ASYMMETRICAL COLD STRIP ROLLING. A NEW ANALYTICAL APPROACH

Σχετικά έγγραφα
Tutorial Note - Week 09 - Solution

4.2 Differential Equations in Polar Coordinates

e t e r Cylindrical and Spherical Coordinate Representation of grad, div, curl and 2

The Friction Stir Welding Process

Analytical Expression for Hessian

Fundamental Equations of Fluid Mechanics

21. Stresses Around a Hole (I) 21. Stresses Around a Hole (I) I Main Topics

Laplace s Equation in Spherical Polar Coördinates

Space Physics (I) [AP-3044] Lecture 1 by Ling-Hsiao Lyu Oct Lecture 1. Dipole Magnetic Field and Equations of Magnetic Field Lines

Matrix Hartree-Fock Equations for a Closed Shell System

Example 1: THE ELECTRIC DIPOLE

Chapter 7a. Elements of Elasticity, Thermal Stresses

Exercises 10. Find a fundamental matrix of the given system of equations. Also find the fundamental matrix Φ(t) satisfying Φ(0) = I. 1.

Oscillating dipole system Suppose we have two small spheres separated by a distance s. The charge on one sphere changes with time and is described by

1 String with massive end-points

ANSWERSHEET (TOPIC = DIFFERENTIAL CALCULUS) COLLECTION #2. h 0 h h 0 h h 0 ( ) g k = g 0 + g 1 + g g 2009 =?

CHAPTER 25 SOLVING EQUATIONS BY ITERATIVE METHODS

ANTENNAS and WAVE PROPAGATION. Solution Manual

Matrices and Determinants

Curvilinear Systems of Coordinates

Section 8.3 Trigonometric Equations

3.7 Governing Equations and Boundary Conditions for P-Flow

Areas and Lengths in Polar Coordinates

dx x ψ, we should find a similar expression for rθφ L ψ. From L = R P and our knowledge of momentum operators, it follows that + e y z d

Example Sheet 3 Solutions

Homework 8 Model Solution Section

Phys460.nb Solution for the t-dependent Schrodinger s equation How did we find the solution? (not required)

The Laplacian in Spherical Polar Coordinates

Απόκριση σε Μοναδιαία Ωστική Δύναμη (Unit Impulse) Απόκριση σε Δυνάμεις Αυθαίρετα Μεταβαλλόμενες με το Χρόνο. Απόστολος Σ.

Exercise, May 23, 2016: Inflation stabilization with noisy data 1

Homework 3 Solutions

DESIGN OF MACHINERY SOLUTION MANUAL h in h 4 0.

( y) Partial Differential Equations

Strain gauge and rosettes

VEKTORANALYS. CURVILINEAR COORDINATES (kroklinjiga koordinatsytem) Kursvecka 4. Kapitel 10 Sidor

D Alembert s Solution to the Wave Equation

6.3 Forecasting ARMA processes

(a,b) Let s review the general definitions of trig functions first. (See back cover of your book) sin θ = b/r cos θ = a/r tan θ = b/a, a 0

3.4 SUM AND DIFFERENCE FORMULAS. NOTE: cos(α+β) cos α + cos β cos(α-β) cos α -cos β

HOMEWORK 4 = G. In order to plot the stress versus the stretch we define a normalized stretch:

Areas and Lengths in Polar Coordinates

2 Composition. Invertible Mappings

the total number of electrons passing through the lamp.

Derivation of Optical-Bloch Equations

Approximation of distance between locations on earth given by latitude and longitude

Appendix to On the stability of a compressible axisymmetric rotating flow in a pipe. By Z. Rusak & J. H. Lee

[1] P Q. Fig. 3.1

Parametrized Surfaces

STEADY, INVISCID ( potential flow, irrotational) INCOMPRESSIBLE + V Φ + i x. Ψ y = Φ. and. Ψ x

ΑΡΙΘΜΗΤΙΚΗ ΠΡΟΣΟΜΟΙΩΣΗ ΣΥΝΕΚΤΙΚΗΣ ΡΟΗΣ ΜΕ ΕΛΕΥΘΕΡΗ ΕΠΙΦΑΝΕΙΑ ΚΑΤΑ ΤΗ ΙΑ ΟΣΗ ΚΥΜΑΤΩΝ ΠΑΝΩ ΑΠΟ ΠΥΘΜΕΝΑ ΜΕ ΠΤΥΧΩΣΕΙΣ ΠΕΡΙΛΗΨΗ

Spherical Coordinates

Solutions to Exercise Sheet 5

derivation of the Laplacian from rectangular to spherical coordinates

Lecture 26: Circular domains

Second Order Partial Differential Equations

Potential Dividers. 46 minutes. 46 marks. Page 1 of 11

TL-Moments and L-Moments Estimation for the Generalized Pareto Distribution

Inverse trigonometric functions & General Solution of Trigonometric Equations

Concrete Mathematics Exercises from 30 September 2016

Jesse Maassen and Mark Lundstrom Purdue University November 25, 2013

1 3D Helmholtz Equation

Math221: HW# 1 solutions

On a four-dimensional hyperbolic manifold with finite volume

Mock Exam 7. 1 Hong Kong Educational Publishing Company. Section A 1. Reference: HKDSE Math M Q2 (a) (1 + kx) n 1M + 1A = (1) =

Research Article Two-Phase Flow in Wire Coating with Heat Transfer Analysis of an Elastic-Viscous Fluid

Section 8.2 Graphs of Polar Equations

r = x 2 + y 2 and h = z y = r sin sin ϕ

Problems in curvilinear coordinates

Exercises to Statistics of Material Fatigue No. 5

ECE Spring Prof. David R. Jackson ECE Dept. Notes 2

Differentiation exercise show differential equation

Forced Pendulum Numerical approach

Second Order RLC Filters

Section 7.6 Double and Half Angle Formulas

ST5224: Advanced Statistical Theory II

Strain and stress tensors in spherical coordinates

b. Use the parametrization from (a) to compute the area of S a as S a ds. Be sure to substitute for ds!

Answer sheet: Third Midterm for Math 2339

Numerical Analysis FMN011

EE512: Error Control Coding

2. Μηχανικό Μαύρο Κουτί: κύλινδρος με μια μπάλα μέσα σε αυτόν.

Differential equations

Srednicki Chapter 55

Econ 2110: Fall 2008 Suggested Solutions to Problem Set 8 questions or comments to Dan Fetter 1

Partial Differential Equations in Biology The boundary element method. March 26, 2013

( ) ( ) ( ) ( ) ( ) λ = 1 + t t. θ = t ε t. Continuum Mechanics. Chapter 1. Description of Motion dt t. Chapter 2. Deformation and Strain

Theoretical Competition: 12 July 2011 Question 1 Page 1 of 2

Jackson 2.25 Homework Problem Solution Dr. Christopher S. Baird University of Massachusetts Lowell

forms This gives Remark 1. How to remember the above formulas: Substituting these into the equation we obtain with

Problem Set 9 Solutions. θ + 1. θ 2 + cotθ ( ) sinθ e iφ is an eigenfunction of the ˆ L 2 operator. / θ 2. φ 2. sin 2 θ φ 2. ( ) = e iφ. = e iφ cosθ.

Trigonometry 1.TRIGONOMETRIC RATIOS

PARTIAL NOTES for 6.1 Trigonometric Identities

Section 9.2 Polar Equations and Graphs

Written Examination. Antennas and Propagation (AA ) April 26, 2017.

4.6 Autoregressive Moving Average Model ARMA(1,1)

THE BLOWUP OF SOLUTIONS FOR 3-D AXISYMMETRIC COMPRESSIBLE EULER EQUATIONS

Dr. D. Dinev, Department of Structural Mechanics, UACEG

A SIMPLE WAY TO ESTABLISH THE EQUATION OF SHELLS s YIELD SURFACE

Space-Time Symmetries

Uniform Convergence of Fourier Series Michael Taylor

Transcript:

ASYMMETICAL COLD STIP OLLING. A NEW ANALYTICAL APPOACH ODICA IOAN * In this pape is given a solution of asymmetical stip olling poblem using a Bingham type constitutive equation and the petubation method. olling pessue distibution, olling foce, olling toque, font tension, position of neutal points, which ae affected by vaious olling conditions ae analyzed. The influence of the olling speed on the whole pocess was studied using a Bingham type constitutive equation.. INTODUCTION A unifom plastic model of symmetical stip olling in which peipheal velocity and adius of the uppe oll ae equal to those of the lowe oll was poposed by Oowan []. ecently, the symmetical stip olling using a Bingham type constitutive equation and the petubation method was studied by N. Şandu and G. Camenschi [, 3]. Asymmetical olling pocess was used to manufactue plates and sheets. The asymmety is due to the olls with diffeent speeds o with diffeent diametes. This pocess impoves poductivity of the olling opeation-the olling foce, pessue, toque is educing, and the popeties of the stip suface ae impoved. An analytical solution fo asymmetical stip olling pocess was poposed by Y. M. Hwang and G.Y. Tzou, using the slab method [4] and the olling pessue, olling foce and toque wee obtained. In this pape is given a solution of asymmetical stip olling poblem using the method pesented in [, 3].. SOLUTION OF THE POBLEM In ode to solve the poblem of asymmetical stip olling the following assumptions wee made: a the oll is igid; the stip being olled is Bingham type viscoplastic, incompessible mateial; b defomation is plain stain; c the pocess takes place with high speed; * Univesitatea Spiu Haet Bucueşti. ev. oum. Sci. Techn. Mec. Appl., Tome 54, N o, P. 34, Bucaest, 9

odica Ioan d the fictional facto between the oll and the mateial is constant ove the ac of contact; e the flow diection of the stip at the entance and the exit of the oll bite ae hoizontal. ω O δ P P S O θ S α α P P x δ O ω Fig. The geomety of asymmetical cold olling. Fig. is a schematic illustation of the asymmetical stip olling pocess. The viscoplastic defomation egion is bounded by two singula sufaces S and S. This zone is divided in thee egions by the sufaces SN and SN passing though the neutal points N fo the uppe oll, and N fo the lowe oll. The position of the neutal points N, and N and the equation of the sufaces SN and SN will be detemined. Assuming that the angle of stip and the uppe oll between the contact point at the entance in the defomation zone and the contact point at the exit fom it (α, also the adius of the uppe oll (δ ae known, we get the following conditions in ode that the pocess to take place δ = ( ( δsin α δsin α δ sin α, (

3 Asymmetical cold stip olling. A new analytical appoach 3 δ α = acsin sin α δ, which we have fom the geomety of the figue. Equations of the poblem ae a Cauchy equation divt =ρ d v, ( dt b continuity equation Id =, (3 c defomation ate tenso equation T ( d Bingham type constitutive equation d= v v, (4 t I k = p η d, IIt > k, (5 II d In ( (5, t is Cauchy stess tenso, p pessue, η, k mateial constants, d defomation ate tenso, II d the second invaiant of defomation ate tenso, II t the second invaiant of tension tenso deviato, v velocity vecto. Witing equations ( (5 in pola coodinates and tuning them into non dimensional fom by means of the elations =, v = v v, v v v θ =, p p η v = θ. (6 The following dimensionless combinations ae put into evidence Bingham s numbe Bg = k η v, and e = ρ v eynolds numbe. η We shall suppose that e <<, theefoe the inetial tems ae neglected and extending the method used in [] fo the symmetical stip olling, we get (, v k i i O( Bg Ψi θ = Ψ ϕ θ η, (7 whee bi ei Ψi ( θ = aiθ sin θ di cosθ, ( 8

4 odica Ioan 4 and with B i Ei ϕi θ = Aiθ sin θ Di cos θ Ki( θ cos θ Ki( θ sin θ dk θ = fi ( θ sin θ, dθ dk θ = fi ( θ cos θ, dθ (9 dψ i dψ i dfi ( θ d d = θ dθ dθ dθ dψ d Ψ dψ d Ψ d 4 d d 4 θ θ θ dθ i i i i. ( Velocity vecto components ae given by dψi k i i v v = ϕ θ O dθ η vi k θ = ϕ i θ O η ( Bg ( Bg The physical components of the stess tenso ae i vη dψ i ηv t = a d i ci θ dψ i d Fi ( θ C ln k θ ϕ θ A O Bg F ai i θ. i i i,, ( ( ( θ i vη ηv F C tθθ = a c k A ϕ θ O i i ln Bg i i i i ai,

5 Asymmetical cold stip olling. A new analytical appoach 5 with v t = k ϕ θ O i θ dψ i η d Ψ i dθ Bg d i θ Fi ( θ F i i d Ψi dψ θ = dθ 4 dθ. (3 Denoting by X, Y the stess esultants in diections Ox, Oy, acting on a θ α, α, we have suface with the equation = ( θ,, α ( θ cos ( θ θθ sin d, X = t t θ t t θ θ α α ( θ sin ( θ θθ cos d. Y = t t θ t t θ θ α (4 So, we get X j sin α sin α = a 4ηv α α j ( α ( α b j cosαsin α cosαsinα cosαcosα cosαcosα ej cj ( ( α sinα ( α sinα α α ( α α Bg Aj ( α sinα ln α sinα ln (5 ( j B sin sin j C sin sin α α α α 4 α α α α ( α Ej ( ( α α ( α α α I cos cos cos j

6 odica Ioan 6 ( sin F sin F j j a α α α α α α j whee α K α K α, ( jcos jsin I j α aj bjcost-ejsin t = d t, (6 F α j ( t with j =,, 3 placed in egions,, 3 of the defomation zone and the vetical stess esultants is Y cosα cosα = 4η α α j a v b j sin αsinα sinαsinα j ( α ( α sinαcos α sinαcos α ej cj ( ( α cosα ( α cos α α α ( α α Bg -Aj ( α cosα ln α cosα ln ( j B cos cos j C cos cos α α α α 4 α α α α (7 ( α E j ( ( α α ( α α α I sin sin sin j ( cos F cos F j j a α α α α α α j α K α K α, j =,. ( jsin jcos ( N We compute the stess esultants acting on sufaces θ =α, ( α, ( α and we obtain

7 Asymmetical cold stip olling. A new analytical appoach 7 and ( α T = tθ θ=α d = vηψ α δsinα N ( α N k ϕ α α Ψ α δ α N F sin ( α N = tθθ θ=α d = vηa δsin α N ( α N ηv δsinα F α C c ( N k ϕ α N a sin sin δ α δ N α δsinα A ln N ln ( (. (8 (9 3 N. In the same way we compute T, 3 T, T, T, 3 T, N, 3 N, N, N and 3. THE DISCONTINUITY SUFACES Consideing sufaces S and S as singula sufaces fo the velocity and stess field, the dynamical compatibility conditions ae v =, and we shall have [ ] n [ t n ] = kl k ( Ψi, θ vjjsinθ= Ci, i =,. ( We impose that the discontinuity suface S passes though the point P, fo θ=α and we get the equation of suface S b e v a θ α ( sin θ sinα ( cos θ cos α (

8 odica Ioan 8 k ϕ ( θ v ( θ sin θ ( α sin α =. η We impose that the discontinuity suface S passes though the point P, fo θ=α and we get the equation of suface S b e v aθ α ( sin θ sin α ( cos θ cosα k ϕ ( θ v ( θ sin θ ( α sin α =. η (3 On sufaces SN Imposing that the equation of suface and S we have satisfied[ v ] =. N N S suface passes though S N in the fom n ( N, N α α, we will obtain k ϕ ( θ ϕ ( θ =. v Ψ θ Ψ α Ψ3 θ Ψ3 α η N Simila, we get the equation of suface 3 S N k ϕ ( θ ϕ ( θ =. v Ψ θ Ψ α Ψ3 θ Ψ3 α η N 3 (4 (5 4. BOUNDAY CONDITIONS The following conditions will be used: a vi θ (, α =, vi ( θ, α =, i =,3 ; b the discontinuity suface S passes though the point P (also, S passes though the point P ; c we assume that X I =, whee X I = X and X ( α = ( α ( α = ( α II = X ( α = ( α ( α = ( α d the following fiction conditions ae imposed θ=α m II t θ = t θ=α, t θ θ=α = m II t θ=α, 3 3

9 Asymmetical cold stip olling. A new analytical appoach 9 θ θ=α = m II θ=α, t t θ θ= α = m II θ= α, t t obtain 3 3 θ θ= α = m II θ= α, t t e on sufaces S N ( N and N θ θ= α = m II θ= α ; t t S we have [ ] v =, f v ( α, α = ω δ, n X ( N, X 3 N =, v α α = ω δ. Fom condition a we have ϕ ( α =, espectively i i X X 3 N = ; ϕ α = and we A iα Bi sin α Di Ei cos α = [ Kicos α Kicos α ], A iα Bi sin α Di Ei cosα =, i =,3. (6 Imposing that the discontinuity suface S passes though the point P (, = α θ= α, we get v b e ( sin sin a α α α α ( cos α cos α v α sin α α sin α =. Using the continuity equation v= v and sin (7 α α α sin α =, (8 we will have b e a( α α ( sin α sin α ( cos α cosα =. (9 In a simila way, imposing that the discontinuity suface S passes though the point P, we get b e a( α α ( sin α sin α ( cos α cos α =. (3 Fom the fiction condition θ=α m II t θ = t θ=α, we obtain whee so b sin α e cosα = m F α, (3 a b ab cosα a e sinα = F α, (3

odica Ioan m ( bsin α ecosα = m a b e cos α sin α and with the notation m m = γ, (34 we get bsin α ecos α = γ ( a bcos α esin α. (35 We also obtain that with and ( ( α ( α Ψ (33 m ϕ α m ϕ α =, (36 F Ψ m = F ( α α. (37 eplacing (37 in (36, we have ϕ ( α = γϕ( α. (38 Using the expessions of ϕ ( α and ϕ ( α, we get A B ( cos sin E ( sin cos γ γ α α γ α α = = f( α 4 K( γsin α cosα K( sin α γcosα. (39 3 3 Fom fiction condition t θ θ=α = m II t θ=α, we have Aγ B γ cosα sinα E γ sinα cosα = = b sin α e cos α =γ ( a b cos α e sin α 3 3 3 3 3 3 3 Fom the expessions of ϕ ( α and (4 ϕ α = γ ϕ α. (4 3 ϕ α we get 3 A γ B γ cosα sinα E γ sinα cosα = 3 3 3 = f3( α 4 K3( cosα γsinα K3( sinα γcosα. (4 In a simila way, using that θ θ=α = m II t t θ=α, we obtain

Asymmetical cold stip olling. A new analytical appoach bsinα ecosα =γ a bcosα esinα. (43 So, we have bisin α eicos α = γ ( ai bicos α eisin α, i =,3, ϕ i( α = γϕi( α, i =,3 (44 and also b sin α e cos α = γ a b cos α e sin α i i i i i ϕi α = γ ϕ α Fom the condition which means fom whee N N i ( N,, i =,3., i =,3 v α α = ω δ, we get the equation fo N N ( α N (45 k ϕ ( α v ( α Ψ ( α η = ω δ, (46 Bg ω δ ϕ α α α Ψ α =, (47 N N v ωδ ωδ 4Bg v v ϕ α Ψ α Bgϕ ( α α = ( N, Simila, fom condition. (48 v α α = ω δ, we get the equation fo Bg ω δ ϕ α α α Ψ α =, (49 3 N N 3 v

odica Ioan and fom (49 N ωδ ωδ 4Bgϕ3 α Ψ3 α v v Bgϕ 3 ( α α = Using that c X I =, we have cos cos a δ δ b α α δδ δ δ ctgαcos α ctgαcos α c δ δ e = and δ δsinα δ δsinα A sin α ln sin ln α ( ( δ δ B C E sin sin 4 α α δ sin I δ sin F δ α sin F a α α α α δ sinα( Kcosα Ksinα =. Fom condition e, X = X, we get = 3 N δ δ cos α cos α N δδ δ δ a b c e ctgαcos α ctgαcos α = δ δ δ δ cos α cos α N 3 3 3 δδ δ δ a b c e3 ctgαcos α ctgα cos α δ δ and δ δ N sinα δ δ N sinα A sin α ln sin ln α ( ( δ δ B C E sin sin 4 α α. (5 (5 (5 (53 (54

3 Asymmetical cold stip olling. A new analytical appoach 3 δ sin I δ sin F δ α sin F a α α α α δ sin α( Kcos α Ksin α = δ δ N sinα δ δ N sinα = A3 sin α ln sin α ln ( ( δ δ B3 C3 E3 sin sin 4 α α δ sin 3 I δ sin F3 δ α sin F3 a α α α α 3 δ sin α( K3cos α K3sin α. Using that X = X, we obtain 3 N δ δ cos α cos α N δδ δ δ a b c e ctgαcos α ctgα cos α = δ δ δ δ cos α cos α N 3 3 3 δδ δ δ = a b c e3 ctgαcos α ctgαcos α δ δ and δ δ N sinα δ δ N sinα A sin ln sin ln ( ( δ δ B C E sin sin 4 α α δ sin I δ sin F δ α sin F a α α α α δ sin α( Kcos α Ksin α = α α δ δ N sinα δ δ N sinα A3 sin ln sin ln ( ( = α α (56 (57

4 odica Ioan 4 δ δ B3 C3 E3 sin sin 4 α α δ sin 3 I δ sin F3 δ α sin F3 a α α α α 3 δ sinα( K3cosα K3sinα. whee so 5. THE OLLING TOQUES, OLLING STESS AND OLLING PESSUE We will detemine the olling toque M =δ T T T, (58 3 T =Ψ ( α v sin N η δ α Ψ α δsinα N Bg ϕ ( α F, α T 3 =Ψ3 ( α v sin N η δ α Ψ3 ( α δsinα N N Bg ϕ 3( α F3, α T =Ψ α v sin η δ α N Ψ ( α δsinα Bg ( N ϕ α F, α M T T3 T = v ηv δη Also, fo the olling toque of oll we have 3 Total olling toque will have the expession M = M M. (59. (6 M =δ T T T. (6 (6

5 Asymmetical cold stip olling. A new analytical appoach 5 Intoducing the stess II σ X x = (63 and σ = k 3, is the mean yield stess of the mateial we obtain the elative olling y stess the elation ( σ x δ δ cos α cos α = a b( Bg σ δδ δ δ y 3 e ctg αcos α ctg αcos α c ( δ δ sin A sin ln δ α δ α δ sinα C δ α sin ln B (64 δ E δ sin α δ sin α sin α I ( sin F sin F δ α α δ α α a 4 and the olling pessue δsin α( Kcosα Ksin α ( θ ti F θθ i = a Bg 4 ln i c i Ai ϕi θ C i. ηv ai (65 6. NUMEICAL ESULTS AND CONCLUSIONS Wee consideed diffeent cases: A. olls with diffeent diametes (geometical asymmety ; B. olls with same diametes, asymmety given by diffeent oll speed Wee studied diffeent chaacteistics of the asymmetical olling pocess.

6 odica Ioan 6 ( α t, θθ ηv.6.4. V /V = V /V =. olling pessue.8.6.4. V /V =. V /V =.3 5.7 7 9.6 3 4 5.6 Contact length (mm Fig. olling pessue fo vaious ole speed atios when =.5 mm, =.5 mm, α = 3, α =.477, δ = mm, δ = mm, Bg =.5, γ =., γ =.. We obseve that the olling pessue (Fig. in case A and Fig. 3 in case B inceases, with the deceasing of the oll speed atio. When the oll speed atio is the neutal points become a single one. The pocess is taking place in bette conditions when oll speed atio inceases. When the fiction facto atio inceases, the olling pessue inceases (Fig. 4. The olling pessue deceases with inceasing stip speed (Fig. 5. The olling pessue deceases with deceasing of the eduction (Fig. 6. The back foce inceases with the inceasing of the fiction facto; fo γ=.6 7, the back foce is zeo, which allows us to conclude that the pocess is taking place only by means of the fiction foces, without aplling a back foce (Fig. 7. The elative olling stess inceases with the inceasing of the fiction facto and deceases with the inceasing of the oll speed. The back foce deceases with the inceasing of the oll speed atio (Fig. 8. The back foce vetical esultant is small and inceases with the inceasing of the fiction facto (Fig. 9.

7 Asymmetical cold stip olling. A new analytical appoach 7.6.4. V /V = V /V =. V /V =. V /V =.3 olling pessue.8.6.4. 9..37 4 5 7 Contact length (mm Fig. 3 olling pessue fo vaious ole speed atios when =.5 mm, =.75 mm, α = α =.36645, δ = δ = mm, Bg =.3, γ = γ =., V =.9v. olling pessue.5.5 γ /γ =3 γ /γ =.5 4 6 8 Contact length (mm Fig. 4 olling pessue fo vaious fiction factos atios when =.3 mm, =.5 mm, α = 3, α =.38, δ = mm δ = 7 mm, Bg =.8, V =.65v, V =.8v, γ =..

8 odica Ioan 8 ( α t, θθ ηv olling pessue.5.5.5 Bg=.8 Bg=.5 4 6 8 Contact length (mm Fig. 5 olling pessue fo the stip speed when =.3 mm, =.5 mm, α = 3, α =.38, δ = mm, δ = 7 mm, V =.7v, V =.8v, γ =., γ =.. ( α t, θθ ηv olling pessue.5.3..9.7.5.3 =4% =35% 3 4 5 6 7 8 9 Contact length (mm Fig. 6 olling pessue fo vaious eductions when =.5 mm, α = 3, δ = mm, Bg =.5, V =.7v, V =.8v, γ =., γ =..

9 Asymmetical cold stip olling. A new analytical appoach 9 X II 4ηv.4. -. -.4 -.6 -.8 -...3.4.5.6.7.8 γ Fig. 7 The back foce fo fiction facto when =.5 mm, =.75 mm, α = α =.36645, δ = δ = mm, Bg =.3, V =.6v, V =.9v. X II 4ηv -. -.4 -.6 -.8 -. -. -.4...3 -.6 V V Fig. 8 The back foce fo vaious ole speed atios when =.5 mm, =.5 mm, α = 3, α =.477, δ = mm, δ = mm, Bg =.5, γ =., γ =.. The back foce vetical esultant is small and emains constant with the inceasing of the oll speed atio (Fig.. The total olling toque M deceases with the inceasing of the oll speed atio (Fig.. The total olling toque M inceases with the inceasing of the fiction facto (Fig..

3 odica Ioan Y II 4ηv -. -.4 -.63 -.84 -.5 -.6 -.47 -.68 -.89 -....3.4.5.6.7.8 γ Fig. 9 The back foce vetical esultant fo fiction facto when =.5 mm, =.75 mm, α = α =.36645, δ = δ = mm, Bg =.3, V =.6v, V =.9v. Y II 4ηv -.5...3 -. -.5 -. -.5 -.3 V V Fig. The back foce vetical esultant fo vaious oll speed atios when =.5 mm, =.5 mm, α = 3, α =.477, δ = mm, δ = mm, Bg =.5, γ =., γ =. The olling pessue fo the lowe oll is smalle than the olling pessue fo uppe oll in defomation zone III. In zones I and II, they ae pactically, equal (Fig. 3. The neutal point fo uppe oll is moving towads the exit of the viscoplastic defomation zone, when the fiction facto inceases and is moving towads the entance in the viscoplastic defomation zone, when the olling speed inceases (Figs. 4, 5.

Asymmetical cold stip olling. A new analytical appoach 3 The neutal point fo lowe oll has an opposite vaiation then the neutal point fo uppe oll. M M M = δ δ olling toque (M - N-m/mm 4 3 - - -3...3 V V Fig. Vaiation of total olling toque with the oll speed atio when =.5 mm, =.5 mm, η = 3 Nmm - s, k = 4 Nmm -, v = 4 mms -, α = 3, α =.477, δ = mm, δ = mm, Bg =.5, γ =., γ =.. M M M = δ δ olling Toque (M - N-m/mm 4 8 6 4...3.4.5.6.7.8 γ Fig. Vaiation of the elative olling toque vesus fiction facto when =.5 mm, =.75 mm, η = 3 Nmm - s, k = 4 Nmm -, v = 5 mms -, α = α =.36645, δ = δ = mm, Bg =.9, V =.6v, V =.9v. The esults obtained with petubation method ae in good ageement with the esults given in [4], whee the poblem was solved with slab method.

3 odica Ioan ( α tθθ, i ηv 7 6 Uppe ole olling pessue 5 4 3 Lowe ole 9 3 4 5 6 7 8 Contact length (mm Fig. 3 Vaiation of olling pessue fo uppe and lowe oll when X II =, =.5 mm, =.75 mm, α = α =.36645, δ = δ = mm, Bg =.9, V =.6v, V =.9v, γ = γ =.67. N (mm 6 4 Bg=.8 8 Bg=.9 6 4...3.4.5.6.7.8 γ Fig. 4 Vaiation of the position of the neutal point with fiction facto fo diffeent speed atios when =.5 mm, =.75 mm, α = α =.36645, δ = δ = mm, Bg =.3, V =.6v, V =.9v.

3 Asymmetical cold stip olling. A new analytical appoach 33 N (mm...9.8.7.6.5.4.3.. Bg=.9 Bg=.8...3.4.5.6.7.8 γ Fig. 5 Vaiation of the position of the neutal point with fiction facto fo diffeent speed atios when =.5 mm, =.75 mm, α = α =.36645, δ = δ = mm, Bg =.3, V =.6v, V =.9v. N (mm 6 4 8 6 4 N N,,,3,4,5,6,7,8 γ Fig. 6 Vaiation of the position of the neutal points with fiction facto when =.5 mm, =.75 mm, α = α =.36645, δ = δ = mm, Bg =.3, V =.6v, V =.9v. The influence of olling speed on whole pocess was descibed using the Bingham numbe. Until now, using othe methods to solve the asymmetical olling poblem, this influence cannot be descibed. eceived on Mach 3, 5.

34 odica Ioan 4 EFEENCES. E. OOWAN, The Calculation of oll Pessue in Hot and Cold Flat olling, Poc. Inst. Mech. Eng., 5, 943.. N. ŞANDU, G. CAMENSCHI, Contibution to the Mathematical Appoach of the High-Speed Stip olling, Lucăile celei de-a XXV-a CNMS Supl. An. Şt. Univ. Ovidius Constanţa,. 3. N. ŞANDU, G. CAMENSCHI, Asymmetical Binay Stip Dawing, ev. oum. Math. Pues Appl., 46, -3,. 4. Y.M. HWANG, G.Z. TZOU, An Analytical Appoach to Asymmetical Cold Stip olling Using the Slab Method, JMEPEG,, 4, 993. 5. G. CAMENSCHI, N. ŞANDU, Viscoplastic Flow though Inclined Planes with Application to the Stip Dawing, Lett. Appl. Engng. Sci., 7, 979. 6. N. ŞANDU, G. CAMENSCHI, A Mathematical Model of the Stip Dawing Poblem, Bul. Ştiinţific al celei de a XXVI-a Confeinţe Naţionale de Mecanica Solidelo, Băila,. 7. G.Y. TZOU, M.N. HUANG, Study on Minimum Thickness of Asymmetical Cold PV olling of Sheet, Jounal of Mateials Pocessing Technology, 5, 3,. 8. G. CAMENSCHI, Intoducee în mecanica mediilo continue defomabile, Edit. Univesităţii Bucueşti,. 9.. IOAN, O soluţie a poblemei tageii benzilo folosind o teoemă de medie, Buletinul Ştiinţific al Univesităţii din Piteşti, Lucăile celei de-a XXVII-a Confeinţe de Mecanica Solidelo,, 7, 3... IOAN, Global and Local Methods fo Solving Stip Dawing Poblem, in: Topics in Applied Mechanics, vol. I, edited by Vetuia Chioiu and Tudo Sieteanu, Editua Academiei omâne, 3.