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Heat Loss Insulated Pipe

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    Heat Loss From An Insulated PipeDate

    Tips & Tricks for Chemical Engineers By

    Pipe Inside Diameter (D1) 23.6 mm

    Outside Diameter (D2) 25.4 mmOperating Temperature 4.0

    Ambient Temperature -15.0

    ind !peed 3.50 m"s

    Insu#ati$n Insulated Pipe

    T%pe &a#'ium !i#i'ate !ura'e Temperature

    !ura'e mmisi*it% 0.04 +eat ,$ss

    Ti'ness 3/.1 mm Bare Pipe

    Outside Diameter D3 101.6 mm !ura'e Temperature

    +eat ,$ssCalculation for Insulated Pipe

    Iterati$ns 1 2

    !ura'e Temperature tsura'e -14 -14.5/ -14

    Intera'e Temperature tintera'e 3.0 4.00 4

    Air Properties

    A*erage i#m Temperature ta*erage -14.5 -14. -14

    25/.65 25/.36 25/

    Terma# &$ndu'ti*it% "m. 0.022 0.022 0.02

    is'$sit% 7 1.64-05 1.64-05 1.64

    Prandt# 8umber Pr 0.1/ 0.1 0.

    9pansi$n &$e:'ient ; 1" 0.003/66 0.003/1 0.003/

    Air Densit% < 1.3664 1.36 1.36

    inemati' is'$sit% = m2"s 1.22-05 1.22-05 1.22

    !pe'i>' +eat &p ?"g. 1.00 1.00 1

    a#pa @ 1.6-05 1.6/-05 1.6/

    e%n$#dBs 8umber e 2140 21/ 21

    a%#eig 8umber a 13440 /2152 /21

    Air Film Resistance

    adiati$n radiati$n 0.16 0.16 0

    &$n*e'ti$n$r'ed &$n*e'ti$n 8u$r'ed 146.5 146./ 14

    $r'ed 33.0/ 33.0 33

    ree &$n*e'ti$n 8uree .2/ .40

    ree 2.0 1.6 1

    &$mbined &$n*e'ti$n 8u&$mbined 146.5 146./ 14

    '$n*e'ti$n 33.0/ 33.0 33

    O*era## air side +T& air 33.23 33.25 33

    Pipe Resistance

    Pipe Terma# '$ndu'ti*it% pipe "m. 64./ 64./ 64

    Pipe Ca## resistan'e rpipe 0.00006 0.00006 0.000Insulation Resistance

    A*erage Insu#ati$n temperature 26 65 26 /60/ 26 /6

    ChemSOF.com

    &

    &

    &

    &

    &

    8"s.m

    g"mE

    m"s

    "m.

    "m.

    "m.

    "m.

    "m.

    m."

    Air

    Insu#ati$n

    Pipe

    #uid

    http://chemsof.com/http://chemsof.com/
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    Heat Loss From An Insulated PipeDate

    Tips & Tricks for Chemical Engineers By

    ChemSOF.com

    Insu#ati$n Terma# '$ndu'ti*it% insu#ati$n "m. 0.05322 0.05323 0.053

    Insu#ati$n resistan'e rinsu#ati$n 1.32 1.32 1Overall Resistance r$*era## 1.353 1.353 1.3

    +eat #$C F 14.04 14.04 14

    Intera'e Temperature Tintera'e 4.0 4.0

    !ura'e Temeperature Tsura'e -14.5/ -14.5/ -14

    +eat ,$ss per Gnit ,engt "m 4.4/ 4.4/ 4

    m."m."

    "m

    &

    &

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    Heat Loss From An Insulated PipeDate

    Tips & Tricks for Chemical Engineers By

    ChemSOF.com

    Calculation for Bare PipeIterati$ns 1 2

    !ura'e Temperature tsura'e -14.0 4.0

    Hare Pipe missi*it% 0./ 0./

    Air Properties

    A*erage i#m Temperature ta*erage -14.5 -5.51 -5

    25/.65 26.64 26

    Terma# &$ndu'ti*it% "m. 0.022 0.023 0.02

    is'$sit% 7 1.64-05 1.6-05 1.6

    Prandt# 8umber Pr 0.1/ 0.16 0.

    9pansi$n &$e:'ient ; 1" 0.003/66 0.00336 0.003Air Densit% < g"m3 1.3664 1.3205 1.32

    inemati' is'$sit% = 1.22-05 1.30-05 1.30

    !pe'i>' +eat &p ?"g. 1.00 1.00 1

    a#pa @ 1.6-05 1./0-05 1./0

    e%n$#dBs 8umber e 2/5 6/51 6/

    a%#eig 8umber a 3022 4/5 4/

    Air Film Resistance

    adiati$n radiati$n 3.13 3.30 3

    &$n*e'ti$n

    $r'ed &$n*e'ti$n 8u$r'ed 55. 53.5 5

    $r'ed 50.31 4./3 4

    ree &$n*e'ti$n 8uree 3.32 6.4 6

    ree 3.00 6.03 6

    &$mbined &$n*e'ti$n 8u&$mbined 55. 53.5 5

    '$n*e'ti$n 50.31 4./3 4

    O*era## air side +T& air 53.44 53.13 53

    Pipe Resistance

    Pipe Terma# '$ndu'ti*it% pipe "m. 64./ 64./ 64

    Pipe Ca## resistan'e rpipe 0.00001 0.00001 0.000

    Overall Resistance r$*era## 0.01 0.01 0.0+eat #$C F 1014.61 100/.0 100/

    Intera'e Temperature Tintera'e 4.0 4.0

    +eat ,$ss per Gnit ,engt "m /0.6 /0.4 /0

    &

    &

    8"s.m

    m"s

    m"s

    "m.

    "m.

    "m.

    "m.

    "m.

    m."

    m.""m

    &

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    23-Jan-15

    ChemS!

    -14.6

    4.5 "m

    4.0

    /0.5 "m

    4 5

    -14.5/ -14.5/

    4.00 4.00

    -14. -14.

    25/.36 25/.36

    0.022 0.022

    1.64-05 1.64-05

    0.1 0.1

    0.003/1 0.003/1

    1.36 1.36

    1.22-05 1.22-05

    1.00 1.00

    1.6/-05 1.6/-05

    21/ 21/

    /2121 /2121

    0.16 0.16

    146./ 146./

    33.0 33.0

    .40 .40

    1.6 1.6

    146./ 146./

    33.0 33.0

    33.25 33.25

    64./ 64./

    0.00006 0.00006

    26 /60 26 /60

    &

    &

    D1 D2 D3

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    23-Jan-15

    ChemS!

    0.05323 0.05323

    1.32 1.321.353 1.353

    14.04 14.04

    4.0 4.0

    -14.5/ -14.5/

    4.4/ 4.4/

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    ChemS!

    4 5

    4.0 4.0

    0./ 0./

    -5.51 -5.51

    26.64 26.64

    0.023 0.023

    1.6-05 1.6-05

    0.16 0.16

    0.00336 0.003361.3205 1.3205

    1.30-05 1.30-05

    1.00 1.00

    1./0-05 1./0-05

    6/51 6/51

    4/5 4/5

    3.30 3.30

    53.5 53.5

    4./3 4./3

    6.4 6.4

    6.03 6.03

    53.5 53.5

    4./3 4./3

    53.13 53.13

    64./ 64./

    0.00001 0.00001

    0.01 0.01100/.0 100/.0

    4.0 4.0

    /0.4 /0.4

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    Thermophysical properties of AirDate

    Tips & Tricks for Chemical Engineers By

    Literature Values Calculated Values

    T &p .103 Pr &p .1

    ?"g. 8.s"m2 m2"s C"m. m2"s ?"g. 8.s"m2 m2"s C

    100 1.032 1.1 2.00 .34 2.54 0./6 1.02 1.2 1.5

    150 1.012 103.4 4.43 13./0 5./4 0.5/ 1.016 103.2 4.45 1

    200 1.00 132.5 .5 1/.10 10.30 0.3 1.00 132.6 .64 1250 1.006 15.6 11.44 22.30 15.0 0.20 1.005 15. 11.4/ 2

    300 1.00 1/4.6 15./ 26.30 22.50 0.0 1.005 1/4./ 15.1 2

    350 1.00 20/.2 20.2 30.00 2.0 0.00 1.00/ 20/.2 20./ 3

    400 1.014 230.1 26.41 33./0 3/.30 0.60 1.014 230.0 26.3 3

    450 1.021 250. 32.3 3.30 4.20 0.6/6 1.021 250.5 32.34 3

    500 1.030 20.1 3/. 40.0 56.0 0.6/4 1.030 26. 3/.4 4

    550 1.040 2//.4 45.5 43.0 66.0 0.6/3 1.041 2//.4 45.55 4

    600 1.051 305./ 52.6 46.0 6.0 0.6/5 1.052 305. 52.4 4

    650 1.063 322.5 60.21 4.0 /.30 0.60 1.063 322./ 60.2 4

    00 1.05 33/./ 6/.10 52.40 /.00 0.65 1.05 33/. 6/.1/ 5

    50 1.0/ 354.6 6.3 54.0 10.00 0.02 1.0/ 354.5 6.3 5

    /00 1.0 36./ /4.3 5.30 120.00 0.0 1.0/ 36.6 /4.1 5

    /50 1.110 3/4.3 3./0 5.60 131.00 0.16 1.110 3/4.1 3.3 5

    00 1.121 3/.1 102.0 62.00 143.00 0.20 1.121 3/.1 102./4 650 1.131 411.3 112.20 64.30 155.00 0.23 1.131 411.5 112.24 6

    1000 1.141 424.4 121.0 66.0 16/.00 0.26 1.141 424.3 121.3 6

    So"rce # !"n$amentals of %eat an$ ass Transfer '2(()*+ !rank , ncropera

    ChemSOF.com

    7.10 =.106 @.106 7.10 =.106

    http://chemsof.com/http://chemsof.com/
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    3-Jan-15

    hemS!

    Pr

    m2"s

    2.6 0./4

    5.6 0.5

    10.10 0.3/15.6 0.21

    22.4/ 0.0

    30.0 0.6

    3/.43 0.60

    4.3 0.6/5

    56./1 0.6/3

    66.64 0.6/4

    6. 0.6/6

    /.22 0.61

    .// 0.66

    10/./ 0.02

    11.2 0.0/

    131.33 0.14

    143.06 0.20

    155.1/ 0.24

    16./ 0.26

    @.106

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    th Order Polynomial Fittin!

    "peci#c Heat Curve Fittin!

    &1.T4 &2.T3 &3.T2 &4.T &5

    3.032336-013 -1.11315-00 1.443/223-006 -0.00056533//1.0223/301

    1.0101361-013 2.234/3//-010 1.6/0506-00 4./4240-005 0.004603615

    0.042213 0.001631331 J8"A J8"A J8"A

    Viscosity Curve Fittin!

    &1.T4 &2.T3 &3.T2 &4.T &5

    -1.5/6-10 5.115-0 -.246-04 ./-01 -1./50K00

    1.0541/345-011 2.3322/625-00/ 1.6062246-005 0.005206/64 0.4/40103/0./0602 0.10/5155 J8"A J8"A J8"A

    $inematic Viscosity Curve Fittin!

    &1.T4 &2.T3 &3.T2 &4.T &5

    2.25/52005-011 -/.3202/4-00/ 0.00012632 0.010632/02 -0.610/351

    3.4322/2/4-012 .536104-00 5.323554-006 0.001653264 0.15/6136

    0./3/0/ 0.055621526 J8"A J8"A J8"A

    Thermal Conductivity Curve Fittin!

    &1.T4 &2.T3 &3.T2 &4.T &5

    3.116340-011 -0.00000005 4.5/530/60-006 0.0///6//60.52002234

    3.221206-012 /.234/4402-00 6.2164326-006 0.001/3/40 0.12023055

    0.10 0.0603246 J8"A J8"A J8"A

    Alpha Curve Fittin!

    &1.T4 &2.T3 &3.T2 &4.T &5

    1.3556/636-010 -3./05/6/-00 0.0004464/25 -0.0353552 2.2544/1641

    1.15144/-011 0.000000026 1.6264351-005 0.005/04454 0.54332434

    0.01606 0.10456206 J8"A J8"A J8"A

    Prandtl %um&er Curve Fittin!

    &1.T4 &2.T3 &3.T2 &4.T &5

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    -2.0/43/6-013 -1.2/234-011 /.0062424-00 -0.000646050./45/121/

    /.6312/14-014 1.055/00-010 1.4415363-00 0.000042633 0.003061

    0.30204 0.0013//6 J8"A J8"A J8"A

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    Thermophysical properties of AirDate

    Tips & Tricks for Chemical Engineers By

    Thermal Conductivity of Plain Car&on "teel

    T &a#'u#ated 'rd Order Polynomial Curve Fitti "m. "m. &1.T3 &2.T2 &3.T

    400 5/. 5/.0 2.0/-0 /.15-1 -5.11-02

    600 4/./ 4/./0 0 0 0

    /00 3.2 3.20 1 0 J8"A

    1000 30.0 30.00

    Thermal Conductivity of Calcium "ilicate

    T &a#'u#ated

    "m. "m. th Order Polynomial Curve Fitti

    310 0.055 0.0551 &1.T4 &2.T3 &3.T2365 0.05 0.05/ 3.1511-013 --010 .366-00

    420 0.063 0.0633 .11501-013 1.-00 1.46-006

    530 0.05 0.04/ 0./63/005 0.0005 J8"A

    645 0.0/ 0.0/1

    50 0.104 0.1040

    So"rce # !"n$amentals of %eat an$ ass Transfer '2(()*+ !rank , ncropera

    ChemSOF.com

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    23-Jan-15

    ChemS!

    !&4

    0

    J8"A

    !

    &4.T &5-0.000225 0.033360404

    0.0004/36 0.05/5561

    J8"A J8"A

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    Heat Loss from Insulated Pipe

    23-?an-15

    +eat #$ss"gain taes p#a'e r$m a pipe 'arr%ing $tter" '$#der Luid tan ambient tempe

    . 3/ Car0on steel pipe is carrying hot oil at 1(C an$ ins"late$ ith 5( mm thick calci

    O*era## eat transer '$e:'ient $ an insu#ated pipe is de>ned as $##$Cing.

    eatured es$ur'esN

    Is Critten $r engineering pr$essi$na#s C$ bu% and spe'i% pr$'ess euip

    ta*erage S ( tsura'e K tambient )" 2

    stimate term$d%nami' pr$perties $ air #ie terma# '$ndu'ti*it% ()M *is'$sit% ()M e

    h(radiation

    +eat transer '$e:'ient due t$ radiati$n is 'a#'u#ated using $##$Cing re#ati$n.

    Cere U is !tean H$#tmann '$ei'ient and V is emissi*it% $r '#added sura'e.

    h(convection

    &$n*e'ti*e eat transer '$e:'ient '$mprises $ $r'ed and ree '$n*e'ti$n. $r'ed '

    CereM PIP

    M I8!G,ATIO8

    are terma# '$ndu'ti*ities $ pipe and insu#ati$n. inis eat trans

    Air "ide Heat Transfer Coe)cient* hAIR

    Air side eat transer is due t$ '$mbined eWe't $ '$n*e'ti$n and radiati$n. Assume a

    radiati$n S U V (ta*erage4- tambient4)" (ta*erage - tambient)

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    $r'ed S 8u.air " D3

    ree '$n*e'ti$n is 'a#'u#ated based $n '$rre#ati$n b% &ur'i## and &u.

    ree S 8u.air " D3

    &$mbined eat transer '$e:'ient due t$ $r'ed and ree '$n*e'ti$n is 'a#'u#ated usin

    '$n*e'ti$n S 8u'$mbined.air " D3

    Air side eat transer '$e:'ient is 'a#'u#ated as $##$Cing.

    air S radiati$n K '$n*e'ti$n

    Overall Heat Transfer Coe)cient* +

    Terma# '$ndu'ti*it% $r insu#ati$n materia# and pipe is a*ai#ab#e in #iterature and depe

    rpipe S D3.#n(D2"D1) " 2.pipe

    rinsu#ati$n S D3.#n(D3"D2) " 2.insu#ati$n

    O*era## eat transer '$e:'ient is 'a#'u#ated as.

    r$*era## S rpipe K rinsu#ati$n K 1"air

    G S 1"r$*era##

    +eat L$Cing tr$ug insu#ati$n is estimated.

    F S (t$perating - tambient)"r$*era##

    A re*ised estimate $r intera'e and sura'e temperature is made.

    tintera'e S t$perating - F.rpipe

    tsura'e S tintera'e - F.rinsu#ati$n

    Ab$*e steps are repeated Cit tese neC estimates ti## tere is neg#igib#e diWeren'e in

    +eat #$ss per unit #engt $ pipe is estimated as $##$Cing.

    8u'$mbined S ( 8u$r'ed 4K 8uree 4) 0.25

    +eat,$ss

    S XD3 F

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    Bare Pipe

    $r eat #$ss r$m bare pipe a## ab$*e steps are repeated Cit resistan'e due t$ insu#at

    rpipe S D2.#n(D2"D1) " 2.piper$*era## S rpipe K 1"air

    $r tis e9amp#e sura'e temperature and eat #$ss are as $##$Cing.

    !preadseet $r +eat ,$ss r$m Insu#ated Pipe

    http://www.chemsof.com/assets/sheet/Heat_Loss_Insulated_Pipe.xlsxhttp://www.chemsof.com/assets/sheet/Heat_Loss_Insulated_Pipe.xlsx
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    rature. Insu#ati$n redu'es te eat #$ss t$ surr$undings. +eat #$ss depends up$n numb

    "m silicate ins"lation4 ns"lation is cla$$e$ ith a sheet ith s"race emissiity of (464

    ent t$ '$$#M 'i## $r reee pr$du'tQ measureM m$nit$r $r... RR

    pansi$n '$ei'ient (; S 1"ta*erage)M air densit% (

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    g $##$Cing re#ati$n.

    nds up$n temperature. It 'an be >tted int$ a p$#%n$mia# euati$n using ,I8!T un'ti$

    temperature.

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    i$n n$t '$nsidered.

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    er $ a't$rs #ie insu#ati$n ti'nessM ambient temperatureM Cind speed et'. Tis arti'#

    m0ient temperat"re is 2C an$ in$ elocity is 345 m7s4 Calc"late s"rface temperat"

    eat (&p) and terma# diusi*it% (@) at a*erage air i#m temperature. Tese pr$perties a

    ng $utside te pipe. Te >rst tC$ terms $ den$minat$r in ab$*e euati$n are genera##

    a*erage air >#m temperature as $##$Cing.

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    n in e9'e#. +eat transer resistan'e due t$ pipe and insu#ati$n is 'a#'u#ated using $##$C

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    e s$Cs $C t$ 'a#'u#ate eat #$ss r$m an insu#ated pipe and a bare pipe t$ surr$undi

    re an$ heat loss from ins"late$ an$ 0are pipe4

    re a*ai#ab#e in #iterature in $rm $ tab#esM tese 'an be itted int$ a p$#%n$mia# $rm u

    sma##er '$mpared t$ remaining terms and 'an be neg#e'ted. $r tis e9amp#e >rst ter

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    ing re#ati$n.

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    gs.

    ing e9'e#Bs ,I8!T un'ti$n. e%n$#dsBs number (e)M Prandt# number (Pr) and a%#eig

    m due t$ pipe Luid is ign$red.

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    number (a) are 'a#'u#ated based $n ab$*e pr$perties.

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