Solved with COMSOL Multiphysics 4.0a. COPYRIGHT 2010 COMSOL AB.

Similar documents
Solved with COMSOL Multiphysics 4.2

Terminal Falling Velocity of a Sand Grain

Strömningslära Fluid Dynamics. Computer laboratories using COMSOL v4.4

Non-Newtonian Transitional Flow in an Eccentric Annulus

A Comparative CFD Analysis of a Journal Bearing with a Microgroove on the Shaft & Journal

Convection Cooling of Circuit Boards 3D Natural Convection

Solved with COMSOL Multiphysics 4.3a

Solved with COMSOL Multiphysics 4.2

FEMLAB Exercise 1 for ChE366

Middle East Technical University Mechanical Engineering Department ME 413 Introduction to Finite Element Analysis Spring 2015 (Dr.

Porous Reactor with Injection Needle

Steady Flow: Lid-Driven Cavity Flow

Solved with COMSOL Multiphysics 4.2

ANSYS AIM Tutorial Turbulent Flow Over a Backward Facing Step

Implementation in COMSOL

CFD Simulation of Cavitation in an Internal Gear Pump

Non-Isothermal Heat Exchanger

Modeling Evaporating Liquid Spray

Modeling Evaporating Liquid Spray

Fluid Motion Between Rotating Concentric Cylinders Using COMSOL Multiphysics

ANSYS AIM Tutorial Steady Flow Past a Cylinder

Microwell Mixing with Surface Tension

SERBIATRIB 15 STATIC PERFORMANCE OF SURFACE TEXTURED MAGNETORHEOLOGICAL FLUID JOURNAL BEARINGS. 14 th International Conference on Tribology

THE EFFECT OF OIL VISCOSITY ON THE PERFORMANCES OF A TEXTURED JOURNAL BEARING

Solution Recording and Playback: Vortex Shedding

Inviscid Flows. Introduction. T. J. Craft George Begg Building, C41. The Euler Equations. 3rd Year Fluid Mechanics

Simulation of Turbulent Flow in an Asymmetric Diffuser

Free Convection in a Water Glass

MASSACHUSETTS INSTITUTE OF TECHNOLOGY. Analyzing wind flow around the square plate using ADINA Project. Ankur Bajoria

Creating a 2D Geometry Model

Simulation of Laminar Pipe Flows

Potsdam Propeller Test Case (PPTC)

Computer Life (CPL) ISSN: Fluid-structure Coupling Simulation Analysis of Wavy Lip Seals

Verification and Validation of Turbulent Flow around a Clark-Y Airfoil

Computational Study of Laminar Flowfield around a Square Cylinder using Ansys Fluent

Use of CFD in Design and Development of R404A Reciprocating Compressor

For this week only, the TAs will be at the ACCEL facility, instead of their normal office hours.

This tutorial illustrates how to set up and solve a problem involving solidification. This tutorial will demonstrate how to do the following:

VOLCANIC DEFORMATION MODELLING: NUMERICAL BENCHMARKING WITH COMSOL

Modeling and Simulation of Single Phase Fluid Flow and Heat Transfer in Packed Beds

FLUENT Secondary flow in a teacup Author: John M. Cimbala, Penn State University Latest revision: 26 January 2016

Coupled Analysis of FSI

The Level Set Method THE LEVEL SET METHOD THE LEVEL SET METHOD 203

Rotating Moving Boundary Analysis Using ANSYS 5.7

Backward facing step Homework. Department of Fluid Mechanics. For Personal Use. Budapest University of Technology and Economics. Budapest, 2010 autumn

Velocity and Concentration Properties of Porous Medium in a Microfluidic Device

The viscous forces on the cylinder are proportional to the gradient of the velocity field at the

Lateral Loading of Suction Pile in 3D

Simulation of Turbulent Flow around an Airfoil

MAE 323: Lab 7. Instructions. Pressure Vessel Alex Grishin MAE 323 Lab Instructions 1

Technical Report TR

Isotropic Porous Media Tutorial

Development of Hybrid Fluid Jet / Float Polishing Process

NASA Rotor 67 Validation Studies

Introduction to CFX. Workshop 2. Transonic Flow Over a NACA 0012 Airfoil. WS2-1. ANSYS, Inc. Proprietary 2009 ANSYS, Inc. All rights reserved.

Tutorial 1. Introduction to Using FLUENT: Fluid Flow and Heat Transfer in a Mixing Elbow

MASTA 9.0 Release Notes

Simulation of Droplet Impingement on a Solid Surface by the Level Set Method

Fiber Orientation (3D) Solver Verification and Validation

Modeling the Acoustic Scattering from Axially Symmetric Fluid, Elastic, and Poroelastic Objects due to Nonsymmetric Forcing Using COMSOL Multiphysics

Tribology Days Ö-vik 6-8 Nov 2012 Andreas Almqvist, Luleå University of Technology

ISSN(PRINT): ,(ONLINE): ,VOLUME-1,ISSUE-1,

cuibm A GPU Accelerated Immersed Boundary Method

Problem description. The FCBI-C element is used in the fluid part of the model.

Tutorial 2. Modeling Periodic Flow and Heat Transfer

Rotary Ball Spline. With Support Bearing Type Models LTR and LTR-A

JOURNAL BEARING OPTIMIZATION FOR MINIMUM LUBRICANT VISCOSITY

Heat Exchanger Efficiency

Outline. COMSOL Multyphysics: Overview of software package and capabilities

2008 International ANSYS Conference

COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF ORIFICE PLATE METERING SITUATIONS UNDER ABNORMAL CONFIGURATIONS

EFFECT OF SURFACE TEXTURING ON HYDRODYNAMIC PERFORMANCE OF JOURNAL BEARINGS

An Introduction to SolidWorks Flow Simulation 2010

Introduction to ANSYS CFX

Compressible Flow in a Nozzle

A B C D E. Settings Choose height, H, free stream velocity, U, and fluid (dynamic viscosity and density ) so that: Reynolds number

The Transient Modeling of Bubble Pinch-Off Using an ALE Moving Mesh

Using a Single Rotating Reference Frame

CFD Post-Processing of Rampressor Rotor Compressor

ANSYS AIM Tutorial Compressible Flow in a Nozzle

Flow Sim. Chapter 16. Airplane. A. Add-In. Step 1. If necessary, open your ASSEMBLY file.

First Steps - Ball Valve Design

Design a Simple Fan in 123D Design

Thank you for downloading one of our ANSYS whitepapers we hope you enjoy it.

Lab 9: FLUENT: Transient Natural Convection Between Concentric Cylinders

Middle East Technical University Mechanical Engineering Department ME 485 CFD with Finite Volume Method Fall 2017 (Dr. Sert)

Computation of Velocity, Pressure and Temperature Distributions near a Stagnation Point in Planar Laminar Viscous Incompressible Flow

CFD ANALYSIS Of COMBINED 8-12 STAGES Of INTERMIDIATE PRESSURE STEAM TURBINE

Flow Sim. Chapter 14 P-51. A. Set Up. B. Create Flow Simulation Project. Step 1. Click Flow Simulation. SolidWorks 10 Flow Sim P-51 Page 14-1

Preliminary Spray Cooling Simulations Using a Full-Cone Water Spray

3D Simulation of Dam-break effect on a Solid Wall using Smoothed Particle Hydrodynamic

NUMERICAL METHOD FOR FREE SURFACE VISCOUS FLOWS

Applications of ICFD solver by LS-DYNA in Automotive Fields to Solve Fluid-Solid-Interaction (FSI) Problems

Driven Cavity Example

ALE Seamless Immersed Boundary Method with Overset Grid System for Multiple Moving Objects

Calculate a solution using the pressure-based coupled solver.

SU 2 : Advanced Analysis Topics

Tutorial: Modeling Domains with Embedded Reference Frames: Part 2 Sliding Mesh Modeling

CHAPTER 3. Elementary Fluid Dynamics

Application of Wray-Agarwal Turbulence Model for Accurate Numerical Simulation of Flow Past a Three-Dimensional Wing-body

Transcription:

Journal Bearing Introduction Journal bearings are used to carry radial loads, for example, to support a rotating shaft. A simple journal bearing consists of two rigid cylinders. The outer cylinder (bearing) wraps the inner rotating journal (shaft). Normally, the position of the journal center is eccentric with the bearing center. A lubricant fills the small annular gap or clearance between the journal and the bearing. The amount of eccentricity of the journal is related to the pressure that will be generated in the bearing to balance the radial load. The lubricant is supplied through a hole or a groove and may or may not extend all around the journal. Under normal operating conditions, the gases dissolved in the lubricant cause cavitation in the diverging clearance between the journal and the bearing. This happens because the pressure in the lubricant drops below the saturation pressure for the release of dissolved gases. The saturation pressure is normally similar to the ambient pressure. The following model does not account for cavitation and therefore predicts sub-ambient pressures. Such sub-ambient pressures are the result of the so-called Sommerfeld boundary condition. For practical purposes, these sub-ambient pressures should be neglected. Future versions of the Lubrication Shell physics interface will offer additional tools for modeling cavitation. Model Definition The pressure in the lubricant (SAE 10 at 70 C) is governed by the Reynolds equation. For an incompressible fluid with no-slip condition, the stationary Reynolds equation in the continuum range is given by ρh 3 T ------------ p ------ ρh v 12η T + ( 2 a + v b ) ρ (( T b v b ) ( T a v a )) = 0 (1) In this equation, ρ is the density (kg/m 3 ), h is the lubricant thickness (m), η is the viscosity (Pa s), p is the pressure (Pa), a is the location (m) of the channel base, v a is the tangential velocity (m/s) of the channel base, b is the location (m) of the solid wall, and v b is the tangential velocity (m/s) of the solid wall. Here the rotating journal is considered to be the solid wall. Figure 1 shows the rotating journal wall on which you solve the Reynolds equation. Because the pressure is constant through the lubricant JOURNAL BEARING 1

film thickness, COMSOL uses the tangential projection of the gradient operator, T, to calculate the pressure distribution on the lubricant surface. Note that in this case the term ρ(( T b v b ) ( T a v a )) equates to 0, so the governing equation simplifies to ρh 3 T ------------ p ------ ρh v 12η T + ( 2 a + v b ) = 0 (2) The lubricant thickness, h, is defined as h = c( 1 + εcosθ) where c R B R J is the difference between the bearing radius and the journal radius, ε is the eccentricity, and θ is the polar angular coordinate of a point on the lubricant. Figure 2 shows the converging and diverging lubricant thickness around the journal. Figure 1: Geometry (cylindrical journal) showing the velocity direction with black arrows. 2 JOURNAL BEARING

Figure 2: The lubricant thickness around the rotating journal. BORDER CONDITIONS The pressure at the ends of the cylindrical journal is assumed to be similar to the ambient pressure. Therefore, the border conditions are p = 0 at z = 0, L (3) where L is the length of the cylindrical journal. Results and Discussion Figure 3 shows the calculated pressure distribution and pressure contours. As expected, the maximum pressure is reached in a region closer to the minimum lubricant thickness. Sub-ambient or negative pressure also results due to approximate boundary conditions. For a more accurate modeling of pressure distribution, gaseous cavitation has to be taken into account. JOURNAL BEARING 3

Figure 3: Pressure distribution and pressure contours on the journal. Model Library path: CFD_Module/Tutorial_Models/journal_bearing Modeling Instructions MODEL WIZARD 1 Go to the Model Wizard window. 2 Click Next. 3 In the Add Physics tree, select Fluid Flow>Thin-Film Flow>Lubrication Shell (tffs). 4 Click Next. 5 In the Studies tree, select Preset Studies>Stationary. 6 Click Finish. 4 JOURNAL BEARING

GLOBAL DEFINITIONS Parameters 1 In the Model Builder window, right-click Global Definitions and choose Parameters. 2 Go to the Settings window for Parameters. 3 Locate the Parameters section. In the Parameters table, enter the following settings: NAME EXPRESSION DESCRIPTION R 0.03[m] Journal radius H 0.05[m] Journal height c 0.03[mm] Clearance between the bearing and the journal omega 1500/60*2*pi[rad/s] Journal angular velocity GEOMETRY 1 Cylinder 1 1 In the Model Builder window, right-click Model 1>Geometry 1 and choose Cylinder. 2 Go to the Settings window for Cylinder. 3 Locate the Object Type section. From the Type list, select Surface. 4 Locate the Size and Shape section. In the Radius edit field, type R. 5 In the Height edit field, type H. 6 In the Model Builder window, right-click Cylinder 1 and choose Build All. 7 Click the Zoom Extents button on the Graphics toolbar. DEFINITIONS Variables 1 1 In the Model Builder window, right-click Model 1>Definitions and choose Variables. 2 Go to the Settings window for Variables. 3 Locate the Variables section. In the Variables table, enter the following settings: NAME EXPRESSION DESCRIPTION angle atan2(y,x)[rad] Angle along circumference h c*(1+0.6*cos(angle)) Lubricant film thickness u -omega*r*sin(angle) x-component of journal velocity v omega*r*cos(angle) y-component of journal velocity JOURNAL BEARING 5

LUBRICATION SHELL Fluid-Film Properties 1 1 In the Model Builder window, expand the Model 1>Lubrication Shell node, then click Fluid-Film Properties 1. 2 Go to the Settings window for Fluid-Film Properties. 3 Locate the Fluid Properties section. From the ρ list, select User defined. In the associated edit field, type 860[kg/m^3]. 4 From the µ list, select User defined. In the associated edit field, type 0.01[Pa*s]. 5 Click to expand the Gap Properties section. 6 In the h 0 edit field, type h. 7 From the u t,w list, select User defined. Specify the associated vector as u x v y 0 z 8 Click to collapse the Gap Properties section. 9 Click to expand the Rarefaction Effects section. 10 From the Q ch list, select No slip. Border 1 As you can see in the Border Settings section, the default condition that applies at the cylinder ends is Zero pressure. MESH 1 Free Triangular 1 1 In the Model Builder window, right-click Model 1>Mesh 1 and choose More Operations>Free Triangular. 2 Go to the Settings window for Free Triangular. 3 Locate the Boundaries section. From the Selection list, select All boundaries. 4 Click the Build Selected button. STUDY 1 In the Model Builder window, right-click Study 1 and choose Compute. 6 JOURNAL BEARING

RESULTS 3D Plot Group 1 The first of the two default plot group shows the pressure field as a surface plot. Add a contour plot of the same quantity to reproduce the plot in Figure 3. 1 In the Model Builder window, right-click Results>3D Plot Group 1 and choose Contour. 2 Go to the Settings window for Contour. 3 Locate the Coloring and Style section. From the Color table list, select GrayScale. 4 Clear the Color legend check box. To see the bearing from different angles just click and drag in the Graphics window. JOURNAL BEARING 7

8 JOURNAL BEARING Solved with COMSOL Multiphysics 4.0a. COPYRIGHT 2010 COMSOL AB.