812 ENGINEERING THERMODYNAMICSdharm
\M-therm\Th15-2.pm5Case II : The heat flow through an insulated wire when critical thickness is used is given
by
Q 2 =^212 0 00343 0 001
0121
35 0 003431
1ππLt t 1
rr
khrair Lt t
c
oc() air
ln ( / )
.()
ln (. /. )
..−
+= − +
×=^2
18 6πLt t() 1 air
.− ...(ii)∴ Percentage increases in heat flow by using critical thickness of insulation=
QQ
Q21
1−
× 100 =1
18.61
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 fW
− mC^2=
°or W/m^2 °C or W/m^2 KThe 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
kD Z CDa
= F
HGI
KJρ
πc
kD
Lp
F μ b c
HGI
KJF
HGI
KJ ...(15.45)or Nu = Z (Re)a (Pr)b D
L
F c
HGI
KJ
where, Nu = Nusselt number h
kF D
HGI
KJ,Re = Reynolds number
ρ
μF uD
HGI
KJ
,