overview
- Simulation Type
- Details of Domain
- Boundary Conditions
- Solver Set-ups
7CFX-Pre Simulation Type
- External Solver Coupling
- None
- ANSYS Multifield Structural, Electro-Magnetics
- ANSYS Multifield via Prep 7
- Simulation Type
- Steady State
- Transient
8Details of Domain General Options
- Basic Settings
- Location 3D regions--gt Multi-Domain Problems
- Domain Type Fluid/Solid/Porous
- Fluids List Various Materials
- Coord Frame
- Domain Models
- Reference Pressure Absolute Press--gtVacuum
- Buoyancy Gravity--gtBuoyant Plumes, Ships
- Domain Motion Stationary/Rotating--gtPumps/Turbo-Ma
chinery - Mesh Deformation Varying Geometry/Moving Walls
--gt Expansion
9Details of Domain Fluid Models-Initialisation
- Heat Transfer
- None incompressible flows
- Isothermal constant temp
- Thermal Energy low-speed flows
- Total Energy high-speed energy effects
- Turbulence- Near Wall Modeling
- None (Laminar) Laminar flows
- K-Epsilon Most Popular
- Shear Stress Transport Advanced
- BSL Reynolds Stress Advanced
- SSG Reynolds Stress Advanced
- Reaction or Combustion
- Thermal Radiation Model
- Initialisation
10Boundary Conditions
- Inlet Flows into the Domain
- Flow Regime (Subsonic/Supersonic/Mixed)
- Mass and Momentum, Turbulence Intensity, Heat
Transfer - Initialise Profile Date
- Outlet Flows out of the Domain
- Flow Regime (Subsonic/Supersonic)
- Mass and Momentum, Pressure Averaging
- Opening Flows both into and out of the Domain
- Flow Regime (Subsonic)
- Mass and Momentum, Pressure, Turbulence, Heat
Transfer - Wall Slip/No-Slip Walls
- Slip/No-Slip, wall Velocity
- Smooth/Rough
- Heat Transfer
- Symmetry Geometric and Flow Symmetry
- General for all boundary types (Location,
Sources, Plot options)
11Solver Set-ups
- Basic Settings (units)
- Solver Control
- Output Control
- Mesh Refinement (Adaptation Option)
- Expert Parameters
12Solver Setups Solver Control
- Advection Scheme (CDS, UDS, Hybrid)
- Maximum Number of Iterations
- Fluid Time Scale Control ?t
- Convergence Criteria
- Residual Types RMS (Root Mean Square), Max
- Residual Target xE-Y
- Equation Class
- Advanced Options
13CFX-pre Finalize
- Additional Variables
- Expressions
- User Functions
- User Routines
- Write Solver File
- CFX-Pre --gt CFX-Solver
14Simulation Type
- External Solver Coupling
- None
- Simulation Type
- Steady State
ANSYS-CFX Website
15Details of Domain General Options
- Basic Settings
- Location B82
- Domain Type Fluid Domain
- Fluids List Air at 25 C
- Coord Frame Coord 0
- Domain Models
- Reference Pressure 1 atm
- Buoyancy Non Buoyant
- Domain Motion Stationary
- Mesh Deformation None
16Details of Domain Fluid Models - Initialisation
- Heat Transfer None
- Turbulence K-Epsilon
- Near Wall Modeling Scalable
- Reaction or Combustion
- Thermal Radiation Model
17Boundary Conditions
- Inlet Inlet
- Flow Regime --gt Subsonic
- Mass FR --gt 0.1 m/s
- Direction --gt Normal to BC
- Turbulence Intensity --gt Medium
- Outlet Outlet
- Flow Regime --gt Subsonic
- Mass FR --gt 0.1 m/s
- TB Wall
- Free Slip
- Plate Wall
- No-slip
- Smooth Wall
- Side Walls Symmetry
18Solver Setups Solver Control
- Advection Scheme Upwind
- Max. Iterations 50
- Fluid Time Scale Control
- Time Scale Control Auto Time Scale
- Time Scale Factor 1.5
- Convergence Criteria
- Residual Types RMS (root mean square)
- Residual Target 1.E-5
19CFX-Pre --gt CFX-Solver
- Save
- Export CCL (CFX Command Language)
- Write Solver File
20CFX-Solver
- Definition File Automatically Uploaded
- Initial Values File If Available (Resume)
- Adaptation Database
- Type of Run
- Full
- Partitioner Only For Parallel Solvers
- Parallel Environment Run Mode
- Serial
- PVMs Parallel Virtual Machine
- MPIs Message Passing Interface
21CFX-Solver
- Out File
- Residuals
- Equations
- Mass and Momentum (3 Momentum (x,y,x) 1
Mass) - Turbulence (KE) (1 ? and 1 e eq.)
- Modes
- RMS
- MAX
22CFX-Post
- Select a Surface
- Color Variable Mode
- Variable Pressure, Velocity,
- Range Global/Local
- Color Scale Linear
- Color Map Rainbow
-
- Apply
22
23CFX-Post Create Locations
- Geometric Locations (X,Y,Z)
- Point, Point Cloud
- Line
- Plane
- Volume
- Geometric and Flow Locations
- Isosurface
- Surface of Revolution
- Polyline
- User Surface
24CFX-Post Visual Options
- Domain
- Location
- Range
- Sampling
- Reduction Factor
- Variable
- Vector
- Contours
- Streamlines
25CFX-Post Define Exp.-Var.
- Insert Expression
- Functions
- CFX-Post
- CEL
- Expressions
- Variables
- Locations
- Constants
- Insert Variable
- Methods
- Expression
- Frozen Copy
- Dimensions
- Scalar
- Vector (3D)
26CFX-Post Tables-Charts
- Insert Chart
- Type
- Regular
- From File
- Location
- X Axis Variable
- Y Axis Variable
- Conservative (original)
- Hybrid (recalculated)
- Insert Table
- Functions
- CFX-Post
- CEL
- Expressions
- Variables
- Locations
- Constants
- Export File .csv
- Export Geometry
- Select Variables
27CFX-Post Tools
- Probe
- Function Calculator
- Macro Calculator (Turbo)
- Mesh Calculator
28CFX-Post
- Plate
- Color
- Mode Variable
- Variable Pressure
- Range Global/Local
- Color Scale Linear
- Color Map Rainbow
-
- Apply
28
29CFX-Post Create Locations
- Insert Locations
- Line
- Method (Two Points)
- Point1 (8,0,5) Point2 (8,10,5)
- Sample 200
- Plane
- Method (XY Plane)
- Z (5 m)
- Isosurface
- Variable (Pressure/Velocity)
- Value (1E-4)
30CFX-Post Visual Options
- Vector
- Locations (Plane 1)
- Sampling (Equally Spaced)
- of Points (200)
- Variable (Velocity)
- Contours
- Locations (Plane1)
- Variable (Pressure/Velocity)
- Range (Global/Local)
- of Contours (20)
- Streamlines
- Type (Surface Streamlines)
- Surfaces (Plane 1)
- Start From (Locations/Inlet)
- Reduction (Max Number of Points)
- Variable (Velocity)
31CFX-Post Define Exp.-Var.
- Insert Expression CPEXP
- (Pressure Variables - Reference Pressure
Expressions) - /(Density Variables(Mass Flow CFX-Function _at_
inlet Locations /Area CFX-Function _at_ Inlet
Locations)2) - Insert Variable CP
- Method Expression
- Scalar
- Expression CPEXP
-
32CFX-Post Tables-Charts
- Insert Chart
- Type Regular
- Location Line 1
- X Axis Variable Velocity
- Y Axis Variable Y
- of Samples for the Line
- 10 ----gt 200
- Export File .csv
- File Out.csv
- Type Generic
- Location Line1
- Boundary Values Hybrid
- Export Geometry Info
- Grid Info (Line/Face Con-Node )
- Select Variables (Velocity/Pressure)