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    Tata Steel for

    Company Limited, is the

    annual crude steel capac

    Indian Parsi Businessma

    operating in the year 191

    India in terms of domesti

    Global 500, it is based i

    Group of companies. Tat

    most profitable compan

    place in Indian businessunique concepts like 8-

    system for the first ti

    industrialization process.

    implemented by Tata b

    Indian employees.

    erly known as TISCO and Tata

    world's seventh largest steel c

    ity of 31 million tones. It was es

    Jamsetji Tata in the year 190

    2. It is the largest private sector s

    c production. Currently ranked 4

    Jamshedpur, Jharkhand, India. I

    Steel is also India's second-larg

    in private sector. Tata Steel h

    history, because it has introducour working days, leave with p

    e in India and the first player

    In the later part the concept

    came lawful and compulsory

    Iron and Steel

    mpany with an

    tablished by an

    and it started

    teel company in

    0th on Fortune

    is part of Tata

    st and second-

    lds a very vital

    ed some of theay and pension

    to start rapid

    s invented and

    ractice for the

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    Tata Steel is the largest, flagship company of the Tata Group of

    companies, headquartered in Mumbai, India. Established in 1907, Tata

    Steel is Asia's first and India's largest private sector steel company. Tata

    Steel is among the lowest cost producers of steel in the world and one ofthe few select steel companies in the world that is EVA-positive (Economic

    Value Added). Concerns over the availability of iron ore and coal, and the

    resultant volatility in prices, meant that most Indian steel producers had to

    integrate backwards in order to have greater access and pricing power over

    these commodities. Tata Steel has its own iron ore, coal and chrome mines

    and reserves (on long term leases from the Government of India), andhence is largely self-sufficient in most critical raw materials. Its main plant

    is located in Jamshedpur, Jharkhand, with its recent acquisitions; the

    company has become a multinational with operations in various countries.

    Its captive raw material resources and the state-of-the-art 7 MTPA (million

    tonne per annum) plant at Jamshedpur have given it a competitive edge.

    The Company plans to enhance its capacity, manifold through organic

    growth and investments. Tata Steel's products are targeted at the quality

    conscious auto sector and the burgeoning construction industry. With wire

    manufacturing facilities in India, Sri Lanka and Thailand, the Company

    plans to emerge as a major global player in the wire business. Tata Steel's

    products include hot and cold rolled coils and sheets, galvanized sheets,

    tubes, wire rods, construction rebars, rings and bearings. In an attempt to

    'discommodities' steel, the company has introduced brands like Tata

    Steelium (the world's first branded Cold Rolled Steel), Tata Shakti

    (Galvanized Corrugated Sheets), Tata Tiscon (re-bars), Tata Bearings, Tata

    Agrico (hand tools and implements), Tata Wiron (galvanized wire

    products), Tata Pipes (pipes for construction) and Tata Structural

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    (contemporary construction material). The company has launched the

    Customer Value Management initiative with the objective of creating

    complete understanding of customer problems and finding solutions

    jointly. The company's Retail Value Management addresses the needs ofdistributors, retailers and end consumers. The company has also launched

    India's first steel retail store steel junction - for making steel shopping a

    happy and memorable experience. Tata Steels profitability ranks among

    the best in the industry.

    Apart from the main steel division, Tata Steel's operations are

    grouped under strategic profit centers like tubes, growth shop (for its steel

    plant and material handling equipment), bearings, Ferro alloys and

    minerals, rings, agrico and wires. Tata Steel's products include hot and

    cold rolled coils and sheets, tubes, wire rods, construction bars, structural,

    forging quality steel, rings and bearings.

    Tata Steel has set an ambitious target to achieve a capacity of

    100 million tonne by 2015. Tata Steel is planning a 50-50 balance

    between greenfield facilities and acquisitions.

    Overseas acquisitions have already added up to 21.4

    million tonne, which includes Corus production at 18.2 million tonne,

    Natsteel production at two million tonne and Millennium Steel production

    at 1.2 million tonne. Tata is looking to add another 29 million tonnes

    through the acquisition route.

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    Tata Steel has

    and outside which includ

    1. 6 million

    2. 6.8 millio3. 5 million

    4. 3-million

    5. 2.4-millio

    6. 5 million

    7. 4.5 millio

    Flow

    lined up a series of greenfield

    s:

    onne plant in Orissa (India)

    tonne in Jharkhand (India)onne in Chhattisgarh (India)

    tonne plant in Iran

    n tonne plant in Bangladesh

    onne capacity expansion at Jams

    tonne plant in Vietnam

    iagram 1: TATA Steel Plant Layout

    rojects in India

    edpur

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    Process Fl

    The multiple st

    machines in a steel plant.

    four-high configuration.

    controllers, work roll ben

    present in these complex

    ow Diagram 2: Hot Strip Mill Operation

    and Finishing mill is one of the m

    It consists of 6 or 7tandem stan

    evices such as loopers, automati

    ers, descalers, coilboxes and oth

    machines.

    st productive

    s, each in a

    gauge

    ers areusually

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    Most of the metallic materials produced commercially undergo

    at least one hot deformation stage during their fabrication. Suchprocessing leads to the production of plates, strips, rods, pipes, etc. at

    low cost when compared to the cold deformation / annealing route.

    Comprehensive study of the metallurgical phenomena associated with hot

    deformation has considerable potential application in the control of

    industrial processes. However, investigations in the hot deformation field

    usually require appreciable effort and specialized equipment. The

    temperatures involved for most metals, especially steels, make the directobservation of mechanisms very difficult. Most steels are ferritic at

    ambient temperatures and hot deformation is, by definition, performed in

    the austenite phase. Therefore, study of the metallurgical mechanisms

    taking place during the hot deformation of steels involves a great deal of

    creativity, imagination and hard work.

    The topic selected in this study is the mathematical modeling of

    flow stress and microstructure during the hot strip rolling of steels. This

    includes such microstructural aspects as hardening and softening. Here,

    the niobium microalloyed steels play the main role, but plain C-Mn steels

    are also of interest and a few multiply-alloyed grades as well. Special

    attention is given to the large-scale softening process concurrent with

    deformation known as dynamic recrystallization and its occurrence during

    industrial hot strip rolling. Some laboratory work was also performed in

    this investigation. However, most of the study is based on data supplied

    by TATA STEEL. These data are considered to come from the laboratory of

    "real life" and are analyzed in some detail here.

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    Definition:Definition:Definition:Definition:

    Flow stress is d

    required to continue defo

    The mean flow stress (MF

    strain curve for the strain

    CalculatioCalculatioCalculatioCalculation:n:n:n:With reference

    o and 1 is calculated as

    Fig 1:

    Although the Mstress-strain curves, in w

    integration, the situation

    description of the MFS is

    be required for the rollin

    efined as the instantaneous value

    rming the material - to keep the

    ) is defined as the area under a g

    interval selected.

    to the following figure the MFS b

    follows:

    raphical representation of the MFS.

    FS calculation is fairly simple in tich case numerical methods can

    is different during rolling. A "mec

    ore complex than that describe

    calculations and is described bel

    of stress

    etal flowing.

    iven stress

    tween strains

    e case ofbe used for the

    anical"

    above, but will

    w.

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    Recrystallizatio

    replaced by a new set of

    the original grains have b

    usually accompanied by a

    material and a simultane

    may be introduced as a d

    A precise defin

    is strongly related to sevegrain growth. In some cas

    which one process begins

    recrystallization as: "... th

    deformed material by the

    boundaries driven by the

    boundaries are those with

    process can be differentiaboundaries do not migrat

    only due to the reduction

    during or after deformati

    treatment, for example).

    termed static.

    Fig.2: Recrystallization of a me

    n is a process by which deformed

    ndeformed grains that nucleate a

    en entirely consumed. Recrystalli

    reduction in the strength and ha

    us increase in the ductility. Thus,

    liberate step in metals processin

    ition of recrystallization is difficul

    ral other processes, most notablyes it is difficult to precisely defin

    and another ends. Doherty et al.

    formation of a new grain struct

    formation and migration of high

    stored energy of deformation. Hi

    greater than a 10-15 misorient

    ted from recovery (where high ane) and grain growth (where the dr

    in boundary area). Recrystallizati

    n (during cooling or a subsequen

    he former is termed dynamic whi

    tallic material (a b) and crystal grains

    grains are

    nd grow until

    zation is

    dness of a

    the process

    .

    as the process

    recovery andthe point at

    (1997) defined

    re in a

    ngle grain

    h angle

    tion" Thus the

    le grainiving force is

    n may occur

    t heat

    le the latter is

    growth (b c d).

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    Types of Recrystallization.Types of Recrystallization.Types of Recrystallization.Types of Recrystallization.

    1) Static recrystallization

    2) Dynamic recrystallization

    Static Recrystallization:Static Recrystallization:Static Recrystallization:Static Recrystallization:

    Static recrystallization (SRX) is a softening mechanism that

    occurs commonly during the hot working of steels; this process involves

    the migration of high angle boundaries, which annihilates dislocations and

    releases stored energy in this way. In a HSM, it frequently occurs betweenpasses, after the deformation and during the interpass time. The driving

    force is the energy stored previously in the material in the form of

    dislocations.

    As static recrystallization is a growth transformation its kinetics

    follows the equation given below:-

    X= 1X= 1X= 1X= 1---- exp(exp(exp(exp(----b.tb.tb.tb.tnnnn)))) ---(1)

    WhereX is the fraction transformed,

    b is a constant that depends on the nucleation and growth rates,

    t is the time, and

    n is the time exponent.

    Dynamic RDynamic RDynamic RDynamic Recrystallization:ecrystallization:ecrystallization:ecrystallization:

    If a material is worked, that is, deformed at the same time as it

    is hot, above the recrystallization temperature, the material will not work

    harden, but will recrystallize at the same time it is being worked. This is

    dynamic recrystallization. It is called hot working. In this case hot is

    relative to the recrystallization temperature, not absolute temperature. A

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    metal can be red hot but still be cold worked because it s below its

    recrystallization temperature.

    DRX occur during deformation when the applied strain exceeds

    the critical strain, for the initiation of DRX. At high strain rates, the work

    hardening is "balanced" by the rapid DRX softening that takes place,

    causing a peak (at a strain%),followed by a drop in stress. After a certain

    time (strain), the generation and annihilation of dislocations reach

    equilibrium and the material can be deformed without any further increase

    or decrease in stress; this is referred to as attaining the steady state stress.

    The occurrence of DRX causes large scale and rapid softening.

    When the strain rate is reduced sufficiently, the stress-strain curve

    generally displays a "cyclic" or multiple peak behavior.

    Knowledge of the critical strain for the initiation of dynamic

    recrystallization (DRX) is a requirement for prediction of the operating

    static softening mechanism during a given hot working interpass period in

    this way, the rapid softening and intense grain refinement caused by DRX

    can considerably modify the work hardening, and therefore the load

    behavior in the following pass.

    Metadynamic recrystallization:Metadynamic recrystallization:Metadynamic recrystallization:Metadynamic recrystallization:

    Metadynamic recrystallization (MDRX) basically results from

    continued growth after unloading of the nuclei formed during deformation.

    This situation is generally observed in hot deformation schedules when the

    reductions applied do not reach the steady-state regime, but nevertheless

    attain or exceed the peak strain. Once deformation is interrupted, thenuclei formed dynamically grow statically during the Interpass time. Like

    DRX, MDRX is known to involve rapid kinetics, sometimes attributed to the

    absence of the incubation period normally required for nucleation.

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    Need of modeling:Need of modeling:Need of modeling:Need of modeling:

    BYBYBYBY

    Flow chart 3: Need of MFS modeling

    Thevariation of MFS value from pass to pass describes themicrostructural changes that occur during rolling such as Recystallization

    and Strain accumulation. Knowledge of microstructural changes will be

    helpful in optimizing the passing schedule. By comparing the mean flow

    stresses from strip to strip, the causes to variations in mechanical

    properties between strips may be identified.

    Desired Mechanical

    Properties

    Knowledge of

    Microstructure

    Correlating the

    microstructure with

    Macroscopic changes

    Observation Of

    Microstructure at every

    stand

    MFS measurement by

    MFS models

    Difficult and requires

    time

    Requires

    OR

    By

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    MFS Models:MFS Models:MFS Models:MFS Models:

    Different para

    (i) By Chemistry.(ii) By Rolling Para

    (iii) By Recrystalliz

    Models byModels byModels byModels by Chemistry:Chemistry:Chemistry:Chemistry:

    Table 1 : MF

    eters which can be used for MFS

    eters.

    tion (Static and Dynamic).

    models based on chemistry of steel [2

    modeling are:

    ]

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    Models by Rolling Parameters:Models by Rolling Parameters:Models by Rolling Parameters:Models by Rolling Parameters:[3](i) OROWANS THEORY

    (ii) SIMS THEORY

    (iii) BLAND & FORD THEORY

    (iv) FORD & ALEXANDER

    (v) TSELIKOV

    Orowans TheoryOrowans TheoryOrowans TheoryOrowans Theory:

    The equation developed does not appear to yield analytical

    solution. Alexander gave the complete solution to his equation using

    fourth order R-K method. Due to its complexity and the need for

    numerical integration to describe the non-uniform deformation associated,

    other theories have been proposed. The model assumed variable

    coefficients of friction.

    Sims Theory:Sims Theory:Sims Theory:Sims Theory:

    Sims considered that sticking friction occurs between the work

    roll and the work piece, resulting in a simpler calculation and generation of

    a analytical solution to MFS.

    It is not straight forward or easy to determine the flow stress in

    the roll gap; this is because of the complexity and inhomogeneity of the

    deformation. Numerical methods such as finite elements have been use

    and which can provide a detailed description of the strain distribution.

    However, this method requires long compute times and simple

    "mechanical" methods are desirable in most applications. The first

    complete and comprehensive calculation of the roll pressure distribution

    was described by Orowan. However, due to its complexity and the need

    for numerical integration describe the non uniform deformation

    associated with the assumption of a variable fiction coefficient, other

    theories have been proposed, like the one developed by Sims.

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    Sims' approach

    assumptions to allow for

    integration needed in Or

    action occurs between th

    simpler calculation that i

    each pass requires knowl

    Diameter and rolling forc

    Where P is the roll for

    R is the roll rad

    W is the strip w

    H is the entry t

    H is the exit thi

    Q is a geometri

    Note that the

    units and the factor 2/3

    geometrical factor is calc

    which shows the geometr

    Fig

    for the calculation of roll force a

    an analytical solution of the num

    wan's theory. Also, Sims conside

    e work roll and the Work piece, re

    widely used. Sims calculation o

    edge of the strip width, thickness

    e. The MFS equation is shown bel

    e,

    ius,

    idth

    ickness,

    ckness, and

    cal factor (defined below).

    FS is expressed in equivalent (vo

    is included to allow for plane str

    lated with reference to the follow

    of the roll gap during strip rolli

    : Geometry of strip/roll contact.

    d torque made

    rical

    ed that sticking

    sulting in a

    The MFS in

    , and work roll

    w:

    Mises) stress

    in. The

    ing Figure,

    g.

    --- (2

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    The normal roll pressure s and the yield strength in plane strain

    compression k are related from the neutral point (((() to the exit point ()

    as given by:

    From the roll gap entrance ( = ( = ( = ( = ))))to the neutral point by,,,,

    Where is a generic angle in the working zone. For small

    angles, the differences between normal and vertical roll pressures are

    negligible. Under this assumption, the neutral point angle, , can be

    determined by settingssss = s= s= s= s and rearranging:

    Where

    r is the reduction, defined by: r ==== (H-h)/H....

    The thickness atatatat the neutral point is defined by:

    Geometric factor Q is finally defined by:

    --- (3

    --- (4

    --- (5

    --- (6

    --- (7

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    The Sims model can also use the elastically flattened work rolls

    radius, which is defined by R' according to the relation derived by

    Hitchcock. The flattened Radius R' is given by:

    Where his the height reduction defined by h= (H-h), Pis

    the roll pressure, w is the strip width and C isan elastic term specified by:

    Here is Poisson's ratio and E is Young's modulus for the work

    roll material. The MFS cane now calculated with the aid of main MFSequation.

    A simplification of the Sims model was proposed by Ford and

    Alexander that is sometimes used in on-line models because of its

    computational simplicity. Their Equation for the "mean shear yield stress"

    (MSYS) is shown below:

    Where P is the roll force, H and h arethe entry and exit

    thicknesses, respectively, as before, and R is the work roll radius.

    Note that the Sims approach refers to the von Mises mean flow

    stress, while the F&A method calculate the "mean shear yield stress". Therelation between the Sims von Mises and the F&A MSYS is therefore:

    --- (8

    --- (9

    --- (10

    --- (11

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    Prediction of th

    important tool for the imsimulations. The control

    also important as it is the

    (MFS) and consequently, t

    function of the inverse ab

    the main microstructural

    followed by MDRX, strain

    Knowledge of these eventfor the control of hot stri

    Fig 4: Representation

    e rolling force during finish rollin

    rovement of rolling schedules byf microstructural evolution durin

    key factor that influences the me

    he rolling load. Analysis of the M

    solute temperature can lead to id

    hanges taking place. These inclu

    accumulation, and phase transfor

    s is vital for the development of amill.

    f mfs as a function of inverse absolute t

    is an

    off-linehot rolling is

    n flow stress

    S behavior as a

    ntification of

    e SRX, DRX

    mation.

    ccurate models

    emperature.

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    1)Recrystallization conRecrystallization conRecrystallization conRecrystallization con

    This approach i

    seamless tubes, where th

    . The high rolling temper

    recrystallization to take pl

    are added, during recryst

    schedule,,,, but preventing

    recrystallization is compladded lead to the precipit

    dispersion prevents the o

    conditions are not suited

    mill load limitations mak

    process should be emplo

    to produce relatively fine

    Fig 5

    trolled rolling(RCR)trolled rolling(RCR)trolled rolling(RCR)trolled rolling(RCR)

    s normally used for thick plates a

    rolling loads are near the upper

    tures involved (above 950C)cau

    lace between passes. For this pur

    llization to go to completion all

    raingrowth from taking place w

    te well before the next pass.... Theation of Tin during continuous ca

    currence of extensive grain grow

    to producing the finest grain size

    this approach necessary in some

    ed in association with fast coolin

    erritic grain sizes after transform

    : Recrystallized controlled Rolling

    nd thick-walled

    limit of the mill

    e full

    ose, Ti and V

    long the

    en

    low levels of Tisting. This fine

    th.... These

    ; nevertheless,

    cases.... The RCR

    rates in order

    ation.

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    2)Conventional controller rolling(CCR)Conventional controller rolling(CCR)Conventional controller rolling(CCR)Conventional controller rolling(CCR)

    The main purpose of CCR is to produce a work hardened

    austenite after the last stand in order to increase the number of nucleation

    sites for the austenite-to-ferrite transformation. This leads to production

    of the fullest ferrite grain sizes, improving mechanical properties such as

    the toughness and yield strength. The application of final passes in the

    austenite + ferrite region is sometimes also desired. In this case, the

    transformed ferrite will work harden and the remaining austenite will

    transform to a undeformed ferrite ....Also, the ferrite present at this stage

    leads to lower loads in the mill because it is softer than austenite, thus

    compensating for the load increase associated with the decrease in

    temperature .... The fine microstructures formed in this way are responsible

    for yield strength and toughness improvements in the hot rolled steel.

    This approach generally involves the use of high reheat

    temperatures so as to dissolve the microalloying elements Nb and V

    completely in the austenite. Then, roughing is carried out at temperatures

    above the Tm,,,, allowing full softening between passes and keeping the

    microalloying elements in solution. Finally,,,, finishing is applied to flatten or"pancake" the austenite grains at temperatures below the Tnr. The effect of

    the microalloying element (usually Nb) is crucial here. The solute drag

    acting on the moving grain boundaries and the particle pinning (after the

    precipitation of Nb(C, N) retard or even prevent the occurrence of

    recrystallization. However, in some cases, the strain accumulation caused

    by this process can trigger DRX,,,, followed by metadynamic recrystallization

    (MDRX),,,, leading to rapid softening between passes. In terms ofmathematical modeling, if there is no precipitation and the accumulated

    strain exceeds the critical strain, DRX is initiated, often causing full and

    fast softening.

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    Fig

    3)Dynamic recrystallizDynamic recrystallizDynamic recrystallizDynamic recrystalliz

    This type of pr

    passes during the rolling

    large single strains to th

    methods will allow the to

    initiation of DRX. The for

    temperatures. The latterthe1st passes, after the s

    Some of the benefits of t

    caused by DRX when hig

    applied (single peak beh

    Fig 7: Dyn

    6: Conventional Controlled Rolling

    d controlled rollingd controlled rollingd controlled rollingd controlled rolling

    cess consists of inducing DRX in

    schedule. This can be done eithe

    material or via strain accumulati

    tal strain to exceed the critical str

    mer can be applied in the initial p

    can occur at relatively low tempertrain has accumulated in the prev

    is approach involve the intense

    strain rates are employed and la

    vior in the stress-strain curve)

    mic Recrystallization Controlled Rolling

    one or more

    by applying

    n. Both

    ain for the

    asses at high

    atures, inious passes.

    rain refinement

    rge strains are

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    DATA ANALYSISUsing

    MATLAB

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    The MFS calculation here is done according to Sims model,

    which is mentioned in the section . MFS result from the mentioned model

    is plotted against the 1000/T. However, the derived MFS's are normalized

    because, in strip rolling, the reductions are applied at various strains and

    strain rates; this makes it difficult to compare MFS values from one stand

    to the next. It is therefore useful, to correct those to constant values of

    strain and strain rate by using the expression:

    MFSMFSMFSMFScorrcorrcorrcorr = MFS= MFS= MFS= MFSsimssimssimssims x (0.4/x (0.4/x (0.4/x (0.4/passpasspasspass))))0.210.210.210.21 xxxx (5/(5/(5/(5/passpasspasspass))))0.130.130.130.13

    These exponents 0.21 and 0.13 are strain sensitivity and strain rate

    sensitivity, respectively.

    These values of Simscorr are plotted against the inverse of

    temperature to give the better idea of temperature history dependence of

    the MFS during strip rolling. Normalized MFS is plotted versus 1000/T for

    several strips to determine MFS values in high temperature region, i.e.

    where SRX occurs. Plot is drawn for the MFS values at 6 six passes of

    several slabs of plain carbon steel of grade A12010. All the 6 passes are

    the part of finishing mill in Hot Strip Mill (HSM) and have taken place at 6

    different stands with varying Roll force, Roll Radius and other geometrical

    parameters but most importantly at different strain and strain rates at each

    stand.

    --- (12

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    Fig 8: MFS plots of plain carbon steel: A12010 by Sims and corrected Sims model

    Figure gives the quite clear picture of, role or effect of strain

    and strain rate terms in the calculation of MFS. As the MFS values areinversely proportional to the strain and strain rates, thus MFS by Sims

    corrected formula are lower than those calculate by original Sims model.

    Lines with black color give the average values or the mean trend for the

    variation of MFSsims and MFScorr.

    0.76 0.78 0.8 0.82 0.84 0.86 0.88100

    150

    200

    250

    1000/T (k-1)-->

    M

    F

    S

    (M

    P

    a)--->

    MFS variation with Temperature by Sims' model

    MFS Sims' cor

    MFS Sims'

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    From the figure, it is clear that at higher temperature values or

    for low 1000/T values, MFS values are quite low for both the models. This

    region of lower MFS is said to be region of Static Recrystallization (SRX).

    These zones represents that at high temperature static recrystallization

    takes place in the slab after coming out of stand which softens the steel

    and results into lower values of MFS.

    Examining the above plot, we can clearly see that at first

    pass (high temperature side) there is a low slope region, where SRX

    occurs. The higher temperature permit full softening during the interpass

    time. After pass 2, the lower temperature does not permit full softening,

    leading to the accumulation of some strain. This accumulation then leadsto the onset of DRX (as there is no precipitation). In the above plot we cant

    observe the DRX region clearly this is because, the strain in the slabs in the

    final passes are also not very high. As DRX demands a optimum increase in

    the strain values and in this particular case these values are not reached to

    the level where we can see a great amount of softening due to DRX, but

    still we can see a small decrease in the slope of curve which shows that

    there is some softening occurring at that strain.

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    Original Misaka model for MFS is based on the strain,

    strain rate, temperature of process and chemistry of steel which includes

    only Carbon. This model has no effect of the other constituents of the steelgrade such as Mn, V, Nb, Ti and etc. Several works including Misaka

    himself predicted a multiplying factor to the original Misaka equation to

    consider the strengthening effect of other alloying elements.

    Fig 9: MFS of plain carbon steel A12010 by different models base on chemistry of steel

    0.76 0.77 0.78 0.79 0.8 0.81 0.82 0.83 0.84 0.85

    100

    110

    120

    130

    140

    150

    160

    170

    180

    1000/Temperature (k-1)-->

    M

    FS(

    M

    Pa)-->

    MFS MODELS BASED ON CHEMISTRY OF STEEL

    original Miska

    Misaka et al.

    Minami et al.

    Mirihata et a.

    Poliak et al.

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    Plot of MFS vs. 1000/T is drawn for the different MFS

    models proposed, based on the chemistry of steel for comparing the

    deviation in MFS values. This plot is for the Plain C-Mn steel A12010. Forall models MFS values are quite low for the initial stages where

    temperature is high or the softening range but as the temperature

    decreases we can see the increment in the MFS which may be the result of

    strain accumulation.

    Original Misaka model doesnt consider the effect of other

    alloying elements except C but for other models as Misaka and Poliak do

    consider the solution hardening effect of Mn, Nb, Al and etc. Thus the MFS

    values for these models are greater than those calculated by original

    Misaka model.

    Other models which are showing lower values because they

    have considered the strengthening effect of other alloying elements and

    are not best applicable for the plain C-Mn steel. These models can show

    the better results for more micro alloyed steel grades.

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    As there is no allowance in the original Misaka equation for the

    occurrence of solution strengthening strain accumulation and DRX, whichlead to its deviation from MFS by Sims as these effects cause increase and

    decrease in the MFS respectively. Modifications in this original Misaka

    equation cover the different chemical composition as well as the

    occurrence of DRX. To examine the difference in two models: Sims and

    Misaka, data for steel: A12010 were plotted for MFS by Sims and Misaka

    vs. inverse of temperature.

    Fig 10: Variation of MFS of plain carbon steel A12010 calculated by Sims and Misaka

    0.76 0.77 0.78 0.79 0.8 0.81 0.82 0.83 0.84 0.85110

    120

    130

    140

    150

    160

    170

    180

    190

    200

    210

    1000/T (k-1) -->

    M

    FS

    (M

    P

    a)-

    ->

    VARIATION IN MFS BY SIMS & MISAKA

    0.76 0.77 0.78 0.79 0.8 0.81 0.82 0.83 0.84 0.850

    10

    20

    30

    40

    50

    60

    70

    1000/T (k-1) -->

    errorinM

    P

    a

    -->

    VARIATION OF ERROR

    sims

    Misaka

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    it is apparent from the plot that in the higher temperature

    region or during initial passes, steel slab experiences full softening due to

    SRX, this is the reason why plots or MFS by two models : Sims and Misaka

    are so close. Lower temperature region (final passes) shows the decrease

    in MFS Misaka as it considers the effect of DRX due to high amount of

    strain accumulation during the higher passes.

    However, even the improved Misaka equation is unable to

    specify the MFS behavior in the high slope regions i.e. in the last few

    passes of rolling. This behavior can be attributed to incomplete SRX,

    leading to strain accumulation.

    This variation in the two models can be clearly observed by the

    plot of error against inverse of temperature, which shows that the

    deviation between the two is not much during higher temperature range or

    softening range. Variation of error between the initially increases and then

    decreases when the MFS by Sims decreases due to the strain accumulation

    before the DRX and MDRX occurs and MFS Sims again increase to result

    into higher error in the lower temperature region.

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    (i)(i)(i)(i) Plain Carbon Steel:Plain Carbon Steel:Plain Carbon Steel:Plain Carbon Steel:It is common to find Mn level varying from 0.2 to 1.5 % in plain

    C-Mn steels. Therefore, the solution strengthening effect due to Mn has to

    be taken into account and thus MFS obtained from the Misaka equation

    matches the initial MFS calculation of MFS by Sims model at higher

    temperature range.

    Fig 11: Variation of MFS of plain carbon steel A12010 calculated by Sims and Misaka

    0.76 0.78 0.8 0.82 0.84 0.86 0.88100

    120

    140

    160

    180

    200

    220

    240

    1000/T (k-1)-->

    M

    FS(MP

    a)

    -->

    Sims vs Misaka for Plain Carbon Steel A12010

    MFS Sims' corr

    MFS Misaka

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    (ii)(ii)(ii)(ii) Niobium steelNiobium steelNiobium steelNiobium steel

    Niobium is a very important alloying element because it can not

    only restrain the growth of austenite grain, but also inhibit austenite

    recrystallization, so controlled rolling and controlled cooling technology is

    very effective to increase the strength and toughness of the steels

    containing Niobium [4].

    During hot strip rolling of Nb steels, Nb in solid solution retards

    recrystallization due to solute drag and at lower temperatures strain-

    induced precipitation of Nb(C, N) may occur which effectively retardrecrystallization [4]. Nb impedes the movement of grain and sub grain

    boundaries causing a retardation of recrystallization. The retarding effect

    on recrystallization depends on both Nb in solid solution and on

    precipitated Nb(C, N) [5]. This effect of Nb results into increase in the no

    recrystallization temperature.

    Because of the presence of Nb in the solution leads to the

    retardation of SRX, it has been proposed that DRX also occurring during

    hot strip rolling, particularly in Nb microalloyed steels. The accumulation

    of retained work hardening leading to the initiation of DRX during the hot

    working of Nb steels was first detected in strip mill simulation [4].

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    Fig 12: Variation of MFS of Niobium Steel A19002 calculated by Sims and Misaka model

    MFS values for low carbon Niobium steel: A19002 were plotted

    against inverse of temperature. Plot analysis shows that during early

    passes, MFS values calculated by Sims are not matching with MFS values

    by Misaka, this may be solid solution strengthening effect of Nb present in

    the steel. This deviation is seen to be decreased while MFS values by Simsdecreases during the initial strain accumulation stages.

    In the lower temperature range or final passes we can observe

    the great increase in the MFS by Sims the reason to which may be the

    precipitation of precipitates going to precipitate out at lower temperature

    during last passes.

    0.74 0.76 0.78 0.8 0.82 0.84 0.86 0.88 0.9100

    120

    140

    160

    180

    200

    220

    240

    260

    1000/T (k-1

    )-->

    M

    F

    S

    (M

    P

    a)

    -->

    Sims vs Misaka for Niobium Steel A19002

    ms cor

    MFS Misaka

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    Plain CPlain CPlain CPlain C----Mn steel vsMn steel vsMn steel vsMn steel vs.... Nb micro alloyed steel:Nb micro alloyed steel:Nb micro alloyed steel:Nb micro alloyed steel: A12010 vs.A12010 vs.A12010 vs.A12010 vs. A19002A19002A19002A19002

    Difference in the MFS behavior of steel due to Nb addition

    can be observed by examining the 2 steel grades with almost same

    chemistry except Nb. Thus for this study, plots of steel grades: A12010

    and A19002 are plotted with their MFS values by Sims and Misaka against

    inverse of absolute pass temperature.

    Chemistry of 2 steel grades to be analyzed:

    Steel GradeSteel GradeSteel GradeSteel Grade CCCC MnMnMnMn AlAlAlAl NbNbNbNb VVVV TiTiTiTi CrCrCrCr CuCuCuCu

    A12010A12010A12010A12010 0.1542 0.8297 0.052 0 0 0 0.0217 0.0045

    A19002A19002A19002A19002 0.1479 0.811 0.016 0.0112 0 0 0.0214 0.0038

    Table 2: chemical composition of 2 steel grades: A12010 and A19002

    From the above table it is clear that 2 steel grades to be

    analyzed have almost same chemistry except the Nb content which is nil in

    the A12010 steel grade but there is around 0.0112 wt % of Nb in the Nb

    steel A19002.

    Point on the Sims curve where the curve deviates from a regular

    pattern and the slope increases steeply is known as no recrystallizationpoint and the temperature at this point is mentioned as Tnr. This

    temperature is to be compared for 2 different steel grades. This point

    gives the temperature after which no recrystallization will occur.

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    Fig 13: Comparison of MFS by Sims and Misaka, for Plain Carbon Steel and Niobium Steel.

    0.76 0.78 0.8 0.82 0.84 0.86 0.88100

    120

    140

    160

    180

    200

    220

    240

    1000/T (k-1)-->

    M

    FS

    (M

    Pa)

    -->

    Sims vs Misaka for Plain Carbon Steel A12010

    0.74 0.76 0.78 0.8 0.82 0.84 0.86 0.88 0.9100

    120

    140

    160

    180

    200

    220

    240

    260

    1000/T (k-1

    )-->

    M

    FS

    (M

    Pa)

    -->

    Sims vs Misaka for Niobium Steel A19002

    ms cor

    MFS Misaka

    MFS Sims' corr

    MFS Misaka

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    Examining the above2 plots we can easily make out the

    following points:

    (a) For all the curves of steel: A19002 deviation on the curve for

    steep slope (no recrystallization point) has started at the lower values of(1000/temperature) or at higher temperatures. As it is clear from the plot

    that for plain C-Mn steel no recrystallization point is starting around 0.83

    while for Nb steel it is started around 0.82, this gives the clear cut idea

    that Tnr, increases after the addition to the Nb to the plain C-Mn steel.

    (b) In the softening range, error between the 2 models is less for

    the C-Mn steel as compared to the Nb steel which may be due to solidsolution strengthening of Nb.

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    Effect of Nb addition on

    the recrystallization behavior of plain

    C-Mn steel has been observed in the previous section, this section deals

    with the effect of increasing Nb content in the Nb steel. This effect can be

    examined by considering the different grades of steel with varying Nb

    concentration. Nb steel grades as J10007, E07000 and E08000 are

    considered for this study, for these grades Nb concentration changes from

    0.0075 to 0.0223.

    Steel GradeSteel GradeSteel GradeSteel Grade CCCC MnMnMnMn AlAlAlAl NbNbNbNb VVVV TiTiTiTi CrCrCrCr CuCuCuCu

    J10007J10007J10007 J10007 0.0842 1.063 0.0344 0.0075 0 0 0.0239 0.0047

    E07000E07000E07000E07000 0.071 0.552 0.039 0.0117 0 0 0.025 0.005

    E08000E08000E08000E08000 0.0664 0.901 0.0424 0.0223 0 0 0.0239 0.0045

    Table 3: chemical composition of 3 Nb steel grades

    For the unbiased study of MFS for the above mentioned steel

    grades the slabs to be analyzed should be rolled to the same final

    thickness so that the effect of strain and, strain rates on the MFS

    calculations can be neutralised. Because of this same strain for all the

    slabs varying MFS for the various steel grades depends upon the varying

    Nb concentration. For this purpose the steel slabs data is divided into 3

    categories based on the final thickness of the slab:

    Category 1: 3.64 to 4.04 mm

    Category 2: 4.55 to 4.90 mm

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    Category 1: (3.64mmCategory 1: (3.64mmCategory 1: (3.64mmCategory 1: (3.64mm 4.04mm)4.04mm)4.04mm)4.04mm)

    For this category the final thickness of the slab varies from

    3.64 to 4.04 mm. Data available for this thickness category is just for 2

    steel grades: J10007 and E07000. For each pass, several MFS values are

    available for which average is taken and plotted against the inverse of

    average pass temperature.

    Fig 14: Effect of Increasing content of Nb on MFS and Tnr

    0.77 0.78 0.79 0.8 0.81 0.82 0.83 0.84 0.85100

    120

    140

    160

    180

    200

    220

    1000/T (K-1) -->

    M

    F

    S

    (M

    P

    a

    )

    -->

    EFFECT OF INCREASING NIOBIUM CONTENT

    J10007

    E07000

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    This plot gives the clear idea about the effect of increasing Nb

    content in the steel. MFS values for the Nb rich E07000 steel grade are

    slightly higher in the higher temperature prior to the start of strain

    accumulation; the reason to this is increasing solid solution strengthening

    due to increasing Nb content.

    Apart from the increasing MFS due to increasing Nb content,

    effect on recrystallization is also examined from the above plot. As it was

    mentioned earlier that the presence of Nb resist the austenitic

    recrystallization due to solute drag and at lower temperatures strain-

    induced precipitation of Nb(C,N) may occur which effectively retard

    recrystallization . Nb impedes the movement of grain and sub grain

    boundaries causing a retardation of recrystallization.

    This retardation of recrystallization in the steel can be clearly

    observed by the increase in the recrystallization temperature Tnr in the

    E0700 steel grade, early occurrence of high slope in the MFS curve of

    E07000 steel is proof to this. Thus we can make out that the

    recrystallization stops at higher temperature for steel with more amount ofNb.

    Category 2: (4.55mm to 4.90 mm)Category 2: (4.55mm to 4.90 mm)Category 2: (4.55mm to 4.90 mm)Category 2: (4.55mm to 4.90 mm)

    For this category the final thickness of slab varies from

    4.55mm to 4.90 mm. for this category data is available for all the 3 steelgrades. Average MFS values for each pass is plotted against the inverse of

    average pass temperature.

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    Fig 15: Effect of Increasing content of Nb on MFS and Tnr

    From this plot also above mentioned effect of increasing Nb

    concentration can be seen clearly;

    MFS values increases from minimum for J10007 to the maximum forE08000 and also the stop recrystallization temperature increases with the

    increasing Nb concentration.

    0.77 0.78 0.79 0.8 0.81 0.82 0.83 0.84 0.85100

    150

    200

    250

    1000/T (k-1) -->

    M

    F

    S

    (M

    P

    a)-->

    EFFECT OF INCREASING Nb CONTENT : CATEGORY 2

    J10007

    E07000

    E08000

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    (i)(i)(i)(i) Need of Optimization.Need of Optimization.Need of Optimization.Need of Optimization.

    This part of the paper gives the optimization of models based

    on chemistry of steel such as: Misaka et al., Minami et al., Mirihata et al.,

    Poliak et al., Kang et al. and Bruna et al. to a derive a model similar to

    above mentioned models but having least deviation to the MFS values

    given by Sims model.

    These above mentioned models give the MFS value depending

    upon the Temperature, strain, strain rate and concentration of micro

    allying elements and carbon. However for the same values of above

    mentioned variables also, there is a difference in MFS reading for all

    models and there is an error or deviation to the MFS calculated by Sims

    model. This difference is due to the different coefficients multiplied to theconcentration of different micro alloying elements. For the least deviation

    from practically calculated MFS, these coefficients have to be optimized at

    a particular temperature and rolling parameters for particular steel grade.

    So there is a need of optimized equation based on chemistry of

    steel which may give the least error while calculating the MFS taking MFS

    by Sims model as reference.

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    (ii)(ii)(ii)(ii) General model for MFS based on chemistry of steel:General model for MFS based on chemistry of steel:General model for MFS based on chemistry of steel:General model for MFS based on chemistry of steel:In all models based on chemistry of steel, the original Misaka

    part is multiplied as such and the rest of the part is dependent on micro

    alloying elements concentration. This multiplication factor takes the effectof solid strengthening by micro alloys into account. Coefficients for

    different micro alloying elements is different for all models which have to

    be optimized for getting better approximation and least deviation from

    MFS calculated by Sims model.

    Taking the above concentration into account, we can write the

    general equation for MFS optimized in the following form:

    MFSMFSMFSMFSoptoptoptopt ====[original[original[original[original MisakaMisakaMisakaMisaka]]]] (A+B(A+B(A+B(A+B [Mn]+C[Mn]+C[Mn]+C[Mn]+C [Nb]+D[Nb]+D[Nb]+D[Nb]+D [Al]+E[Al]+E[Al]+E[Al]+E [V])[V])[V])[V]) --(13)

    Thus for getting optimized model for MFS, we have to

    optimized these coefficients (A, B, C, D and E). The optimal values for A, B,

    C and other will result in the least deviation of MFS from MFS practicallycalculated in rolling mill by Sims model. Misaka model is a good

    prediction for C-Mn steel if full SRX occurs in the steel while it has no

    provision for controlling MFS with changing values if strain accumulation

    and DRX occurs there. This variation in the coefficients will help to get the

    close results in the lower temperature or high strain rate range.

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    (iii)(iii)(iii)(iii) Optimization Criterion:Optimization Criterion:Optimization Criterion:Optimization Criterion:

    Optimization is to maximize or minimize some variable

    function which is dependent on one or many independent variables. Thesevalues to be assigned to these variables have some constraints or

    requirements which have to be followed and following these limits only

    independent variables are adjusted to get the optimized results. These

    requirements can be given in the form of equation known as constraint

    equations.

    In this study we have to optimize the MFS model based on

    chemistry to get the close results to MFS by sims model or we can say that

    there is need on minimizing the error between MFS Misaka and MFS Sims .

    This error function can be written as:

    Error= l MFSoptError= l MFSoptError= l MFSoptError= l MFSopt MFS Sims lMFS Sims lMFS Sims lMFS Sims l -------- 14)

    Where MFSopt comes from the equation 2 mentioned above,

    coefficients A, B, C are independent variables which have to be

    optimized to give the minimum error or optimized results. Constraintequations for these coefficients can be derived from the previous MFS

    models designed by Misaka, Minami, Mirihata, Poliak and etc. The value of

    the coefficients in all these models varies within a range. Smallest and

    largest limit is calculated for each coefficient and is considered as the

    constraint equation.

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    (iv)(iv)(iv)(iv) Constraint Equation:Constraint Equation:Constraint Equation:Constraint Equation:

    Analyzing the models we can sort out that the value of all

    coefficients multiplied to micro alloys concentrations vary between certaininterval. Value of coefficients A, B, C, D and E also varies between a certain

    intervals which give constraint equations.

    Constraint Equations:

    1.0.6 A 1.2 ---(15)

    2.0.1 B 0.2 ---(16)

    3.0.5 C 4.54 ---(17)4.0.05 D 0.06 ---(18)

    Where coefficients belong to:

    A Independent

    B Mn

    C Nb

    D Al

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    Optimization Steps:Optimization Steps:Optimization Steps:Optimization Steps:

    Flow chart 4: Optimization steps

    General Equation forGeneral Equation forGeneral Equation forGeneral Equation for

    MFS by chemistryMFS by chemistryMFS by chemistryMFS by chemistry

    MFS by Sims modelMFS by Sims modelMFS by Sims modelMFS by Sims model

    Error functionError functionError functionError function

    formulationformulationformulationformulation

    Constraint EquationsConstraint EquationsConstraint EquationsConstraint Equations

    fcoefficients

    MFS models byMFS models byMFS models byMFS models by

    ChemistryChemistryChemistryChemistry

    Optimized Model ofOptimized Model ofOptimized Model ofOptimized Model of

    MFSMFSMFSMFS

    Data forData forData forData for

    OptimizationOptimizationOptimizationOptimization

    Optimization usingOptimization usingOptimization usingOptimization using

    MATLABMATLABMATLABMATLAB

    OptimizedOptimizedOptimizedOptimized

    coefficientscoefficientscoefficientscoefficients

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    FMINCON finds a constrained minimum of a function of several

    variables. FMINCON attempts to solve problems of the form:

    min F(X) subject to: A X

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    MATLAB PROGRAM FOR OPTIMIZATION:MATLAB PROGRAM FOR OPTIMIZATION:MATLAB PROGRAM FOR OPTIMIZATION:MATLAB PROGRAM FOR OPTIMIZATION:

    clc;clear all;

    C= input (carbon percentage in steel);Mn = input (Mn percentage in steel);Al= input (Al percentage in steel);Cr= input (Cr percentage in steel);Nb= input (Nb percentage in steel);Ti= input (Ti percentage in steel);

    Cu= input (Cu percentage in steel);T= input ('temperature of observations');

    mfscorr= input ('values of MFS by sims corrected');mfsmisakao= input ('values of MFS by Misaka original');

    mfsmisaka= input ('values of MFS by Misaka');observation = (length(mfscorr));for i=1:observation

    x0=[0.6 0.1 0.05 0.5];lb=[0.6 0.1 0.05 0.5];

    ub=[1.2 0.2 0.06 4.54 ];f=@(x) abs(mfscorr(i)-(mfsmisakao(i)*(x(1)+(Mn*x(2))+(x(3)*Al)+(0.128*Cr)+(0.3*Cu));[x]=fmincon(f,x0,[],[],[],[],lb,ub,[])mfsopt(i)=mfsmisakao(i)*(x(1)+(x(2)*Mn)+(x(3)*Al)+(0.128*Cr)+(0.3*Cu)+(x(4)*Nb));

    e(i)=(abs(mfscorr(i)-mfsopt(i)));em(i)=(abs(mfscorr(i)-mfsmisaka(i)));

    t(i)=1000/T(i);

    endj=1;

    l=length(t)for k=1:(l/6)

    for i=1:6MFSmisaka(i)=mfsmisaka(j);

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    MFSopt(i)=mfsopt(j);MFScorr(i)=mfscorr(j);tp(i)=t(j);

    E(i)=e(j);

    Em(i)=em(j);j=j+1;

    endsubplot(1,2,1)

    plot(tp,MFScorr,'g*-');hold on;

    plot(tp,MFSmisaka,'b*-')

    plot(tp,MFSopt,'r*-')xlabel ('1000/T')ylabel ('MFS')subplot(1,2,2)scatter(tp,E,'b')hold on;scatter(tp,Em,'r')

    xlabel ('1000/T')ylabel ('error in MPa')

    end

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    (i)(i)(i)(i) CCCC----Mn steel:Mn steel:Mn steel:Mn steel:For plain carbon steel as A12010, only coefficients A, B and C

    are considered while framing the general equation for MFS in terms ofcomposition of steel. Coefficients attached to Cr and Cu are taken constant

    as there is not much change seen in them while observing the original MFS

    equations.

    Fig 16: MFS Results with minimum error using Optimized model for C-Mn :A12010 steel

    0.76 0.78 0.8 0.82 0.84 0.86 0.88100

    150

    200

    250

    1000/T (k-1

    ) -->

    M

    F

    S

    (M

    P

    a

    )

    -->

    Comparison b/w MFS calculated by Sims,Misaka & Optimized

    0.76 0.78 0.8 0.82 0.84 0.86 0.880

    20

    40

    60

    80

    100

    1000/T (k-1

    ) -->

    e

    rror

    in

    M

    P

    a

    -->

    Error from 2 models : Misaka & Optimized

    MFS opt

    MFS misaka

    MFS sims corr

    5 error b/w MFS sims corr & MFS optimized

    error b/w MFS sims corr & MFS misaka

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    (ii) Nb Steel:While for the case of Nb alloyed steel, coefficient of Nb is varied

    along a long interval as it is done in the original equations. To give better

    results in the lower temperature region, value of coefficient A is variedover a larger range as compared to the previous case of plain carbon steel.

    Fig 17: MFS Results with minimum error using Optimized model for C-Mn :A12010 steel

    In both the cases MFS values from optimized model are very

    close to MFS by Sims resulting into the minimum error, almost zero. For

    most of the portion MFS optimized is just overlapping the MFS Sims

    corrected, except some in the lower temperature.

    0.74 0.76 0.78 0.8 0.82 0.84 0.86 0.88 0.9100

    150

    200

    250

    300

    1000/T (k-1

    ) -->

    M

    F

    S

    (M

    P

    a)-->

    Comparison b/w MFS by Sims, Misaka & optimized

    0.74 0.76 0.78 0.8 0.82 0.84 0.86 0.88 0.90

    50

    100

    150

    1000/T (k-1

    ) -->

    errorin

    M

    P

    a

    -->

    Error from 2 models : Misaka & Optimized

    MFS opt

    MFS misaka

    MFS sims corr

    5 error b/w MFS sims corr & MFS optimized

    error b/w MFS sims corr & MFS misaka

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    Variation of Optimized coefficients:Variation of Optimized coefficients:Variation of Optimized coefficients:Variation of Optimized coefficients:

    As optimization of MFS model is done at each

    temperature, thus we get different optimized coefficients for optimized

    model for every calculation. This variation of coefficients is plotted againstinverse of temperature.

    (i)(i)(i)(i) CCCC----Mn steelMn steelMn steelMn steel

    Fig 18: Variation of coefficients with temperature for Optimized model of C-Mn :A1201

    steel

    0.76 0.78 0.8 0.82 0.84 0.86 0.880

    0.2

    0.4

    0.6

    0.8

    1

    1.2

    1.4

    1000/T (k-1) -->

    coeffici

    ents

    value-->

    Variation of Coefficients

    A: Independent

    B: Mn

    C:Al

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    (ii)(ii)(ii)(ii) Nb microNb microNb microNb micro alloyed steelalloyed steelalloyed steelalloyed steel

    Fig 19 : MFS Results with minimum error using Optimized model for Nb steel: A19002

    For Nb steel extra coefficient D, attached to Nb concentration is

    also plotted. This coefficient is allowed to vary from 0.5 to 5 during the

    optimization process, but its most of the values are varying between the

    interval (1, 2).

    0.74 0.76 0.78 0.8 0.82 0.84 0.86 0.88 0.90

    0.5

    1

    1.5

    2

    2.5

    3

    3.5

    4

    4.5

    5

    1000/T (k

    -1

    ) -->

    coefficients'value

    -->

    Variation of Coeffic ients -->

    A: Independent

    B: Mn

    C: Al

    D: Nb

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    From figure 14 and 15, it can be observed that the Optimized

    coefficients vary with the temperature with a regular pattern. Observing

    this pattern closely, we can find out 2 cluster of variation. For 1000/T

    value less than 0.83, there is a regular variation in value of coefficients but

    for further values, we can observe this variation is following another trend.

    Thus we can find out the 2 different equations for the variation of

    coefficients with varying Temperature.

    MATLAB CodeMATLAB CodeMATLAB CodeMATLAB Code (for A19002 Nb steel):

    clc;clear all;

    C= input (carbon percentage in steel);Mn = input (Mn percentage in steel);

    Al= input (Al percentage in steel);Cr= input (Cr percentage in steel);Nb= input (Nb percentage in steel);

    Ti= input (Ti percentage in steel);Cu= input (Cu percentage in steel);

    T=input('temperature');mfscorr=input('MFS sims corrected');

    mfsmisakao=input('misaka original');mfsmisaka=input('misaka');observation =(length(mfscorr));

    l=1;m=1;for i=1:observationx0=[0.6 0.1 0.001 0.5];lb=[0.6 0.1 0.05 0.5 ];ub=[1.2 0.2 0.06 5];f=@(x) abs(mfscorr(i)-(mfsmisakao(i)*(x(1)+(Mn*x(2))+(x(3)*Al)+(0.128*Cr) +(0.3*Cu)

    +(x(4)*Nb) )));

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    [x]=fmincon(f,x0,[],[],[],[],lb,ub,[])t(i)=1000/T(i);if (t(i)

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    x32=xc32(1).*(t2)+xc32(2);x42=xc42(1).*(t1)+xc42(2);l=1;m=1;

    for i=1:observation

    if (t(i)

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    xlabel ('1000/T')ylabel ('MFS')subplot(2,1,2)

    [tpp,index]=sort(t);

    E1=e(index);plot(tpp,E1,'b')xlabel ('1000/T')ylabel ('error in MPa')

    end

    MATLAB Plots:MATLAB Plots:MATLAB Plots:MATLAB Plots:

    (i)(i)(i)(i) CCCC----Mn steel:Mn steel:Mn steel:Mn steel:

    0.76 0.77 0.78 0.79 0.8 0.81 0.82 0.83 0.84

    0.7

    0.8

    0.9

    1

    1.1

    1.2

    1.3

    1.4

    1.5

    1000/T (k-1)-->

    valueofcoefficientA

    -->

    y = 0.26*x + 0.59 optimized value

    Regression

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    Fig 20: best fit curve for the variation of Coefficient A for C-Mn steel :A12010

    Fig 21: best fit curve for the variation of Coefficient B for C-Mn steel :A12010

    0.83 0.84 0.85 0.86 0.87 0.88 0.89 0.9 0.91

    0.7

    0.8

    0.9

    1

    1.1

    1.2

    1.3

    1.4

    1.5

    1000/T (K-1)-->

    valueofcoe

    fficientA-

    ->

    y = 5.7*x - 3.8 optimized

    Regression

    0.76 0.77 0.78 0.79 0.8 0.81 0.82 0.83 0.840.11

    0.12

    0.13

    0.14

    0.15

    0.16

    0.17

    0.18

    0.19

    0.2

    0.21

    1000/T (k-1)-->

    valueofcoefficientB

    -->

    y = 0.043*x + 0.099 Optimized

    regression

    0.83 0.84 0.85 0.86 0.87 0.88 0.89 0.9 0.91

    0.12

    0.14

    0.16

    0.18

    0.2

    0.22

    1000/T (k-1)-->

    value

    ofcoef

    ficientB

    -->

    y = 0.95*x - 0.64

    Optimized

    Regression

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    Fig 22: best fit curve for the variation of Coefficient C for C-Mn steel :A12010

    Now from the above plots and best fitted equations, we can get

    2 different sets of equations for calculating coefficients to be used for

    calculating MFS by chemistry of steel.

    (i) For (1000/Temperature) < 0.83

    0.76 0.77 0.78 0.79 0.8 0.81 0.82 0.83 0.840.051

    0.052

    0.053

    0.054

    0.055

    0.056

    0.057

    0.058

    0.059

    0.06

    0.061

    1000/T (k-1)-->

    valueofcoefficien

    tC-

    ->

    y = 0.0042*x + 0.05 Optimized

    Regression

    0.83 0.84 0.85 0.86 0.87 0.88 0.89 0.9 0.910.051

    0.052

    0.053

    0.054

    0.055

    0.056

    0.057

    0.058

    0.059

    0.06

    0.061

    1000/T (k-1)-->

    valueofcoe

    fficientC-

    ->

    y = 0.094*x - 0.023

    Optimized

    Regression

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    a. A= 0.26 x (1000/T) +0.59 ---(19)

    b. B= 0.043 x (1000/T) +0.099 ---(20)

    c. C= 0.0042 x (1000/T) +0.05 ---(21)

    (ii) For (1000/Temperature) > 0.83

    a.A= 5.7 x (1000/T) -3.8 ---(22)

    b.B= 0.95 x (1000/T) - 0.64 ---(23)

    c. C= 0.094 x (1000/T) -0.023 ---(24)

    Now these equations are used to calculate the different coefficients at

    different temperature values and are further used to calculate the MFS by

    chemistry of steel. This MFS calculated is examined and plotted against

    inverse of temperature along with the MFS calculated by Sims. Error

    between the 2 MFS is calculated to examine the applicability of these

    coefficients equations.

    MFS model for plain C-Mn steel:

    Temperature > 1200 k

    MFS = Original Misaka x (0.2544 x (1000/T) +0.5913) + (Mn x (0.0424 x

    (1000/T) +0.0986)) + (( 0.0042 x (1000/T) +0.0499) x Al) +

    (0.128Cr) +(0.3Cu) ---(25)

    Temperature < 1200 k

    MFS = Original Misaka x ((5.6823 x (1000/T) -3.8628) + (Mn x (0.9471 x(1000/T) - 0.6438)) + ((0.0937 x (1000/T) -0.0235) x Al) +

    (0.128Cr) + (0.3Cu) ---(26)

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    Fig 23: MFSregression and its deviation from MFS Sims corr for C-Mn steel :A12010

    Above plot gives the MFS (MFSreg) calculated by equation similar

    to Misaka with the coefficients attached to alloying elements

    concentration changing according to the equations (9-14). Analyzing the

    plots we can see that MFSreg is close to the MFSsims almost for all the

    temperature ranges and have maximum error of around 30 MPa which is

    very less as compared to the error between original Misaka and Sims.

    Most importantly it is good observe that the error is almost constant.

    0.76 0.78 0.8 0.82 0.84 0.86 0.88100

    150

    200

    250

    1000/T (k-1) -->

    M

    F

    S

    (M

    Pa

    )-->

    0.76 0.78 0.8 0.82 0.84 0.86 0.880

    10

    20

    30

    40

    1000/T (k-1) -->

    errorin

    M

    P

    a

    -->

    MFS regression

    MFS corr

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    Nb steel:Nb steel:Nb steel:Nb steel:

    Temperature > 1200 k

    MFS = original Misaka ((1.2010 x (1000/T) -0.0603)+( 0.2002 x

    (1000/T) - 0.0101) x Mn +( 0.0198 x (1000/T) +0.0392) x Al )+(12.5494x(1000/T) 8.6947) x Nb ) + (0.128Cr) +(0.3Cu)

    Temperature < 1200 k

    MFS = original Misaka ((3.2843 x (1000/T) -1.6521)+( 0.5473 x

    (1000/T) - 0.2753) x Mn +( 0.0542 x (1000/T) +0.0129) x Al )

    +(55.9623x(1000/T) 43.7398) x Nb ) + (0.128Cr) +(0.3Cu)

    Fig 24: MFSregression and its deviation from MFS Sims corr for Nb steel :A19002

    0.74 0.76 0.78 0.8 0.82 0.84 0.86 0.88 0.9100

    150

    200

    250

    300

    1000/T (k-1) -->

    M

    F

    S

    (M

    P

    a)-->

    0.74 0.76 0.78 0.8 0.82 0.84 0.86 0.88 0.90

    10

    20

    30

    40

    50

    60

    70

    1000/T (k -1) -->

    error

    in

    M

    P

    a

    -->

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    Rolling a new steel grade, will require the first idea of Roll force

    to be used to design a needed Rolling atmosphere and get the desired

    microstructural results. MFS determination is required for this, which can

    be fitted into the Sims equation to find out Roll Force. Misaka equation is

    used for calculating the MFS for these new steel grades using chemical

    composition and absolute rolling temperature. This calculated MFS is then

    back fitted into the MFS equation by Sims to find out the Roll force.

    This section of paper deals with the calculation of Roll force forthe plain C-Mn steel: A12010, using the regressed MFS model developed

    in the previous section and then it is compared with the actual Roll force

    used. Revised Misaka equation used for this calculation is given in 2 parts:

    Equation 1:Equation 1:Equation 1:Equation 1: Temperature > 1200 k

    MFS = Original Misaka x (0.2544 x (1000/T) +0.5913) + (Mn x (0.0424 x(1000/T) +0.0986)) + (( 0.0042 x (1000/T) +0.0499) x Al) +

    (0.128Cr) +(0.3Cu) ---(27)

    Equation 2Equation 2Equation 2Equation 2: Temperature < 1200 k

    MFS = Original Misaka x ((5.6823 x (1000/T) -3.8628) + (Mn x (0.9471 x

    (1000/T) - 0.6438)) + ((0.0937 x (1000/T) -0.0235) x Al) +(0.128Cr) +(0.3Cu) ---(28)

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    Observation Table:Observation Table:Observation Table:Observation Table:

    slab

    num.

    Temperature Eq.

    applied

    MFS by revised

    Misaka

    Roll Force

    Calculated

    Actual

    Roll

    Force

    Error

    1 1309.65 1 118.833079 11.3577956 12.46 1.1022041 1286.81 1 126.784033 10.78515625 12.51 1.72484375

    1 1263.63 1 140.614695 10.02162208 10.72 0.69837792

    1 1238.4 1 146.494352 8.597858288 10.48 1.88214172

    1 1210.93 1 147.225849 6.152436363 8.18 2.02756364

    1 1181.26 2 172.087169 5.603219072 6.02 0.41678093

    2 1272.03 1 117.868809 15.41418188 19.3 3.88581812

    2 1244.71 1 129.832289 14.46243003 18.49 4.0275698

    2 1225.01 1 143.148339 14.11343195 16.64 2.52656806

    2 1204.59 1 148.747126 11.67224689 15.15 3.477753112 1180.81 2 177.169622 9.817497289 10.86 1.0425027

    2 1154.27 2 192.545211 8.384089983 8.08 -0.30409

    3 1282.43 1 119.482278 16.0739462 17.78 1.7060538

    3 1255.09 1 130.711243 14.65671889 18.52 3.86328111

    3 1235.09 1 142.70511 13.90773395 16.76 2.8522660

    3 1214.34 1 154.869648 12.42278094 14.91 2.48721907

    3 1190.32 2 173.113607 9.6755656 10.83 1.1544344

    3 1163.68 2 193.670212 8.684389174 8.85 0.16561083

    4 1289.97 1 114.245007 15.19473976 17.51 2.315260244 1262.95 1 121.495359 12.96557069 17.63 4.66442930

    4 1242.6 1 137.219763 13.03110823 16.16 3.12889177

    4 1221.37 1 144.801179 11.26494867 13.78 2.51505133

    4 1197.25 2 160.967859 9.04890326 11.1 2.0510967

    4 1170.61 2 178.755311 8.14263722 9.03 0.8873628

    5 1280.55 1 120.6052025 12.52551539 14.28 1.7544842

    5 1256.18 1 128.7370189 10.38804408 13.06 2.6719552

    5 1242.74 1 141.7723088 9.928720039 11.15 1.22127991

    5 1228.04 1 150.9967475 8.768288437 10.79 2.021711565 1209.41 1 149.3410288 6.314884225 8.94 2.62511577

    5 1187.71 2 170.6318812 5.732091519 7.09 1.35790848

    Table 4: Roll Force by Revised Misaka and error from the actual

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    While the slab enters the finishing mill in the stand one,

    temperature of slab is very well known to us but after that we just calculate

    the temperature of slab according to the model proposed and finally when

    the slab comes out of the last stand, we can measure its temperature. This

    knowledge of temperature after last stand is very important and it should

    be very close to the upper critical temperature (Ar3) temperature for the

    steel grade.

    As the transformation of steel microstructure takes place onlywhen the steel is cooled below Ar3, prior to the attainment of this

    temperature steel slab is just cooled to bring down the temperature which

    just a waste of energy. If the temperature variation between the stands is

    controlled such that the final temperature of the slab coming out of

    finishing mill is having the temperature almost very close to Ar3 then this is

    the most productive condition with least energy wastage. Energy savings

    are mostly due to the controlled heating of slab before it enters thefinishing mill which is adjusted in such a way that the temperature of slab

    finally coming out of finishing mill is very close to Ar3 temperature.

    For this a model or equation is to be formed for the calculation

    of decrease in temperature from stand to stand which depends upon the

    various variable and constant parameters. The parameters which will

    control this temperature decrement are:

    (a)Strain rate:Strain rate:Strain rate:Strain rate: the strain induced in the slab during the pass at

    particular stand and the time required for this deformation both are

    used for the determination of this temperature decrement. These

    both the parameters are very well covered by a single parameter i.e.

    strain rate.

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    (b)Residence time:Residence time:Residence time:Residence time: Interstand residence time which represents the time

    interval for open exposure to the coil between the 2 stand rolls. This

    really controls the temperature loss as more the residence time, more

    will be the temperature decrement.

    (c)Initial temperature:Initial temperature:Initial temperature:Initial temperature: Initial temperature of the slab before entering

    into the stand decides the rate of temperature loss as more the

    temperature difference b/w slab and atmosphere higher will be the

    rate of heat transfer from slab to open atmosphere.

    (d)(d)(d)(d)WidWidWidWidth/ thickness ratio:th/ thickness ratio:th/ thickness ratio:th/ thickness ratio: Ratio is directly related to the ease ofradiating heat from the slab as more the surface area more easy will

    be the temperature reduction while it is inversely proportional to the

    volume or thickness of slab.

    (e) Interstand coolingInterstand coolingInterstand coolingInterstand cooling : between all the stands, cooling is provided using

    the water sprays which can be very important parameter for the

    decrease in the temperature of slab between the 2stands.

    (f)Coefficient of thermal conductivity of steel slabCoefficient of thermal conductivity of steel slabCoefficient of thermal conductivity of steel slabCoefficient of thermal conductivity of steel slab: this is a constant

    quantity for a particular steel grade and describes the rate of heat

    transfer from the metal slab to the rolling machinery.

    Last parameter with several other parameters such as specific

    heat of rolling machinery and etc can be taken as constant values as these

    values do not change for a rolling process of one steel grade. Interstand

    cooling rate can be variable from stand to stand but can be taken as a

    constant for the cooling between particular 2 stands.

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    Considering above parameters a general equation for the

    temperature decrement between two stands can be given as:

    T = aT = aT = aT = a + b+ b+ b+ b ttttresresresres + c+ c+ c+ c TTTT1111 + d+ d+ d+ d (W/H) +eW/H) +eW/H) +eW/H) +e ---(29)

    Where:

    : Strain rate

    Tres : Residence time between two stands

    T1 : Initial temperature of slab

    (W/H) : Width / average thickness ratio.

    The regression of the provided data to find out the coefficients

    a, b, c, d and e is done by using MATLAB with the help of function regressregressregressregress

    , the MATLAB code to this problem is:

    MATLAB Program:

    clc;clear all;for i=1:5

    Tenter= input ('value of temperature of slabs on entering into stand');Texit= input ('value of temperature of slabs on exit out of stand');tt=(Tenter-Texit);

    sr= input ('value of strain rates at stand');restime= input ('value of Residence time between stand 1 & stand 2');

    wh= input ('ratio of width to thickness for slabs considered')if i==1

    [X]=[ones(length(tt),1),(sr)',(restime)',(Tenter)',(wh)'];[c,ibeta,res,Ires,stats]=regress(tt',X,0.05)treg=c(1)+(c(2).*sr)+(c(3).*restime)+(c(4).*Tenter)+(c(5).*wh);

    else[X]=[ones(length(tt),1),(sr)',(restime)',(Tenter)',(wh)',t'];[c,ibeta,res,Ires,stats]=regress(tt',X,0.05)

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    treg=c(1)+(c(2).*sr)+(c(3).*restime)+(c(4).*Tenter)+(c(5).*wh)+(c(6).*t);endsubplot(1,2,1)

    scatter(tt,treg,'filled')

    hold on;t=tt;plot(t,tt)ylabel( 'Temperature difference by regression model')

    xlabel('actual Temperature difference')subplot(1,2,2)

    rcoplot(res,Ires)

    pauseend

    data for temperature decrement between the first two rolls of

    the finishing mill is used to find the regression model to keep the

    interstand cooling rate constant. The data includes the rolling of 29 slabs

    of plain C-Mn steel: A12010 between first two stands.

    Regression results and plot:Regression results and plot:Regression results and plot:Regression results and plot:

    (i)(i)(i)(i) CCCC----Mn steel : pass1Mn steel : pass1Mn steel : pass1Mn steel : pass1 Regression ResultRegression ResultRegression ResultRegression ResultEquation formed for the calculation of temperature decrement

    of Plain carbon steel between first two stand is:

    T = -(1.0946 )-(4.1458 tres) +(0.0966 T1)+(0.8646x (W/H))

    -113.8650 ---(30)

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    PLOT:PLOT:PLOT:PLOT:

    Fig 25: temperature decrement b/w stand 1 and stand 2 for A12010 by regression model

    The plot shows the scattered points which represents the

    temperature decrement between stand 1and 2 calculated by regression

    model formed after regression. The plot present on the right side gives the

    residuals between the regressed data and the actual data. The lines with

    the green are representing that the regression is having 95% confidencelimit while the red one is outside this limit. As most of the data is lying

    inside 95 % confidence limit thus the proposed model is quite acceptable.

    15 20 25 30 3515

    20

    25

    30

    35

    T

    em

    perature

    difference

    by

    regression

    m

    odel

    actual Temperature difference5 10 15 20 25

    -6

    -4

    -2

    0

    2

    4

    6

    8

    10

    Residual Case Order Plot

    R

    esiduals

    Case Number

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    (ii)(ii)(ii)(ii) CCCC----Mn steel : Pass 2Mn steel : Pass 2Mn steel : Pass 2Mn steel : Pass 2 Regression ResultRegression ResultRegression ResultRegression ResultAs the regression equation for the temperature decrement has

    been calculated for pass 1, the next step is the temperature decrement

    equation for further passes in the finishing mill. For this calculation,temperature decrement in the previous stand is also taken as the judging

    parameter for the calculation of temperature decrement. Thus the general

    equation for this decrement can be written as:

    T = a + b tres + c T1 + d (W/H) +e (T) +f ---(31)

    Where T is temperature decrement in the previous stand.

    EquationEquationEquationEquation::::

    T = -(0.0262 ) - (0.6641 tres )+ (0.1180 T1 )+ ( 0.1344 (W/H)

    + (0.1347 xT) -139.2790 ---(32)

    PlotPlotPlotPlot::::

    Fig 26: temperature decrement b/w stand 2 and stand 3 for A12010 by regression model

    12 14 16 18 20 22 2412

    14

    16

    18

    20

    22

    24

    Tem

    peraturedifferenceby

    regressionm

    ode

    l

    actual Temperature difference5 10 15 20 25

    -5

    -4

    -3

    -2

    -1

    0

    1

    2

    3

    4

    5

    Residual Case Order Plot

    R

    esiduals

    Case Number

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    (iii)(iii)(iii)(iii) CCCC----Mn steel : Pass 3Mn steel : Pass 3Mn steel : Pass 3Mn steel : Pass 3 Regression resultRegression resultRegression resultRegression resultEquationEquationEquationEquation

    T = -( 0.0917

    ) - (2.5864

    tres )+ (0.0046

    T1 ) - (0.0774

    (W/H)+ ( 1.0129 xT) +11.2039 ---(33)

    Plots:Plots:Plots:Plots:

    Fig 27: temperature decrement b/w stand 3 and stand 4 for A12010 by regression model

    14 16 18 20 22 24 2614

    16

    18

    20

    22

    24

    26

    28

    T

    em

    pera

    ture

    difference

    by

    regressio

    n

    m

    odel

    actual Temperature difference5 10 15 20 25

    -2

    -1.5

    -1

    -0.5

    0

    0.5

    1

    1.5

    2

    Residual Case Order Plot

    R

    esiduals

    Case Number

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    (iv)(iv)(iv)(iv) CCCC----Mn steel : Pass 4 Regression resulMn steel : Pass 4 Regression resulMn steel : Pass 4 Regression resulMn steel : Pass 4 Regression resulttttEquationEquationEquationEquation

    T = -( 0.0707

    ) - (2.4051

    tres ) + (0.0159

    T1 ) - (0.0007

    (W/H)+ (0.8960) x T) -7.2319 ---(34)

    PlotsPlotsPlotsPlots

    Fig 28: temperature decrement b/w stand 4 and stand 5 for A12010 by regression mode

    18 20 22 24 26 28 3018

    20

    22

    24

    26

    28

    30

    Tem

    peraturedifferenceby

    regressionmo

    del-->

    Actual Temperature difference -->5 10 15 20 25

    -1.5

    -1

    -0.5

    0

    0.5

    1

    Residual Case Order Plot

    R

    esiduals

    -->

    Case Number -->

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    (v)(v)(v)(v) CCCC----Mn steel : Pass 5Mn steel : Pass 5Mn steel : Pass 5Mn steel : Pass 5 :::: Regression resultRegression resultRegression resultRegression resultEquationEquationEquationEquation

    T = -( 0.0171

    ) - (0.9302

    tres ) - (0.0076

    T1 ) +( 0.0132

    (W/H))+ ( 0.8455 x T) + 14.9623 ---(35)

    PlotPlotPlotPlot

    Fig 29: temperature decrement b/w stand 5 and stand 6 for A12010 by regression model

    21 22 23 24 25 26 27 28 29 30 3121

    22

    23

    24

    25

    26

    27

    28

    29

    30

    31

    Tem

    peraturedifferenceby

    regressionm

    odel

    actual Temperature difference

    5 10 15 20 25

    -0.4

    -0.2

    0

    0.2

    0.4

    0.6

    0.8

    Residual Case Order Plot

    R

    esiduals

    Case Number

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    OUTPUT TABLE:OUTPUT TABLE:OUTPUT TABLE:OUTPUT TABLE:

    Slab

    number

    Temperature decrements

    Stand 1 to stand 2 Stand 2 to stand 3 Stand 3 to stand 4

    Actual By

    regression

    Actual By

    Regression

    Actual BY

    regression

    1 16.91 16.32 17.7 17.41 18.71 18.45

    2 17.4 16.96 19.13 18.53 20.75 20.99

    3 20.54 18.55 20.06 20.23 22.51 21.75

    4 23.73 25.55 20.35 21.51 23.84 24.06

    5 28.49 28.25 23.09 21.6 25.19 26.1

    Table 5: Temperature decrement for slab of A12010 stand by stand

    Slab

    number

    Temperature decrements

    Stand 4 to stand 5 Stand 5 to stand 6

    Actual By

    regression

    Actual By

    Regression

    1 23.07 23.14 25.02 25.02

    2 24.21 24.44 26.71 27.433 25.43 24.9 27.23 27.23

    4 25.94 25.94 30.78 30.78

    5 27.22 27.47 29.67 28.98

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    All mathematical models based on chemical composition of

    steel and Rolling parameters for predicting MFS were compiled. Plant datafrom the HSM section of TATA STEEL was taken and then analyzed and

    statistically operated to draw out the following conclusions:

    1.MFS models by Sims and Misaka were compared for different

    temperature range and passes , both the models are very close to

    each other in the softening or high temperature range while there is

    large deviation between the two in the lower temperature region

    during final passes.

    2.Effect of Nb microalloying on the MFS values of different steel grades

    was studied and found that there is increase in the MFS values on Nb

    addition due to its solution strengthening effect. Variation in the no

    Recrystallization temperature was also observed which is increased asthe Nb concentration increases through the different grades.

    3.Misaka model was optimized using MATLAB programming close to

    the MFS values by Sims model resulting into varying optimized

    equations from temperature to temperature to give excellent

    prediction of MFS. Values of coefficients attached MFS model bychemistry can be observed varying over a temperature range.

    4.Variation of these coefficients was observed to be 2 clusters in the

    whole temperature range during rolling operation. Thus this variation

    is tried to be best fitted by using a linear relation of these coefficients

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    with temperature. 2 equations for each coefficient is formed in the

    two temperature range ( 1200 k) which are finally

    collected together to give the final equation to predict MFS. MFS

    results from this revised equation are finally compared to the MFS bySims and found that the error is constant throughout the Rolling

    process and reaches maximum to around 30-35 MPa which is quite

    acceptable as compared to error between Misaka and Sims which

    goes up to 80-90 MPa.

    5.Roll Force is calculated by putting MFS calculated from the revisedEquation in the Sims formula. This Roll force is then finally compared

    with the actual Roll force used during the process and found that

    error is maximum during the middle passes (pass 3 or Pass 4) while

    during early and final passes, error is maximum to 1 kilo tone.

    6.Readings of temperature decrements through the Rolling stands in

    finishing mill are finally regressed taking Strain rate, width by height

    ratio for slab, residence time between the 2 stands and initial

    temperature of slab as the controlling parameters. Results shows that

    the regression model grows more accurate and more predictable if

    we consider the temperature decrement in the previous stand also as

    a controlling parameter.

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    [1] Folio Sicilian Jr. Thesis on Mathematical Modeling of the Hot Strip

    Rolling of Nb Microalloyed Steels, 1999, p. 1-63.[2] Folio Sicilian, Oswald Marini, Roberto G. Bruna, p.3.

    [3] L. Petty KARJALAINEN, T. Terrence, M. MACCAGNO and John J. JONAS,

    1995, p .3.

    [4] Linda Lasses, Groan Newberg and Ulrika Berggren, 1996, p.7.

    [5] Ningbo Yu, Shandong Wang, Xinhua Liu and Gooding Wang, Materials

    and Science Engineering , 2004, p.1.

    [6] M. Piertrzyk, John G. Lenard, Thermal-Mechanical Modelling of theFlat Rolling Process, 1991, p.53-63.

    [7] www.wikipedia.org

    [8] www.tatasteel.com