HEAT TRANSFER 791
dharm
\M-therm\Th15-1.pm5
t 1
t 2
hcf
hhf
Hot fluid film
Q Q
thf
1
Metal wall
Cold fluid film
tcf
2
L
thf t 1 t 2 tcf
1
h.Ahf
L
k.A
1
h.Acf
k
Fig. 15.7. The overall heat transfer through a plane wall.
The equations of heat flow through the fluid and the metal surface are given by
Q = hhf. A(thf – t 1 ) ...(i)
Q = kt t
L
A() 12 − ...(ii)
Q = hcf. A(t 2 – tcf) ...(iii)
By rearranging (i), (ii) and (iii), we get
thf – t 1 =
Q
hAhf. ...(iv)
t 1 – t 2 =
QL
kA. ...(v)
t 2 – tcf =
Q
hAcf. ...(vi)
Adding (iv), (v) and (vi), we get
thf – tcf = Q
11
hA
L
hf.. .kA h Acf
++
L
N
M
M
O
Q
P
P
or Q =
At t
h
L
kh
hf cf
hf cf
()−
(^11) ++
...(15.31)
If U is the overall coefficient of heat transfer, then
Q = U.A (thf – tcf) =
At t
h
L
kh
hf cf
hf cf
()−
(^11) ++
or U =
1
11
h
L
hf khcf
++
...(15.32)