Rolling contact stresses between two rigid, axial and flat cylinders

Similar documents
Formulae for calculations A) Nomenclature

EXPERIMENTAL INVESTIGTION OF THE FRETTING PHENOMENON-DEPENDENCE OF NUMBERS CYCLES

NUMERICAL AND EXPERIMENTAL VALIDATION OF CHIP MORPHOLOGY

FINITE ELEMENT SIMULATIONS OF THE EFFECT OF FRICTION COEFFICIENT IN FRETTING WEAR

Nonlinear behavior of Reinforced Concrete Infilled Frames using ATENA 2D

Behaviour of shot peening combined with WC-Co HVOF coating under complex fretting wear and fretting fatigue loading conditions

The Behaviour Of Round Timber Sections Notched Over The Support On The Tension Face. Justin Dewey

An Alternative Formulation for Determining Stiffness of Members with Bolted Connections

ARTICLE IN PRESS. Wear xxx (2007) xxx xxx. Nanofretting behaviors of NiTi shape memory alloy

FRETTING FATIGUE BEHAVIOR OF A TITANIUM ALLOY TI-6AL-4V AT ELEVATED TEMPERATURE THESIS. Onder Sahan, Lieutenant, TUAF AFIT/GAE/ENY/02-11

Fretting Wear Failures In Bearing Steel EN31 Mated Against Structural Steel EN 24

Drawing of Hexagonal Shapes from Cylindrical Cups

Thermo-mechanical Coupled Simulation Analysis of Solid End Mill on. Milling Process

EFFECTS OF PROCESS VARIABLES ON DIMENSIONAL CONTROL OF COLD DRAWN 1526 GRADE STEEL TUBING NICKOLAS LANGILOTTI

Fatigue and Fretting Studies of Gas Compressor Blade Roots

Permanent fasteners: Riveted joints Welded joints Detachable joints: Threaded fasteners screws, bolts and nuts, studs. Cotter joints Knuckle joints

INFLUENCE OF PILES ON LOAD- SETTLEMENT BEHAVIOUR OF RAFT FOUNDATION

Module 3 Selection of Manufacturing Processes

THEORY OF METAL CUTTING

THE COEFFICIENT OF FRICȚION IN THE FRETTING PHENOMENON

Process simulation using finite element method prediction of cutting forces, tool stresses and temperatures in highspeed flat end milling

THIN-WALLED HOLLOW BOLTS

Computational modelling of a precision optical lens polishing process on small radius spherical surfaces

TRANSVERSE FATIGUE CHARACTERISTICS OF BOLTED JOINTS TIGHTENED THIN PLATES

EFFECTS OF GEOMETRY ON MECHANICAL BEHAVIOR OF DOVETAIL CONNECTION

The influence of gouge defects on failure pressure of steel pipes

Research on the Strength of Roadheader Conical Picks Based on Finite Element Analysis

Hours / 100 Marks Seat No.

Ultrasonic Testing using a unipolar pulse

3-D Finite Element Analysis of Bolted Joint Using Helical Thread Model

PRO LIGNO Vol. 11 N pp

Stress Analysis Of Bolted Joint

Structural Deformation of a Circular Thin Plate with Combinations of Fixed and Free Edges

AIR FORCE INSTITUTE OF TECHNOLOGY

What Is EHD? examining the concepts involved in hydrodynamic lubrication is fundamental to our understanding of elastohydrodynamics.

MECH 344/M Machine Element Design

Indian Journal of Engineering An International Journal ISSN EISSN Discovery Publication. All Rights Reserved

SIMULATION AND EXPERIMENTAL WORK OF SINGLE LAP BOLTED JOINT TESTED IN BENDING

Bending. the bend radius is measured to the inner surface of the bent part

Effect of Bolt Layout on the Mechanical Behavior of Four Bolted Shear Joint

Contact Pressure Prediction Comparison Using Implicit and Explicit Finite Element Methods and the Validation with Hertzian Theory

Fasteners. Fastener. Chapter 18

Bearing Capacity of Strip Footings on Two-layer Clay Soil by Finite Element Method

Supporting Online Material for

Technical Data. 17. Technical data Deep groove ball bearing radial internal clearances and axial internal clearances A

Rotary Steering Spindle System Parameter Design Based on Fatigue Life

A Full 3-D Finite Element Analysis of Group Interaction Effect on Laterally Loaded Piles

Physics 506 Winter 2006 Homework Assignment #2 Solutions

Young W. Park Department of Industrial and Manufacturing Systems Engineering Iowa State University Ames, IA 50011

Fatigue crack propagation in uniaxial loading and bending fatigue in 20 khz testing. Mohamed Sadek PhD Student Karlstad university

Study on embedded length of piles for slope reinforced with one row of piles

Improving Edge Quality in Film Applications with Tangent Shear Slitting

Glued laminated timber beams repair.

MANUFACTURING TECHNOLOGY

Rayleigh Wave Interaction and Mode Conversion in a Delamination

A Numerical study on proper mode and frequency selection for riveted lap joints inspection using Lamb waves.

Vertical Struts. P16603: Work Piece Movement Jonathan Sanabria April 19, Contents

Finite Element Modeling of Early Stage Self-loosening of Bolted Joints Haoliang Xu 1, a, Lihua Yang 1, b,, Lie Yu 1,2, c

THE INFLUENCE OF MULTIPLE NESTED LAYER WAVINESS ON COMPRESSION STRENGTH OF CARBON FIBER COMPOSITE MATERIALS

1. Enumerate the most commonly used engineering materials and state some important properties and their engineering applications.

Effect of die channel angle and friction coefficient in ECAP-Conform process for Al-6061 alloy

Compression vs. Fusion: The Source of Strength in Fused Sight Glasses for Chemical and Pharmaceutical Processes

Power Threads. Shigley s Mechanical Engineering Design

Failure of Engineering Materials & Structures. Code 34. Bolted Joint s Relaxation Behavior: A FEA Study. Muhammad Abid and Saad Hussain

EPS Allowable Stress Calculations (Rev. 2)

THE INFLUENCE OF GOUGE DEFECTS ON FAILURE PRESSURE OF STEEL PIPES

DESIGN AND ANALYSIS OF FORM TOOL

RESEARCH PAPERS FACULTY OF MATERIALS SCIENCE AND TECHNOLOGY IN TRNAVA, SLOVAK UNIVERSITY OF TECHNOLOGY IN BRATISLAVA, 2016 Volume 24, Number 39

EFFECT OF ADHEREND SHAPE ON STRESS CONCENTRATION REDUCTION OF ADHESIVELY BONDED SINGLE LAP JOINT

Influence of Lubrication and Draw Bead in Hemispherical Cup Forming

Ph.D. Preliminary Qualifying Examination. Cover Page. Thermodynamic. January 17, 2013 (Thursday) 9:30 am 12:30 noon Room 2145 Engineering Building

VIBRATIONAL MODES OF THICK CYLINDERS OF FINITE LENGTH

Bar, Wire and tube drawing

ANALYSIS OF LATERAL STIFFNESS FOR INFILLED FRAME WITH OPENING

This is an author-deposited version published in: Handle ID:.

Abaqus Beam Tutorial (ver. 6.12)

Sliding shear capacities of the Asymmetric Friction Connection

EXAMPLE 1-4 EXAMPLE 1-5

AN INNOVATIVE FEA METHODOLOGY FOR MODELING FASTENERS

Fundamentals of Machining/Orthogonal Machining

Quantitative Crack Depth Study in Homogeneous Plates Using Simulated Lamb Waves.

Fretting Fatigue of Slot-dovetails in Turbo-generator Rotor

D DAVID PUBLISHING. Analysis of Leakage in Bolted-Flanged Joints Using Contact Finite Element Analysis. 1. Introduction.

Note: Conditions where bending loads are imposed on the bolt e.g. non-parallel bolting surfaces, should be avoided.

Prediction Of Thrust Force And Torque In Drilling On Aluminum 6061-T6 Alloy

3-D FEA OF HARD TURNING: INVESTIGATION OF PCBN CUTTING TOOL MICRO- GEOMETRY EFFECTS

Finite Element Analysis of Multi-Fastened Bolted Joint Connecting Composite Components in Aircraft Structures

Traction and Efficiency Performance of Ball Type CVTs

This thesis is approved, and it is acceptable in quality and form for publication:

Stress Analysis of Flanged Joint Using Finite Element Method

# in 1 Metal Worker Auxiliary Operating Instructions

Optimization of a Love Wave Surface Acoustic Device for Biosensing Application

Traction and Efficiency Performance of Ball Type CVTs

Settlement Analysis of Piled Raft System in Soft Stratified Soils

Fretting Fatigue. Etude & prédiction de la durée de vie. LTDS, CNRS, Ecole Centrale de Lyon, Ecully, France. contact :

International Journal of Machine Tools & Manufacture 42 (2002)

Abaqus/CAE (ver. 6.14*) Plate/Shell Tutorial

Study on micro extra deep drawing process with ultrahigh fluid pressure and press motion controls

Modeling and Finite Element Analysis Methods for the Dynamic Crushing of Honeycomb Cellular Meso-Structures

Finite Element Study of Using Concrete Tie Beams to Reduce Differential Settlement Between Footings

Transcription:

Rolling contact stresses between two rigid, axial and flat cylinders Subhankar Das Bakshi Department of Materials Science and Metallurgy, University of Cambridge, U.K. E-mail : sd444@cam.ac.uk/subhankar.dasbakshi@gmail.com Statement of Purpose of the code The code is written to calculate the distribution of forces and stresses during rolling contact of to rigid, parallel and flat cylinders assuming Hertzian contact between the mating surfaces under various conditions of slip. It aims to estimate the magnitude and distribution of normal and tangential forces acting over the Hertzian contact half-width and subsequently calculates the tangential, normal and shear stresses under plane strain condition. A range of stress distribution from perfect rolling to perfect sliding between mating cylinders can be calculated. Distribution of force over the Hertzian contact width The schematic of the twin-disc set up is shown in Fig.. The discs compressed against each other will (a) (b) Figure : Schematic of the (a) twin-disc set up, (b) stress distribution over the Hertzian contact. initially have a straight line of contact having length equal to the thickness of the disc and the width of the one-half of the contact strip is expressed by; b = ν P ( E + E ) π l( R + R ) () where, ν = Poisson s ratio for the materials pressed against each other, P = applied force on the cylinders,

E, E = modulus of elasticity of the materials under compression, R,R = radii of the compressed cylinders, and l = length of cylinders. Under plain strain condition, the normal force distribution, p z (x) and the tangential force distrinution, p x (x) over the Hertzian contact zone (-b x b) is exprressed as ; p z (x) = p n πb b x, x <b, 0, x b, () This gives raise to a parabolic distribution of the normal force over the Hertzian contact width which drops down to zero at both the boundaries. p x (x) = 0, x b, sgn(s ) µpn πb b x, x b, x b + b >b, sgn(s ) µpn [ b πb x b (x b b ) ], x b, x b + b b. (3) where, sgn(s ) = +, fors >0, 0, fors = 0,, fors <0. s is the symbolic variable, µ is the dynamic coefficient of friction, p n is the normal load per unit length (P/l), b is the half-width of the stick zone. The stick-slip ratio, ξ, is defined as the ratio between contact half-width of the stick zone to the Hertzian contact half-width,i.e., ξ = b /b. Now, Integrating eq.3 within the entire contact width (a,-a) results in; b b = p t µp n (4) where p t is the tangential load per unit length. Substituting eq.4 in eq.3; p x (x) = 0, x b, sgn(s ) µpn πb sgn(s ) µpn πb ( x b ), b x<b bξ ( x b ) ξ (ξ + x b ), b bξ x b. normal load per unit contact half-width, p n /b, can be taken as constant for the given pair of rollers and experimental condition. The coefficient of friction, µ during stable rolling/sliding regime are to be considered during calculations. These set of equations are numerically solved by writting a code in C language for various values of ξ and distribution of tangential force, p x (x), and normal force, p x (z) can be calculated. (5) 3 Calculation of stresses in the x-z plane The normal and shear stresses due to the distributed normal and tangential force acting on the Hertzian contact width is expressed as [, ]; σ x (x, z) = z b σ z (x, z) = z3 b p z (s).(x s) [(x s) + z ds b p z (s) z b [(x s) + z ds p x (s).(x s) 3 [(x s) + z ds (6) p x (s).(x s) [(x s) + z ds (7)

τ xz (x, z) = z b p z (s).(x s) z b [(x s) + z ds substituting p z (x), p x (x) and x/b = i, z/b = j and s/b = t; p x (s).(x s) [(x s) + z ds (8) where, σ x (i, j) = 4p n bπ (9) σ z (i, j) = 4p nj bπ (0) τ xz (i, j) = 4p nj bπ () I x = t (i t) [(i t) + j dt, () I x3 (ξ) = I z3 (ξ) = I xz3 (ξ) = I x (ξ) = ξ ξ t (i t) 3 [(i t) + j dt, (3) [ t ξ (ξ + t ) ](i t) 3 I z = I z (ξ) = ξ [(i t) + j dt, (4) t [(i t) + j dt, (5) ξ t (i t) [(i t) + j dt, (6) [ t ξ (ξ + t ) ](i t) [(i t) + j dt, (7) I xz = I xz (ξ) = ξ t (i t) [(i t) + j dt, (8) ξ t (i t) [(i t) + j dt, (9) [ t ξ (ξ + t ) ](i t) [(i t) + j dt, (0) Having calculated σ x, σ z and τ xz, the two principle stresses σ,xz and σ,xz are exprressed as; σ,xz = σ x + σ z σ,xz = σ x + σ z + x σ z σ x σ z σ + τ xz () + τ xz () These set of integrations are numerically solved in a program written in C programming language. 3

4 Input and output parameters A list of input parameters to be called from an input data.txt file are listed below in Table. The list of the output parameters, generated in an output file is listed in Table. Table : List of input parameters for the code. Parameter, unit Poisson s ratio Load, N Overlap length, mm Young s modulus, disc, GPa Young s modulus, disc, GPa Radius, disc, mm Radius, disc, mm Coefficient of friction -(%Slip/00) variable type Table : List of input parameters for the code. Parameter, unit Distance in x-direction, mm Distance in z-direction, mm Tractionals stress, σ x, MPa Tractional force/nornal load, σ x.b/p normal Normal stress, σ z, MPa Normal force/nornal load, σ z.b/p normal Shear stress, τ xz, MPa Shear force/nornal load, τ xz.b/p normal variable type 5 Accuracy limits The stress values are accurate to the errors equivalent to that of the input values. 6 Key words Hertzian contact stress, rolling contact, %slip in rolling/sliding. 7 Sample program To be submitted in a separate ASCII text format. The code has been tested on Windows/Linux/Mac OSx platforms and found to work perfectly. An example of the output of the code, plotted using GNUplot is shown in Fig.. 4

(a) (b) (c) (d) (e) (f) (g) (h) (i) Figure : Calculation of tractional stress σx, normal stress σz and shear stress τxz for l = 5 mm. (a-c) Assuming perfect rolling, (d-f) roll-slide parameter ξ = 0.95, assuming marginal slip, and (g-i) assuming perfect sliding of rolling/sliding cylinders. 5

8 Notification of the use of the code The code has been used and cited in article titled Dry rolling/sliding wear of nanostructured bainite by S. Das Bakshi, A. Leiro, B. Prakash and H. K. D. H. Bhadeshia, submitted in Wear. 6

References [] K. L. Johnson. Contact Mechanics. Cambridge University Press, Cambridge, UK, 985. [] L. WenTao, Y. Zhang, F. ZhiJing, and Z. JingShan. Effects of stick-slip on stress intensity factors for subsurface short cracks in rolling contact. Science China Technological Sciences, 56:43 4, 03. 7