812 ENGINEERING THERMODYNAMICS
dharm
\M-therm\Th15-2.pm5
Case II : The heat flow through an insulated wire when critical thickness is used is given
by
Q 2 =^212 0 00343 0 001
012
1
35 0 00343
1
1
ππLt t 1
rr
khr
air Lt t
c
oc
() air
ln ( / )
.
()
ln (. /. )
.
.
−
+
= − +
×
=^2
18 6
πLt t() 1 air
.
− ...(ii)
∴ Percentage increases in heat flow by using critical thickness of insulation
=
QQ
Q
21
1
−
× 100 =
1
18.6
1
20.77
1
20.77
−
× 100 = 11.6%. (Ans.)
15.3. Heat Transfer by Convection
l The rate equation for the convective heat transfer (regardless of particular nature)
between a surface and an adjacent fluid is prescribed by Newton’s law of cooling (Refer
Fig. 15.29)
Q = hA(ts – tf) ...(15.44)
where, Q = Rate of conductive heat transfer,
A = Area exposed to heat transfer,
ts = Surface temperature,
tf = Fluid temperature, and
h = Co-efficient of conductive heat transfer.
The units of h are, h =
Q
At t()s f
W
− mC^2
=
°
or W/m^2 °C or W/m^2 K
The coefficient of convective heat transfer ‘h’ (also known as film heat transfer coefficient)
may be defined as ‘‘the amount of heat transmitted for a unit temperature difference between the
fluid and unit area of surface in unit time.’’
The value of ‘h’ depends on the following factors :
(i) Thermodynamic and transport properties (e.g., viscosity, density, specific heat etc.) ;
(ii) Nature of fluid flow ;
(iii) Geometry of the surface ;
(iv) Prevailing thermal conditions.
Since ‘h’ depends upon several factors, it is difficult to frame a single equation to satisfy all
the variations, however a dimensional analysis gives an equation for the purpose which is given as
under :
h
k
D Z CD
a
= F
HG
I
KJ
ρ
π
c
k
D
L
p
F μ b c
HG
I
KJ
F
HG
I
KJ ...(15.45)
or Nu = Z (Re)a (Pr)b D
L
F c
HG
I
KJ
where, Nu = Nusselt number h
k
F D
HG
I
KJ
,
Re = Reynolds number
ρ
μ
F uD
HG
I
KJ
,