TITLE.PM5

(Ann) #1

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)

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