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    IGATE  1998

    CHEMIC L ENGINEERING

    SECTION

    A

    ONE

    MARKS QUESTIONS (1-25)

    Write.

    in

    t

    he

    boxes provided ln your Mswer

    (boxes I to 2,5) the most appropriate

    ans\1

    ar to the

    followtng 111ultlp le choice questions

    by

    wri ting the

    letters - A B, C or 0 - agmnsl subqu

    es ti

    on

    Jtumber. (25 x i

    :

    25

    t

    lJ

    Mks)

    I. '11\e transform

    of

    Function

    e   '

    has

    the form ·

    3.

    4,

    I

    c.

    I

    d. f +

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    I() A globe voh'c is most fQr

    llpplieahon

    ;;

    In

    wh1w l l < > ~ r o l is requU:ecl,

    c,

    th

    e

    nllid co

    nlnin

    • d f ~ r t n c l ~ .

    d.

    {)tl: -\1

    uy n

    uw s roq,llircd.

    U The hydraulic r o d i ~ U l(lr now in o

    rectansula•

    l

    ho

    ct

    of c r o ~ t o n a J

    ~ II. w

    o$

    ~ f ?

    W

    h

    l l l •W)

    Hll')'

    0.

    4

    (1-1

    •W)

    u rn 

    d.

    (ff +

    W)

    1 2.

    ln e work ind

    e:<

    in Bond·, l•w for crushing

    of

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    K(s · l) will hove a

    8

    (28

    - l}(: s i 1)

    dofina

    nnmbor variation of K

    fmm

    0

    In

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    42

    45 

    b. Inn

    er ~ o l y •

    oore vf rndi

    us l t

    2 doe1

    n

    ot

    participate fn reaction

    c. I

    nn

    er c.ore llf radius

    1R

    '8 l.l(>cs

    nut

    pnrtic i

    patc in

    cl F.llec

    ti

    vene.• foctur t w

    zero Q

    rd

    er

    ltl:tction cnnn c1t he 711 >S

    it

    mlll\1

    lllwav

    l be

    I,

    t

    dC I bring about uamain ehans.:

    in the l bte

    }'j;te.m omi CI' adiab

    :tt

    ie

    l

    undi l

    in

    ut-.

    : 'r

    he :1lllO

    Unl

    o f wo

    rk is

    palh

    deren

    dent.

    h Work alone .:.>nll ll bring ab11ui such. a

    clutn

    ge

    n lat.,,

    c. '

    lb

    c nmouot or " 'o

    rk

    needed

    i•

    independent o poth.

    d.

    o

    uuouuatluu is nooded to

    anything Jboul tho path

    or

    O

    berwise

    of

    the wo

    rt<

    tteeded,

    l f

    U1

    e beat of

    1o

    lu

    lio

    n of n id

    l. r'

    2.$

    tJrvt

    lose<

    l to "

    (to mt.,gral

    with

    I e r

    fu

    ij

    cliop-

    1

    - , When

    ;s

    a step clranllc

    rn

    set point Is •pplicd to s uch

    a do.sed loop

    ;-ys

    tem,

    th

    e co

    nt

    ro

    ll

    ed

    vatia

    bl

    e

    wi

    th

    ex

    lc

    iliil

    a. 6vc

    rdaJn

    ped

    r""pn

    ns

    e

    b.

    Ll

    nd

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    11

    only i f

    UlC r.pening is on lite p h e r i

    ves>el.

    b. unly ir the

    i" 11n

    ve.tiCill

    .,yliudric;, l vcssu

    l.

    c,

    only

    i f ite opening is

    on •

    n l l ~ c m t r t l

    cyl

    in

    (lric3

    l

    \1\:sij¢

    \.

    tL irrc:sp J V c : b ~ c of moderAte

    helghl.

    the weld

    joint t f r c t e n e y t or

    join

    iS

    p ~ m l l e l

    to the

    cylinder is

    si"e"

    as 1.0

    "hilc li '

    joinl• nloug tloc

    irth

    ( c i r c

    u m f

    ~ : r e n c c )

    i t

    is given

    liS

    0.8. l l i

    calculating the

    shell wall i c k n e s s

    u. I(Unntit

    )'

    uf J)urc ntllk.'YS""

    to

    he u J > J l l . i e < ~ in

    kglh,

    in

    stcody

    S

    lat

    e

    Qp er ill inn

    .

    (iii

    Draw •

    t Coat blocl.. diaJ ,r•m h o w i n ~ t

    tho- t llljor

    units,

    iltJW& an d c o m o ~ i t i o n s .

    nnd

    jndicote

    the e n v e ~ c

    bO\Indar

    y

    ~ t r o u which the ,quisitc

    mollS balnncc:(s

    )

    I

    arc bcinS

    mode.

    ·

    n,

    e

    elevant

    rooctlun

    il

    rcptC.1ent

    cd

    by

    K':..t t.; • a, •

    2c,u .

    o

    (g) (g) (g)

    IAl>swnc

    a

    tmtLi

    c m•sses

    os:

    C - 1

    2,0 ~ J.

    a. Ohu in an expression for

    U1

    e pres•ure

    drop

    on

    the pipe (

    \P

    } In lenns

    of

    the

    1

    ulurue llow rnte I()

    }.

    b.

    Obtain an ex prcfisioo

    Jbr the sh:ody

    opcratlng

    now

    rote

    in

    tbe sy•

    t"111,

    llSs

    um

    in9 t

    hn

    t

    th

    e only pressure h•

    ss ln

    llt

    csyst

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      .

    I>S.

    67.

    The rndin•

    of th

    e

    jet

    far

    from

    the

    ~ l a g n n t i

    j)Otnl

    (0) is

    11. :md the ~ i t y

    is

    u. A s . ~ u m Ut

    e lluw

    Ill

    be

    find

    l l ~ i s y n u u o t

    r k , and ncijlccl grav

    it

    y. Also

    " " ~ ' " 1 1 " tluu

    the w l

    oo

    it

    y

    prqfil

    es •1" Ant

    (iotirom

    th

    e

    n u t i < p ~ ~ i n L

    fhe

    presl Uttt

    llulSi(lt> the ,icl iR :iUitoSphCJic UIIU tll

    e

    dl

    'll thntthe

    bubhles

    OIC well

    separated

    rrom each

    o

    th

    er. The

    bubbl

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