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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$n temperature 26 65 26 /60/ 26 /6
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Heat Loss From An Insulated PipeDate
Tips & Tricks for Chemical Engineers By
ChemSOF.com
Insu#ati$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 ,$ss per Gnit ,engt "m 4.4/ 4.4/ 4
m."m."
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Heat Loss From An Insulated PipeDate
Tips & Tricks for Chemical Engineers By
ChemSOF.com
Calculation for Bare PipeIterati$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
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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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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
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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$m Insu#ated Pipe
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rature. Insu#ati$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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