Workshop 5 Centrifugal Pump

Slides:



Advertisements
Similar presentations
Workshop 6 Electronics Cooling with Natural Convection and Radiation
Advertisements

Chapter 10 Transient Flow Modeling
Fluent Overview Ahmadi/Nazridoust ME 437/537/637.
Workshop 7 Tank Flushing
Outline Overview of Pipe Flow CFD Process ANSYS Workbench
Workshop 10 Turbo Pre and Post
Workshop 5 Cavitating Centrifugal Pump
Workshop 8 Transient Brake Rotor
Chapter 4 Boundary Conditions
D-1 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory # Appendix D Profile Boundary Conditions Introduction.
Computer Simulation of Vehicle Aerodynamic Forces and Moments Using Fluent 6.2 MSC VisualNastran 4D WorkingModel 2D Zerguy Maazouddin California State.
An Analysis of Hiemenz Flow E. Kaufman and E. Gutierrez-Miravete Department of Engineering and Science Rensselaer at Hartford.
Workshop 6 Modeling of Catalytic Convertor
Numerical Modeling of Fluid Flows (BMEGEÁTAM5)
Workshop XX Transonic Flow over a RAE 2822 Airfoil
Computer Aided Thermal Fluid Analysis Lecture 10
© Fluent Inc. 5/17/ Introductory FLUENT Notes FLUENT v6.0 Jan 2002 Fluent User Services Center Boundary Conditions.
Boundary Conditions.
Electromagnetic Analysis of a 2 Gap Solenoid
Workshop 1 Mixing T-Junction
DesignXplorer Parameter Manager Workshop 9. DesignXplorer Parameter Manager Workshop Supplement August 26, 2005 Inventory # WS9-2 Workshop 9 – Goals.
Workshop 3 Room Temperature Study
Chapter 7 Interfaces, Sources and Additional Variables
Chapter 10 Heat Transfer Introduction to CFX.
Chapter 3 Meshing Methods for 3D Geometries
ANSYS BladeModeler 11.0 Practical 1
Workshop 2 Transonic Flow over a NACA 0012 Airfoil
Workshop 2 Transonic Flow Over a NACA 0012 Airfoil.
Ansys Workbench 1 Introduction
© Fluent Inc. 9/20/ Introductory FLUENT Notes FLUENT v6.0 Jan 2002 Fluent User Services Center Solver Basics.
Workshop 4 Flow Through Porous Media
Catalytic Converter Simulation
CFD Pre-Lab 2 Simulation of Turbulent Flow around an Airfoil Seong Mo Yeon, and Timur Dogan 11/12/2013.
15-1 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory # Chapter 15 Review and Tips Introduction to CFX.
Workshop 3 Room Temperature Study (Part 1)
Workshop 4 Electronics Cooling with Natural Convection and Radiation
WS8.1-1 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory # Workshop 8.1 Line and Surface Bodies DesignModeler.
Numerical investigation on the upstream flow condition of the air flow meter in the air intake assembly of a passenger car Zoltán Kórik Supervisor: Dr.
WS09-1 VND101, Workshop 09 MSC.visualNastran 4D Exercise Workbook Belted Cylinder.
Appendix B Turbo Pre and Post
6-1 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory # Chapter 6 Day 1 Review and Tips Introduction to CFX.
CFX-10 Introduction Lecture 1.
Version 1.0 3/23/2007 © 2007 ANSYS, Inc. All rights reserved. Inventory # W2-1 BladeModeler 11.0 ANSYS, Inc. Proprietary ANSYS BladeModeler 11.0.
Heating Coil Simulation
WS7-1 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory # Introductory FLUENT Training Workshop 7 Tank Flushing.
2006 International ANSYS Conference BladeModeler Demonstration Creating a Centrifugal Compressor Impeller Workshop 20 ANSYS CFX 11.0.
Version 1.0 3/23/2007 © 2007 ANSYS, Inc. All rights reserved. Inventory # W8-1 BladeModeler 11.0 ANSYS, Inc. Proprietary BladeModeler 11.0 Practical.
Multiple Species Chapter 7. Training Manual May 15, 2001 Inventory # Objectives The FLOTRAN multiple species capabilities. Dilute mixture option.
1-1 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory # Chapter 1 ANSYS Workbench ANSYS Meshing Application.
Version 1.0 3/23/2007 © 2007 ANSYS, Inc. All rights reserved. Inventory # W6-1 BladeModeler 11.0 ANSYS, Inc. Proprietary BladeModeler 11.0 Practical.
WS6.3-1 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. July 2009 Inventory # Chapter 6 Introduction to Hexa – Workshop 3 3D Pipe.
13-1 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory # Chapter 13 Solver.out File and CCL Introduction to.
1 Tutorial. 2 Solution Process 1.Gather Information 2.Create the Computational Grid 3.Set the Boundary Conditions 4.Set the Initial Conditions 5.Set the.
Version 1.0 3/23/2007 © 2007 ANSYS, Inc. All rights reserved. Inventory # W3-1 BladeModeler 11.0 ANSYS, Inc. Proprietary ANSYS BladeModeler 11.0.
Version 1.0 3/23/2007 © 2007 ANSYS, Inc. All rights reserved. Inventory # W0-1 BladeModeler 11.0 ANSYS, Inc. Proprietary ANSYS TurboSystem Practical.
Version 1.0 3/23/2007 © 2007 ANSYS, Inc. All rights reserved. Inventory # W4-1 BladeModeler 11.0 ANSYS, Inc. Proprietary ANSYS BladeModeler 11.0.
WS2B-1 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 30, 2009 Inventory # Workshop 2B Assembly Contact Workbench-Mechanical.
7-1 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. April 28, 2009 Inventory # Chapter 7 Introduction to MultiZone Meshing ANSYS.
TransAT Tutorial Backward Step May 2015 ASCOMP
Chapter 10 Transient Flow Modeling
Workshop 6 Electronics Cooling with Natural Convection and Radiation
Workshop 7 Tank Flushing
Workshop 7 Tank Flushing
Workshop 6 Modeling of Catalytic Convertor
Workshop 5 Cavitating Centrifugal Pump
Workshop 5 Centrifugal Pump
Workshop 4 Electronics Cooling with Natural Convection and Radiation
Workshop 2 Transonic Flow Over a NACA 0012 Airfoil.
Fluent Overview Ahmadi/Nazridoust ME 437/537/637.
Workshop 4 Flow Through Porous Media
Presentation transcript:

Workshop 5 Centrifugal Pump Introductory FLUENT Training

Introduction The Purpose of the tutorial is to model fluid flow in a centrifugal pump, which involves the use of rotation model. Problem consists of a five blade centrifugal pump operating at 2160 rpm. The working fluid is water and flow is assumed to be steady and incompressible. Due to rotational periodicity a single blade passage will be modeled.

Starting Fluent in Workbench Open the Workbench (Start > Programs > ANSYS 12.0 > ANSYS Workbench) Drag FLUENT into the project schematic Change the name to Duct Double click on Setup Choose 3D and Double Precision under Options and retain the other default settings

Import Mesh This starts a new Fluent session and the first step is to import the mesh that has already been created: Under the File menu select Import> Mesh Select the file tfa-pump-lite-cav-300k.msh and click OK to import the mesh After reading the mesh, check the grid using Mesh>Check option or by using Check under Problem Setup>General

Setting up the Models Select Pressure Based, Steady state solver Problem Setup>General>Solver Specify Turbulence model Problem Setup > Models > Viscous Double click and Select k-epsilon (2 eqn) under Model and Realizable under k-epsilon model and retain the default settings for the other parameters Make sure that the Energy Equation is disabled Problem Setup > Models> Energy

Materials Define the materials. Problem Setup > Materials Click on air to open Create/Edit Materials panel Change Name to water and Density and Viscosity to 1000 kg/m3 and 0.001 kg/(m-s) respectively Click on Change/Create Click on Yes, on being asked for Change/Create mixture and Overwrite air

Fluid Zone Conditions Under Problem Setup >Cell Zone Conditions (operating conditions are also in BC panel) double click on Fluid Select Material Name : water Select Motion Type: Moving Reference Frame Specify Rotational Velocity : 2160 rpm Click on OK

Operating Conditions Under Problem Setup >Cell Zone Conditions (operating conditions are also in BC panel) Click on Operating Conditions… and set the Operating Pressure (Pascal) to 0

Boundary Conditions Under Problem Setup > Boundary Conditions Select inlet under Zone and choose velocity-inlet from the drop down menu under Type Now double click on inlet under Zone Input all the parameters in Momentum tab as shown below

Boundary Conditions Under Problem Setup > Boundary Conditions Select outlet under Zone and choose pressure-outlet from the drop down menu under Type Now double click on outlet under Zone Input all the parameters in Momentum tab as shown below

Boundary Conditions Under Problem Setup > Boundary Conditions Select blade under Zone and choose wall from the drop down menu under Type Now double click on blade under Zone Input all the parameters in Momentum tab as shown below

Boundary Conditions Under Problem Setup > Boundary Conditions Select hub under Zone and choose wall from the drop down menu under Type Now double click on hub under Zone Input all the parameters in Momentum tab as shown below

Boundary Conditions Under Problem Setup > Boundary Conditions Select shroud under Zone and choose wall from the drop down menu under Type Now double click on shroud under Zone Input all the parameters in Momentum tab as shown below

Boundary Conditions Under Problem Setup > Boundary Conditions Select hub-outer under Zone and choose wall from the drop down menu under Type Now double click on hub-outer under Zone Input all the parameters in Momentum tab as shown below

Boundary Conditions Under Problem Setup > Boundary Conditions Select inlet-shroud under Zone and choose wall from the drop down menu under Type Now double click on inlet-shroud under Zone Input all the parameters in Momentum tab as shown below

Boundary Conditions Under Problem Setup > Boundary Conditions Select shroud-outer under Zone and choose wall from the drop down menu under Type Now double click on shroud-outer under Zone Input all the parameters in Momentum tab as shown below

Boundary Conditions Under Problem Setup > Boundary Conditions Select periodic.10 under Zone and choose periodic from the drop down menu under Type Now double click on periodic.10 under Zone Select Periodic Type: Rotational Click on OK Now double click on periodic.11 under Zone

Monitors Residual Monitoring Solution > Monitors Double click on Residuals (By default it is on) Enable Plot under Options. Specify Absolute Criteria for continuity: 1e-5

Monitors Surface Monitors Monitor points are used to monitor quantities of interest during the solution. They should be used to help judge convergence. In this case you will monitor the Total Pressure and Static Pressure at inlet. Solution > Monitors > Surface Monitors Click on Create to create a new surface monitor Type ‘total_pressure’ under Name Enable Printing, Plotting and writing of monitors by marking check boxes under Options Select Mass-Weighted Average from the drop-down menu under Report Type Select Pressure as the Field Variable and select Total Pressure under Pressure variable

Monitors Select inlet as the Surfaces to be monitored Click on OK to create the monitor and to close the panel

Monitors Solution > Monitors > Surface Monitors Click on Create to create a new surface monitor Type ‘static_pressure’ under Name Enable Printing, Plotting and writing of monitors by marking check boxes under Options Select Area-Weighted Average from the drop-down menu under Report Type Select Pressure as the Field Variable and select Static Pressure under Pressure variable Select inlet as the Surfaces to be monitored Click on OK to create the monitor and to close the panel

Initialization Before starting the calculations we must initialize the flow field in the entire domain Solution > Monitors > Solution Initialization Initializing the flow field with near steady state conditions will result in faster convergence Select Compute from: inlet Click on Initialize to initialize the solution

Run Calculations The solution process can be started in the following manner Solution >Run Calculation Enter 1000 for Number of Iterations and click on Calculate During the iteration process, both the residue plot and monitor plots will be shown in different windows. If the velocity monitor is not changing further we can stop the iterations. You may specify more number of iterations if the monitors are still changing significantly. The magnitude of change of a monitor per iteration can be observed from the console (enabled by clicking on Print to Console while creating the monitor) Note: Iterations can be stopped in between, by pressing Ctrl+ C together in the Fluent’s console.

Higher Order Accurate Solution Once first order run is converged (it takes 211 iterations) Under Solution>Solution Methods setup the parameters as shown below The solution process can be started in the following manner Solution >Run Calculation Enter 1000 for Number of Iterations and click on Calculate

Residuals

Write Case File You can now save the project and proceed to write a case file for the solver: To save the project, go to Project Page File>Save as To write the case files, go to FLUENT session File>Export>Case..

Post Processing To Draw Contours of Static Pressure on blade Display > Graphics and Animations Double Click on Contours, a new window will pop up Select Pressure under Contours of and Static Pressure below that Select blade under Surfaces

Post Processing To Draw Contours of Static Pressure on hub Display > Graphics and Animations Double Click on Contours, a new window will pop up Select Pressure under Contours of and Static Pressure below that Select hub under Surfaces

Post Processing To Draw Contours of Static Pressure on shroud Display > Graphics and Animations Double Click on Contours, a new window will pop up Select Pressure under Contours of and Static Pressure below that Select shroud under Surfaces