SOLVED PROBLEMS SOLVED PROBLEMS
Combined Convection and Radiation Combined Convection and Radiation Problem 1:
Problem 1:
A surface is
A surface is at 200°C and
at 200°C and is exposed to surroundings at
is exposed to surroundings at 60°C
60°C
and convects and
and convects and
radiates heat to the surroundings. The convection coefficient is 80W
radiates heat to the surroundings. The convection coefficient is 80W //m
m
22K.
K.
The radiation factor is one. If the heat is conducted to the surface through
The radiation factor is one. If the heat is conducted to the surface through
a solid of conductivity 12 W/mK, determine the temperature gradient at
a solid of conductivity 12 W/mK, determine the temperature gradient at
the surface in the solid.
the surface in the solid.
Solution: Solution:
Heat convected + heat radiated = heat conducted considering 1
Heat convected + heat radiated = heat conducted considering 1m
m
22,,
h
h((T
T
11–
– T
T
22) +
) +
σσ((T
T
1144–
– T
T
2244) = –
) = – kdT
kdT //dx
dx
Therefore, 80(200 – 60) + 5.67 {[(200 +
Therefore, 80(200 – 60) + 5.67 {[(200 + 273)/100]
273)/100]
44– [(60 + 273)/100]
– [(60 + 273)/100]
44}
}
= – 12
= – 12 dT/dx
dT/dx
Therefore
Therefore dT/dx
dT/dx =
= – (11200
– (11200 + 2140.9)/12
+ 2140.9)/12 = –
= –
1111.7°C/m.1111.7°C/m. Problem 2:Problem 2:
Heat is conducted through a material with a temperature
Heat is conducted through a material with a temperature
gradient of – 9000 °C
gradient of – 9000 °C//m. The conductivity of the material is 25W/mK. If
m. The conductivity of the material is 25W/mK. If
th
this
is he
heat
at is
is co
conv
nvec
ecte
ted
d to
to su
surr
rrou
ound
ndin
ings
gs at
at 30
30°C
°C wi
with
th a
a co
conv
nvec
ecti
tion
on
coefficient of 345W/m2K, determine the surface temperature.
coefficient of 345W/m2K, determine the surface temperature.
If the heat is radiated to the surroundings at 30°C determine the surface
If the heat is radiated to the surroundings at 30°C determine the surface
temperature.
temperature.
Solution:
Solution:
In this case only convection and conduction are
In this case only convection and conduction are involved.
involved.
–
– kAdT
kAdT //dx
dx =
= hA
hA((T
T
11–
– T
T
22). Considering unit area,
). Considering unit area,
– 25 × 1 × (– 9000) = 345 × 1 (
– 25 × 1 × (– 9000) = 345 × 1 ( T
T
11– 30)
– 30)
Therefore,
Therefore,
TT11 = 682.17°C= 682.17°CIn this case conduction and radiation are
In this case conduction and radiation are involved.
involved.
Heat conducted = Heat radiated
Heat conducted = Heat radiated
– 25 × 1 × (– 9000) = 5.67 [(
– 25 × 1 × (– 9000) = 5.67 [(T
T
11/100)
/100)
44– (303/100)
– (303/100)
44]]
Therefore,
Therefore,
TT11 = 1412.14K = 1139°C.= 1412.14K = 1139°C.Problem 3:
Problem 3:
There is a heat flux through a wall of 2250W/m
There is a heat flux through a wall of 2250W/m
22. The same is
. The same is
dissipated to the
dissipated to the
surroundings by convection and radiation. The surroundings is at 30°C.
surroundings by convection and radiation. The surroundings is at 30°C.
The convection
The convection
coefficient has a value of 75W/m
coefficient has a value of 75W/m
22K. For radiation F = 1. Determine the
K. For radiation F = 1. Determine the
wall surface temperature.
wall surface temperature.
Solution:
Solution:
For the specified condition, Consider unit area.
For the specified condition, Consider unit area.
The heat conducted = heat conv
The heat conducted = heat convected + heat radiated
ected + heat radiated
Using the rate equations, with absolute
Using the rate equations, with absolute temperature
temperature
2250 = [(T
2250 = [(T
22– 303)/(1/75 × 1] + 5.67 × 1[(
– 303)/(1/75 × 1] + 5.67 × 1[(T
T
22/100)
/100)
44– (303/100)
– (303/100)
44]]
= 75
= 75T
T
22– 22725 + 5.67(
– 22725 + 5.67(T
T
22/100)
/100)
44– 477.92
– 477.92
or, (
or, (T
T
22/100)
/100)
44+ 13.2275
+ 13.2275T
T
22– 4489.05 = 0.
– 4489.05 = 0.
This equation can be solved only by trial. It may be noted that the
contribution of (T
2/100)
4is small and so the first choice of T
2can be a little
less than 4489/13.227 = 340K. The values of the reminder for T
2= 300,
310, 320, 330 are given below:
Assumed value of T 2
300 310 320 330 330.4 330.3
Remainder – 439.80 – 296.2 – 15.1 – 5.38 0.484 – 0.98
So, the temperature T
2is near 330K. By one more trial T
2is obtained
as330.4K or 57.4°C.
Check:
Q = 75(330.4 – 303) + 5.69(3.304
4– 3.03
4)
= 2047.5 + 206 = 2253.5 W.
PROBLEM 1.1
The outer surface of a 0.2m-thick concrete wall is kept at a temperature of –5°C, while the inner surface is kept at 20°C. The thermal conductivity of the concrete is 1.2 W/(m K). Determine the heat loss through a wall 10 m long and 3 m high.
GIVEN
10 m long, 3 m high, and 0.2 m thick concrete wall
Thermal conductivity of the concrete (
k ) = 1.2 W/(m K)
Temperature of the inner surface (
Ti) = 20°C
Temperature of the outer surface (
To) = –5°C
FIND
The heat loss through the wall (
qk )
ASSUMPTIONS
One dimensional heat flow
The system has reached steady state
SKETCH
SOLUTION
The rate of heat loss through the wall is qk = (AK/L)
×
(∆T )qk = [(10m) (3m)
(
1.2W/(mK))/
0.2m]×
(20°C – (–5°C)) qk = 4500 WCOMMENTS
Since the inside surface temperature is higher than the outside temperature heat is transferred from the inside of the wall to the outside of the wall.
PROBLEM 1.9
Heat is transferred at a rate of 0.1 kW through glass wool insulation (density = 100 kg/m3) of 5 cm thickness and 2 m2 area. If the hot surface is at 70°C, determine the
temperature of the cooler surface. GIVEN
Glass wool insulation with a density (
ρ) = 100 kg/m3
Thickness (
L) = 5 cm = 0.05 m
Area (
A) = 2 m2
Temperature of the hot surface (
Rate of heat transfer (
qk ) = 0.1 kW= 100 W
FIND
The temperature of the cooler surface (
T C)
ASSUMPTIONS
One dimensional, steady state conduction
Constant thermal conductivity
SKETCH
PROPERTIES AND CONSTANTS
From Appendix 2, Table 11
The thermal conductivity of glass wool at 20°C ( k ) = 0.036 W/(m K) SOLUTION
For one dimensional, steady state conduction, the rate of heat transfer, is qk = (Ak/L)
×
(T h – T c)Solving this for Tc Tc = T h – qk L/A k
T c= 70°C – [(100W) (0.05m)]/[(2 m2)( 0.036W/mK)]
T c= 0.6°C
PROBLEM 1.10
A heat flux meter at the outer (cold) wall of a concrete building indicates that the heat loss through a wall of 10 cm thickness is 20 W/m2. If a thermocouple at the inner surface
of the wall indicates a temperature of 22°C while another at the outer surface shows 6°C, calculate the thermal conductivity of the concrete and compare your result with the value in Appendix 2, Table 11.
GIVEN Concrete wall Thickness ( L) = 100 cm = 0.1 m Heat loss ( q/ A) = 20 W/m2 Surface temperature Inner ( T i) = 22°C Outer ( T o) = 6°C FIND
The thermal conductivity (
k ) and compare it to the tabulated value
ASSUMPTIONS
One dimensional heat flow through the wall
Steady state conditions exist
SKETCH
SOLUTION
The rate of heat transfer for steady state, one dimensional conduction, is qk = (k A/L)
×
(T hot– T cold)Solving for the thermal conductivity k = (qk / A)
×
L/(T i – T o )This result is very close to the tabulated value in Appendix 2 , Table 11 where the thermal conductivity of concrete is given as 0.128 W/(m K).
PROBLEM 1.11
Calculate the heat loss through a 1-m by 3-m glass window 7 mm thick if the inner surface temperature is 20°C and the outer surface temperature is 17°C. Comment on the possible effect of radiation on your answer.
GIVEN Window: 1 m by 3 m Thickness ( L) = 7 mm = 0.007 m Surface temperature Inner ( T i) = 20°C and outer (To) = 17°C FIND
The rate of heat loss through the window (
q)
ASSUMPTIONS
One dimensional, steady state conduction through the glass
Constant thermal conductivity
SKETCH
PROPERTIES AND CONSTANTS From Appendix 2, Table 11
Thermal conductivity of glass (k ) = 0.81 W/(m K) SOLUTION
The heat loss by conduction through the window is qk = (k A/L)
×
(T hot– T cold)qk = [[(0.81W/(mK))(1m) (3m)]/(0.007m)]
×
(20°C – 17°C)qk = 1040 W
COMMENTS
Window glass is transparent to certain wavelengths of radiation, therefore some heat may be
lost by radiation through the glass.
During the day sunlight may pass through the glass creating a net heat gain through the
window.
PROBLEM 1.12
If in Problem 1.11 the outer air temperature is –2°C, calculate the convective heat transfer coefficient between the outer surface of the window and the air assuming radiation is negligible.
Problem 1.11: Calculate the heat loss through a 1 m by 3 m glass window 7 mm thick if the inner surface temperature is 20°C and the outer surface temperature is 17°C.
Comment on the possible effect of radiation on your answer. GIVEN Window: 1 m by 3 m Thickness ( L) = 7 mm = 0.007 m Surface temperatures Inner ( T i) = 20°C and outer (T o) = 17°C
The rate of heat loss = 1040W (from the solution to Problem 1.11)
The outside air temperature = –2°C
FIND
The convective heat transfer coefficient at the outer surface of the window (
hc )
ASSUMPTIONS
The system is in steady state and
radiative loss through the window is negligible
SKETCH
SOLUTION
For steady state the rate of heat transfer by convection (Equation (1.10)) from the outer surface must be the same as the rate of heat transfer by conduction through the glass
qc= hcA ∆T = qk Solving for hc hc = qk / A (T o – T ∞ ) hc= 1040W / (1m)(3m)( 17°C – – 2°C) hc= 18.2 W/(m2K) COMMENTS
This value for the convective heat transfer coefficient falls within the range given for the
PROBLEM
The wall of an industrial furnace is constructed from 0.15-m-thick fireclay
brick having a thermal conductivity of
1.7 W/m. K.Measurements made
during steady-state operation reveal temperatures of 1400 and 1150 K at
the inner and outer surfaces, respectively. What is the rate of heat
transfer through a wall that is 0.5 m by 1.2 m on a side?
Solution
Known: Steady-state conditions with prescribed wall thickness, area, thermal conductivity, and surface temperatures.
Find:Heat transfer rate through the wall. Schematic and Given Data:
Assumptions:
1.Steady-state conditions.
2.One-dimensional conduction through the wall. 3. Constant thermal conductivity.
Analysis: Since heat transfer through the wall is by conduction, the heat flux may be determined from Fourier’s law.
q x= k ∆T /L = 1.7 W/m. K × 250 K / 0.15 m = 2833 W/m2
The heat flux represents the rate of heat transfer through a section of unit area, and it is uniform across the surface of the wall.
The heat rate through the wall of area A = H × W is then Q x= ( HW ) q x= (0.5 m × 1.2 m) 2833 W/m2= 1700 W