HEAT TRANSFER 789dharm
\M-therm\Th15-1.pm5Since the quantity of heat transmitted per unit time through each slab/layer is same, we
have
Q = kAt t
LkAt t
LkAt t
LA
AB
BC
C.( 12 − )=. ( 23 − )=. ( 34 − )(Assuming that there is a perfect contact between the layers and no temperature drop occurs
across the interface between the materials).
Rearranging the above expression, we get
t 1 – t 2 = QL
kAA
A.
.
...(i)t 2 – t 3 =
QL
kAB
B.
.
...(ii)t 3 – t 4 =
QL
kAC
C.
.
...(iii)
Adding (i), (ii) and (iii), we have(t 1 – t 4 ) = QL
kAL
kAL
kAA
AB
BC
...CL ++
N
MO
Q
Por Q =At t
L
kL
kL
kA
AB
BC
C() 14 −
++
L
N
MO
Q
P...(15.27)or Q =
()...()
[]tt
L
kAL
kAL
kAtt
A RRR
AB
BC
Cth A th B th C14 − 14
++
L
NM
O
QP
= −
−−−++...(15.28)
If the composite wall consists of n slabs/layers, thenQ =[]tt()
L
kAn
n111− +∑
...(15.29)ACB
QkA kC kGkB D
kDF
kFE
kEGQComposite wallRth–A
Rth–CRth–B
Rth–DRth–ERth–GRth F–Fig. 15.5. Series and parallel one-dimensional heat transfer through a composite wall and electrical analog.