HEAT TRANSFER 791
dharm
\M-therm\Th15-1.pm5t 1t 2hcfhhf
Hot fluid filmQ Qthf1Metal wallCold fluid film
tcf
2
L
thf t 1 t 2 tcf
1
h.AhfL
k.A1
h.AcfkFig. 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
LA() 12 − ...(ii)Q = hcf. A(t 2 – tcf) ...(iii)
By rearranging (i), (ii) and (iii), we getthf – t 1 =
Q
hAhf. ...(iv)t 1 – t 2 =
QL
kA. ...(v)t 2 – tcf =
Q
hAcf. ...(vi)
Adding (iv), (v) and (vi), we getthf – tcf = Q11
hAL
hf.. .kA h Acf++L
NM
MO
QP
Por Q =
At thL
khhf cfhf 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)