HEAT TRANSFER:
Tutorial problems
Pick the subject area of your choice:
Solutions will be made available via hyperlinks after the problems have
been dealt with in tutorial sessions.
Conduction tutorial problems
-
A heat rate of 3 kW is conducted through a section of an insulating material
of cross sectional area 10 m2 and of thickness 25 mm. If the
inner (hot) surface temperature is 415°C and the thermal conductivity
of the material is 0.2 W/m.K, what is the outer surface temperature?
[377.5°C]
-
One-dimensional, steady-state conduction without heat generation occurs
in a plane wall of thickness 0.5 m and thermal conductivity 25 W/m.K. Determine
the unknown quantities for each case in the table below, sketch the temperature
distribution and show the direction of the heat flux.
|
Case
|
Inside temp (T1)
|
Outside temp (T2)
|
dT/dx (K/m)
|
Heat flux (W/m2)
|
|
1
|
400K
|
300K
|
?
|
?
|
|
2
|
100°C
|
?
|
-250
|
?
|
|
3
|
80°C
|
?
|
+200
|
?
|
|
4
|
?
|
-5°C
|
?
|
4000
|
|
5
|
30°C
|
?
|
?
|
-3000
|
[-200 K/m, +5000 W/m2;
-25°C, 6250 W/m2; 180°C, -5000 W/m2, 75°C,
-160 K/m; 90°C, 120 K/m]
-
A plain slab is subjected to a temperature of 400 K on one side and 300
K on the other. The thermal conductivity of the material of the slab is
a function of temperature given by 30exp(T/100) W/m.K. Find the temperature
at the mid point within the slab.
[362 K]
-
A lagged steam pipe has a total outside diameter of 0.12 m, including a
20 mm thick layer of calcium silicate insulation on the outside. The inner
and outer surfaces of the insulation are at temperatures of 800 K and 490
K respectively. Calculate the heat loss per unit length of pipe.
Thermal conductivity of calcium silicate = 0.07 W/m.K.
[336 W/m length]
[Click here for WORKED EXAMPLE]
-
A steam pipe 0.2 m OD is covered by two layers of insulation material,
each 0.025 m thick, and the thermal conductivity of one material is three
times that of the other. Calculate the difference in the effective
conductivity of the two layers for the situations:
(i) better insulating material on outside;
(ii) better insulating material on inside.
Assume that the temperatures of the two surfaces remain unaltered.
[(i) conducts 10% more heat
than (ii)]
-
A scraped surface chiller, used for crystallising para-xylene, consists
of long steel cylinders 0.3 m OD and walls 0.01 m thick containing rotating
scrapers which remove the crystals. This cylinder is surrounded by a coolant
at low temperature. As the scrapers wear, a layer of crystals build up
on the inner surface hence new scrapers have to be installed when the chiller
efficiency falls by 20%. What will be the thickness of the crystal layer
when this point is reached?
| ksteel |
= 40 W/m.K |
| kp-xylene crystals |
= 1.0 W/m.K |
[60 mm]
-
A cylindrical cement kiln has an external shell of 0.02 m thick steel and
OD of 2.0 m. The refractory temperature inside the kiln is 1400 K and the
outer steel surface has a temperature of 400 K when there is a refractory
lining 0.2 m thick. The outer surface temperature is used to determine
the time between shutdowns for relining which occurs when this is 500 K.
What is the running time for a refractory erosion rate of 1 mm per week?
Assume that the heat loss remains unchanged.
| ksteel |
= 30 W/m.K |
| krefractory |
= 1 W/m.K |
[20 weeks]
-
If the setting of concrete is accompanied by the diffuse evolution of heat
at the rate of 50 W/m3, determine the maximum temperature in
a concrete slab used for foundations 1 m thick by 1 m deep, during the
setting period. It may be assumed that steady state conditions prevail
through the setting period and that the surface temperature of the slab
is maintained at 280K. Thermal conductivity of wet concrete is 0.8 W/m.K.
[284 K]
Conduction example
Saturated steam at 800 kPa flows through a pipe of outside diameter
4.8 cm. The outside of the pipe is insulated with magnesia insulation,
5 cm thick; the thermal conductivity of the magnesia is 0.07 W/m.K. The
outside pipe surface is at 170°C and the outside of the insulation
is at 35°C. Calculate the rate of condensation of steam in a 30 m length
of pipe.
Solution:
r1 = 2.4 cm; r2 = 7.4 cm; T1 = 170°C;
T2 = 35°C
Q’ = m’ lfg
m’ = 1582 ¸ 2040 J/g = 0.78 g/s
Convection tutorial problems
In all problems involving natural convection, assume gases to be
ideal
[Click here for WORKED EXAMPLE]
-
Derive the expression that relates the thermal cubic expansivity of an
ideal gas to its absolute temperature.
[b
= 1/T]
-
An unlagged pipe of outer diameter 15 cm carries steam the 20 metre distance
along a road between boilerhouse and plant. If steam at 1 bar (gauge) is
used, 3.0 grammes per second of condensate have formed by the time the
pipe has reached the plant. If the outside air is at 15°C, what is
its convective heat transfer coefficient? Assume that the resistances to
heat transfer presented by convection inside the pipe and conduction through
its walls are negligible in comparison.
[6.7 W/m2K]
-
Justify the above coefficient with a suitable correlation.
[solution]
-
A 30cm pipe carries crude oil from an off-shore drilling platform to a
storage tanker. The length of the pipe is submerged in sea water at 7°C,
the oil enters at 23°C and leaves at 17°C. Taking the physical
properties of sea water to be the same as those for pure water, what is
the predicted heat transfer coefficient of the sea, and what doubts do
you have in this prediction? Again, assume that the resistances to heat
transfer presented by convection inside the pipe and conduction through
its walls are negligible in comparison.
[340 W/m2K]
-
Atmospheric air is blown at is 7.50 ´
10-4 m3/s through a tube 2.00 m long and 40.0 mm
inner diameter, and heated from 290 to 310 K. Calculate the inside film
coefficient by the most appropriate correlation.
[3.35 W/m2K]
-
Water is heated from 20.00°C to 50.00°C in the shell-side of a
heat exchanger. Inside the exchanger, tubes with 19.05 mm outer diameter
(do) are arranged in a horizontal bundle of 8 rows, on a tube
pitch (pt) of 23.81 mm. The equivalent diameter for the narrowest
gap between tubes is given by:
The water at the narrowest gap between tubes has a velocity of 1.600
m/s and the outer surface of the tubes are maintained at a constant 100.0°C.
Calculate the outside film coefficient by the most appropriate correlation,
and hence find the heat flux.
[8.903 kW/m2K,
578.7 kW/m2]
-
Engine oil is stored in a sump below an internal combustion motor. To keep
its viscosity low enough for easy pumping, but high enough for useful lubrication,
the oil temperature is maintained at 310 K. This is done by diverting some
of the exhaust fumes down a pipe of 12.7 mm outer diameter, which then
passes horizontally through the sump. If the pipe has an average outer
surface temperature of 353 K, and 4.5 kW of heat is needed to keep the
oil temperature steady, how long must the pipe be?
[26 m]
-
The element inside an electric kettle has a circular cross-section of 11
mm diameter. If the element has a steady temperature of 120°C, what
are the heat transfer coefficients when the kettle is newly filled (take
tap water as 12°C) and just before the water starts to boil?
[1780 & 1531 W/m2K]
-
If the kettle element in the above question were 50 cm long, to what power
output would it have to be rated?
[3 kW]
Convection example
Water is being heated from 50.0 to 90.0°C inside a tube of internal
diameter 40.0 mm. The water flow rate is 3.00 ´
10-3 m3/s. Calculate the inside film coefficient
by the most appropriate correlation.
SOLUTIONS
Heat transfer is by forced convection. The mean temperature
of the water in contact with the tube must be calculated first. As no information
on the film temperature is available, the overall temperatures will have
to be used:
Average temperature of water is:
We can only therefore use a correlation that takes the fluid temperature
as being the average of the inlet and outlet temperatures, as calculated
above. The physical properties are found in Steam Tables.
| At 70.0°C, |
m |
|
= 400 ´ 10-6 |
kg/m.s |
| |
k |
|
= 662 ´ 10-3 |
W/m.K |
| |
r |
= 1 ¸ (0.1023
´
10-2) |
= 977.5 |
kg/m3 |
| |
Pr |
|
= 2.532 |
(dimensionless) |
But before choosing the correlation, the Reynolds number needs to be
known.
i.e turbulent
The length of the tube is unknown, hence the Nusselt correlation for
turbulent flow cannot be used. Alternatively, there is the Dittus-Boelter
correlation, if the tube is assumed to be long enough with respect to its
internal diameter. Expect an accuracy of ±
20%.
Nu = 0.0225 Re0.8Pr0.4 where Re > 10 000, 0.7
> Pr > 160
Nu = 0.0225 (233 365)0.8 (2.532)0.4 = 642.68
As the tube wall temperature (and hence the water viscosity at this temperature)
is unknown, one can only use the Sieder-Tate turbulent forced convection
correlation it the viscosity is assumed to be only marginally different.
If this were the case, the viscosity correction factor would be approximately
one. The answer will be of roughly the same accuracy as the Dittus-Boelter
calculation.
where
Re > 10 000, 0.7 > Pr > 16 700
Nu = 0.027 (233 365)0.8 (2.532)0.33 (1) = 722.69

If the tube surface temperature were to be given as 100°C, this
opens avenues to several more calculations.
Firstly, we can confirm the assumptions made for the Dittus-Boelter
prediction:
| At 50.0°C, |
r |
= 1 ¸ (0.1012
´
10-2) |
= 988.14229 |
kg/m3 |
| |
Water flowrate |
= 988.14 ´
(3 ´ 10-3) |
= 2.9644269 |
kg/s |
| At 70.0°C, |
CP |
|
= 4191 |
J/kg.K |
| |
Heat load |
= 2.964 ´ 4191(90-50) |
= 496 956 |
W |
i.e. assumption valid
Secondly, we can recalculate the Sieder-Tate prediction with greater
accuracy, although still not as good as ±
12%:
At 100°C, mW = 279 ´
10-6 kg/m.s

Nu = 0.027 (233 365)0.8 (2.532)0.33 (1.0517)
= 760.04
As with the Dittus-Boelter calculation, length can now be calculated with
relation to heat load and transfer coefficient.

Use this to give an iterative solution for the Nusselt correlation,
with 12000 W/m2K as the first estimate:

= 0.036 (233365)0.8
(2.532)0.33 (0.73429) = 707.53
Re-inserting this answer for a second iteration:

= 0.036 (233365)0.8
(2.532)0.33 (0.73330) = 706.57
Re-inserting this answer for a third iteration:

= 0.036 (233365)0.8
(2.532)0.33 (0.73325) = 706.52
i.e. Nusselt correlation is valid
IN SUMMARY
|
Dittus-Boelter
|
Sieder-Tate (without viscosity correction)
|
Sieder-Tate (with viscosity correction)
|
Nusselt
|
|
10 636 W/m2K
|
11 961 W/m2K
|
12 579 W/m2K
|
11 639 W/m2K
|
Heat exchange (combining resistances)
tutorial questions
-
The composite wall of an oven consists of three materials, two of which
are of known thermal conductivity, kA = 20 W/m.K, and kC
= 50 W/m.K, and of known thicknesses D xA
= 0.30 m and D xC = 0.15 m. The third
material B is sandwiched between materials A and C and is of thickness
0.15 m.
Under steady state conditions measurements reveal that the outer surface
of material C is at a temperature of 20°C, the inner exposed surface
of material A is at 600°C and the air temperature adjacent to this
surface is 800°C with a convective heat transfer coefficient to this
surface of 25 W/m2K.
Determine the thermal conductivity of material B
[1.5 W/m.K]
-
A composite wall separates combustion gases at 2600°C from a liquid
at 100°C, with respective coefficients of 50 and 1000 W/m2K.
The wall is composed of a layer of beryllium oxide 10 mm thick on the gas
side and a slab of stainless steel 20 mm thick on the liquid side. The
poor contact between the two gives rise to a resistance between the oxide
and the steel of 0.05 m2K/W.
What is the heat flux through the composite?
Sketch the temperature distribution from the gas to the liquid.
| Thermal conductivities; |
Beryllium oxide |
272 W/m.K |
| |
Stainless steel |
14.9 W/m.K. |
[33 900 W/m2]
-
A composite wall of height H and of unit depth perpendicular to the page
is insulated at its ends and is comprised of four different materials as
shown in the diagram below.
(a) sketch the analogue electrical circuit of the system;
(b) consider a wall for which H = 3.0 m, HB = HC
= 1.5 m, L1 = L3 = 0.05 m, L2 = 0.10 m,
kA = kD = 50 W/m.K, kB = 10 W/m.K, and
kC = 1 W/m.K. Under conditions for which
T¥,1 = 200°C, h1
= 50 W/m2K,
T¥,2 = 25°C, h2
= 10 W/m2K.
determine the rate of heat transfer through the wall. What are the interfacial
temperatures T1 and T2?
[3745 W; 173.8, 151.1°C]
-
A 0.2 m diameter thin-walled steel pipe is used to transport saturated
steam at an absolute pressure of 20 bar in a room for which the air temperature
is 25°C and the convection heat transfer coefficient at the outer surface
of the pipe is 20 W/m2K.
(a) Considering convection losses only determine the rate of heat loss
per metre length of pipe.
(b) Recalculate the heat loss on the assumption that the pipe has been
insulated with a 50 mm thick layer of magnesia (k = 0.28 W/m.K).
(c) The costs associated with generating steam and installing the insulation
are known to be £4 per 109 J and £100 per metre
length of pipe length respectively. If the steam line is to operate for
625 hours per month, how many months are needed to pay back the investment
in the insulation?
[2355 W/m, 661 W/m, 6.6 months]
-
A storage tank consists of a cylindrical section that has a length of 2
m and an inner diameter of 1 m. The end sections are hemispherical. The
tank is constructed from 20 mm thick glass (k = 1.4 W/m.K) and is exposed
to ambient air for which the temperature is 300 K and the convection coefficient
is 10 W/m2K. The tank is used to store heated oil that maintains
the inner surface at a temperature of 400 K.
Determine the electrical power needed to supply a submerged heater in
order to maintain the oil temperature.
[8700 W]
-
A hollow aluminium sphere (k = 237 W/m.K) with an electrical heater at
the centre is used to determine the thermal conductivity of insulating
materials. The inner and outer radii of the sphere are 0.15 and 0.18 m
respectively and the testing is done under steady state conditions with
the inner surface of the aluminium maintained at 250°C.
In a particular test a spherical insulating shell is cast on the outer
surface of the aluminium sphere to a depth of 0.12 m. The system is in
a room for which the air temperature is 20°C and the convection coefficient
from the sphere is 30 W/m2K. The heater dissipates 80 W.
Determine the thermal conductivity of the insulation.
[0.0621 W/m.K]
-
A hot cylinder is insulated with a layer of insulation of conductivity
k and loses heat to atmosphere from the surface of this insulation with
a heat transfer coefficient h. Show that the heat loss from the cylinder
will be a maximum when the outer surface of the insulation has a radius
of k/h. Find a typical radius for a lagged domestic hot water pipe.
Determine the equivalent critical radius for the insulation of a sphere,
and try to name an instance where insulating only as far as the critical
radius is a GOOD idea.
[r = 2k/h]
-
Calculate the thickness of insulating material of thermal conductivity
0.07 W/m.K necessary to reduce the heat loss from a hot-water tank to 25%
of the unlagged loss.
Assume that the tank is a perfect conductor and that the heat transfer
coefficients at the surface due to convection are 3.5 W/m2K
for the unlagged and 6.8 W/m2K for the lagged case. The dimensions
of the tank may be assumed to be sufficiently large for the areas of the
unlagged and lagged tank to be the same.
[70 mm]
-
North Sea oil enters the well head at 32°C and flows at a rate of 100kg/s
down 10 km of 0.9m OD steel pipe 1.6 cm thick, coated on the outer surface
with a 2 cm layer of protective material. Assuming that the average sea
temperature is 5°C and a linear temperature profile throughout the
length of the pipeline, what will be the exit temperature of the oil? What
would this temperature be for a 100 km pipeline?
| Thermal conductivity of steel |
= 40 W/m.K |
| Thermal conductivity of coating |
= 20 W/m.K |
| Heat transfer coefficient on outer surface |
= 30 W/m2K |
| Heat transfer coefficient on inner surface |
= 10 W/m2K |
| Specific heat capacity of oil |
= 2.2 kJ/kg.K |
[T = 15°C for 10 km,
for 100km common sense is required.]
-
Butyl rubber cement solution is to be stored at 460 K in a domed storage
vessel equipped with mechanical stirring to maintain a uniform temperature.
The designers require to estimate the maximum heat duty of the steam
heaters that will be required to maintain a full insulated tank at this
temperature in the depth of winter when the air temperature will be 260
K.
The vessel may be regarded as a 10 m high cylinder with one hemispherical
dome of internal diameter 10 m. The shell is an epoxy lined carbon steel
insulated by mineral wool and weather-proofed by thin aluminium sheeting
which may be regarded as a perfect conductor.
Use the following data to estimate the heat duty:
| |
wall thickness (m)
|
thermal conductivity (W/m.K)
|
|
epoxy coating
|
0.002
|
0.5
|
|
carbon steel
|
0.01
|
3.0
|
|
mineral wool
|
0.02
|
0.025
|
Heat transfer coefficient on outer surface = 15 W/m2K
Heat transfer coefficient on inner surface = 20 W/m2K
The contact coefficients between surfaces may be ignored and the vessel
may be assumed to be perfectly insulated on the ground face.
[74 kW]
-
A refrigerated room is to be constructed from brick 0.1m thick, insulated
externally by cork that is protected by wood 0.02m thick. Estimate the
thickness of cork that would be necessary to prevent ice forming on the
outside walls when the temperature of the inside wall is -10°C and
the ambient temperature is 20°C.
The thermal conductivities of brick, cork and wood are 10, 0.5 and
2 W/m.K respectively and the heat transfer coefficient at the external
surface is given by
h = 2(DT)0.5
where DT is the temperature difference
between the air and the external surface.
[0.018 m]
Heat exchanger tutorial questions
Click here for WORKED EXAMPLE
-
Water flows at a rate of 2.0 kg/s through a 40 mm internal diameter tube
of length 15.0 m. The water enters the tube at 25°C and the surface
temperature of the tube is constant at 90°C.
Calculate the temperature at which the water leaves the tube and the
corresponding heat transfer rate to the water.
Physical property data for water are given in Steam Tables. Assume a
mean water temperature of 50°C and check your assumption.
[79.5°C, 455.6 kW]
-
A cooling coil, consisting of a single length of tubing through which water
is circulated, is provided in a reaction vessel, the contents of which
are kept uniformly at 360 K by means of a stirrer. The inlet and outlet
temperatures of the cooling water are 280 K and 320 K respectively. What
would the outlet water temperature become if the length of the cooling
coil were increased 5 times? Assume the overall heat transfer coefficient
to be constant over the length of the tube and independent of the water
temperature.
[357.5 K]
-
Under what conditions, if any, would you recommend the use of co-current
rather than counter-current flow in a single pass heat exchanger?
A double pipe heat exchanger is used to cool a process liquid from 410
K to 350 K, with cooling water flowing through the annulus. The cooling
water enters at 285 K at a rate of 0.18 kg/s and the process liquid flows
at a rate of 0.23 kg/s. If the thermal resistance of the pipe wall can
be neglected, and the mean diameter of the pipe is 1.5 cm, estimate the
length of the heat exchanger required, assuming the flow to be counter-current.
Compare your answer with that required if co-current flow were used.
| Film coefficient of heat transfer for process
liquid |
= 2.3 kW/m2K |
| Film coefficient of heat transfer for water |
= 6.2 kW/m2K |
| Specific heat of process liquid |
= 2.3 kJ/kg.K |
| Specific heat of water |
= 4.18 kJ/kg.K |
[5.5 m; 6.7 m]
-
When designing a multi-pass heat exchanger the log mean temperature difference
calculated on the basis of true counterflow has to be corrected. Explain
why this is necessary and indicate the weaknesses of the method usually
adopted.
The feed to a distillation column is to be pre-heated from 290 K to
370 K in a 1-2 heat exchanger using the bottom product from the column
as the heating medium. If the bottom product leaves the column at 415 K
and is to be cooled to 365 K, determine whether an exchanger having 100
tubes, of mean diameter 2.5 cm and arranged in two passes, will be suitable.
The feed is passed at a rate of 5 kg/s through the tubes and the tube length
is 3 m.
| Overall coefficient of heat transfer |
= 1.5 kW/m2K |
| Specific heat of feed |
= 3.8 kJ/kg.K |
Comment upon:
-
the reliability of the design calculation carried out, bearing in mind
the value of F obtained;
-
the length to diameter ratio for the tubes used in the available heat exchanger.
[Satisfactory]
-
It is desired to warm an oil of specific heat 2.0 kJ/kg.K from 300 K to
325 K by passing it through a tubular heat exchanger with metal tubes of
inner diameter 10 mm. Along the outside of the tubes flows water, inlet
temperature 372 K, and outlet temperature 361 K.
The overall heat transfer coefficient from water to oil, based on the
inside area of the tubes, may be assumed constant at 230 W/m2K,
and 75 g/s of oil is to be passed through each tube. The oil is to make
two passes through the heater. The water makes one pass along the outside
of the tubes. Calculate the length of the tubes required.
[5.09 m]
-
A heat exchanger is required to cool continuously 20 kg/s of warm water
from 360 K to 335 K by means of 25 kg/s of cold water, inlet temperature
300 K. Assuming that the water velocities are such as to give an overall
efficient of heat transfer of 2 kW/m2K, assumed constant, calculate
the total area of surface required:
-
in a counterflow heat exchanger, i.e. one in which the hot and cold fluids
flow in opposite directions;
-
in a multi-pass heat exchanger, with the cold water making two passes through
the tubes, and the hot water making one pass along the outside of the tubes.
In case (b) assume that the hot-water flows in the same direction as the
inlet cold water, and that its temperature over any cross-section is uniform.
[27.95 m2; 30.06
m2]
-
A heat exchanger contains 450 tubes, each being 2 cm in diameter and 3
m long. Untreated pressurised water passes through the tubes where it is
heated from 410 K to 500 K by saturated steam condensing at 40 bar (gauge)
outside the tubes. The water flows at a total rate of 37.5 kg/s. Initially,
the heat exchanger was capable of attaining the water outlet temperature
of 500 K, but as time went on, this exit temperature dropped, and finally
stabilised at 470 K. If this loss of performance is assumed to be due to
scale formation on the inside of the tubes, estimate the thermal resistance
of this scale, assuming the tubes to be thin-walled and of negligible thermal
resistance.
What temperature must the saturated steam be raised to so that the water
exit temperature returns to its required value? Is this a good idea?
Specific heat of water = 4.18 kJ/kg K
[0.000376 m2K/W;
307°C]
-
A liquid has its temperature raised from 15°C to 65°C by passing
it through a heater in which the heating surface is maintained at 125°C
by condensing steam. If the overall coefficient of heat transfer can be
assumed to vary as the velocity raised to the power 0.8, what will be the
exit temperature of the liquid if its velocity is doubled? Assume liquid
thermal properties are temperature-independent over the range concerned.
[60.15°C]
-
A process liquid is heated in the tubes of a shell and tube heat exchanger,
where vapour condenses outside the tube. For a fixed flowrate of vapour,
the following values of the fluid velocity and the overall coefficient
of heat transfer were measured:
| v (m/s) |
1.000
|
1.139
|
1.322
|
1.564
|
1.898
|
2.378
|
| U (W/m2K) |
2174
|
2326
|
2500
|
2688
|
2924
|
3195
|
Regard the tubes as thin-walled and of negligible thermal resistance.
Use the above data to estimate the film heat transfer coefficient of heat
transfer of the condensing vapour, and the liquid film heat transfer coefficient
for a velocity of 0.8 m/s. State any assumptions made. (This form of data
investigation is called a WILSON PLOT).
[ho = 6015 W/m2K;
hi = 2866 W/m2K]
-
Air is being pre-heated by passing it through tubes, which have their temperature
held constant at 110°C by electrical heating. Normally, the air enters
at 15°C and leaves at 80°C. On a particular day, the air requirement
is increased by 50%. Can the heater deliver the increased flow of air without
the exit air temperature dropping below 75°C?
Assume that the thermal properties of air are independent of temperature
over the range concerned. State any other assumptions made.
[Yes]
-
In a multi-pass heat exchanger why is it necessary to correct the log mean
temperature difference based on true counterflow? Outline briefly the method
usually adopted.
A 1-4 heat exchanger (i.e. one shell-side pass, four tube-side passes)
is to be designed to heat liquid from 300 K to 370 K. The heating medium
enters the shell-side at 430 K and leaves at 380 K. If 10 kg/s of cold
liquid is supplied, find the heat transfer area required and suggest a
suitable tube arrangement.
If the hot fluid outlet temperature drops to 360 K, is the design method
still valid? If not, why not?
| Overall coefficient to heat transfer |
= 1.3 kW/m2K |
| Specific heat of both liquids |
= 3.8 kJ/kg K |
[34.2 m2, No]
-
The feed to a distillation column is to be pre-heated from 400 K to 510
K by passing it through the tubes of a shell and tube heat exchanger at
a rate of 30 kg/s. Saturated steam at 50 bar (absolute) is to condense
outside the tubes. A heat exchanger, containing 500 tubes of 2 cm diameter
and 3 m length, is available. Assuming the tubes to be thin-walled and
of negligible thermal resistance, determine whether this exchanger would
be suitable ("rating" the exchanger). The overall coefficient of heat transfer,
on a clean basis UC, is 3.2 kW/m2K and the fouling
resistance on the tube side is 0.00037 m2K/W. It may be assumed
that the condensing steam is clean.
If the heat exchanger cannot meet the conditions required, by how much
must the steam temperature be raised to meet the design specification?
Specific heat of tube-side fluid = 3.6 kJ/kg.K
[No, 15.4 deg C]
-
Derive, from first principles, the relationship that gives the cross-sectional
area "S" of shell-side flow perpendicular to the tube bundle as:
Show, with some numerical example as justification, why the above
can be approximated to:
[solution]
Heat exchanger examples
-
An aluminium kettle has a 20 cm diameter and a 1.2 mm thick bottom. The
heat load for boiling 0.833 grams per second of water at 100°C is 1883
W. Find the flame temperature and the kettle base temperature for the following
values of the heat transfer coefficients:
hi (boiling water) = 4000 W/m2K; ho
(gas flame) = 40 W/m2K
SOLUTION:
U = 106 ¸ 25256 = 39.6 W/m2K
Thus U is not much smaller than ho; the outside resistance
is the controlling resistance.
Q’ = 1883 W
A = p ´
10-2 m2. .
Q’ = UA (T0 - T3)
T3 = 100°C
T0 = 1615°C
Also Q’ = hoA (T0 - T1)
T1 = 115°C
From lectures:
(T1 - T2) = 0.35 deg K
T2 = 114.7°C
Alternatively, as a check: Q’ = hiA (T2 - T3)
T2 = 115°C
-
Water at 80°C flows through a copper pipe di = 1.8 cm, do
= 2.0 cm, k = 380 W/m.K. The surrounding air is at 20°C. Correlations
have been used to predict the values of the coefficients as:
hi = 8000 W/m2K; ho = 15 W/m2K.
Calculate the rate of heat loss per unit length of pipe.
SOLUTION:
The individual thermal resistances can be calculated:
Hence, Ro is controlling, and we can write:
or Uo = ho = 15 W/m2K
= 15 ´p´
0.020 ´ (80 - 20) = 56.6 W
-
The pipe in Example 2 is lagged with a 1 cm thickness of magnesia insulation
[k = 0.06 W/m.K]. The predicted outside transfer coefficient is ho
= 10 W/m2K. What is the percentage reduction in the rate of
heat loss?
SOLUTION:
We have four resistances in series:
(neglecting two small resistances)
Uo = 3.02 W/m2K (cf .15 W/m2K for unlagged
pipe)
For 1 metre length:
Q’ = 3.02 ´ (p´
0.04 ´ 1) ´
60 = 22.8 W
% Reduction in heat loss = [100 ´ (55.6
- 22.8)] ¸ 55.6 = 59%
-
A stream of oil, with specific heat 2.4 kJ/kg.K, flowing at 1000 kg/hr
is to be cooled from 130 to 80°C in a double pipe heat exchanger, using
1200 kg/hr water at 20°C as the cooling medium. The predicted overall
heat transfer coefficient, based on the outside diameter of the insider
pipe, is 360 W/m2K. Find the heat transfer area required if
the flow is to be (a) co-current and (b) counter-current.
SOLUTION:
(a)
Q’ = m’A CPA (TA1 - TA2)
= m’B CPB (TB2 - TB1)
= 1000 ´ 2400 ´
50 = 1200 ´ 4200 ´
(TB2 - 20)
TB2 = 44°C
(b) Q’ and TB2 will be the same
Note: counter-current flow requires less area for the same terminal
temperature.
-
A double pipe heat exchanger contains a 6m long tube of 5cm OD. It is being
used to condense 100 kg/hr of saturated steam at atmospheric pressure.
Cooling water enters the tubes at 25°C and leaves at 38°C. Calculate
the water flow rate m’W (kg/s) and the observed overall heat
transfer coefficient.
SOLUTION:
One phase is at constant temperature, so although this type of exchanger
does not provide true counter-current or co-current flow, we may still
use:
Q’ = UA DTLM
The rate at which the condensing steam gives up heat is given by the energy
balance equation:
Q’ = m’S lfg
where the enthalpy of condensation of steam, lfg,
at 1 atm is 2260 kJ/kg (from steam tables).
Q’ = (100 ¸ 3600) ´
2260 = 62.8 kW
Heat is transferred into the cooling water at the same rate:
Q’ = m’W CP (t1-t2)
62.8 = m’W ´ 4.18 ´
(38 - 25)
m’W = 1.16 kg/s
Area of outside of tubes:
Ao = p ´
0.05 ´ 6 = 0.3p
m2
Note that the arithmetic mean (= 68.5) could have been used in this case.
Radiation tutorial problems (view factors)
Click here for WORKED EXAMPLE
-
Without reference to tables or charts calculate the factors F12
and F21 for each of the following configurations;
[0.5,
0.3714; 1, 0.4142]
-
A cube of 0.6 m side has a disc of 0.2 m diameter placed in the centre
of the base. Determine the view factors between;
-
the disc and the inside of the cube
-
the inside of the cube and the disc
-
that part of the cube base not covered by the disc and the inside surface
-
the inside surface of the cube and that part of the base not covered by
the disc
[1, 0.0175, 1, 0.1825]
-
Two surfaces at right angles one 0.3 ´
0.6 m and the other 0.3 ´ 0.7 m share
a common short edge. Making use of the appropriate chart determine the
two view factors of the surfaces relative to each other.
Each long surface is divided into two equal parts by a line perpendicular
to its longer edge. Determine the view factors of the two surfaces remote
from the common edge relative to each other.
[0.1326, 0.1547; 0.0280,
0.0326]
-
A ring of 0.8 m outside and 0.4 m inside diameter lies 0.5 m above a smaller
ring of 0.4 m outside and 0.2 m inside diameter. The two discs are concentric
and parallel. Determine the view factor of the larger ring with reference
to the smaller one.
[0.2425]
Radiation tutorial worked example (view
factors)
Determine view factors F12 and F21 for the following
geometries:
-
Sphere (1) of inside a cubical box (2) of side length L equal to sphere
diameter D
-
Diagonal partition (1) within a long square duct (2 and 3)
-
End (1 or 3) and inner side (2) of a circular cylinder of equal length
L and diameter D.
SOLUTIONS
(a) As the sphere is convex, no radiation will reach one part of its
surface from another, i.e. all radiation from the sphere goes to the box
F12 = 0
Rule of reciprocity: A1F12 = A2F21
Surface areas are p D2 for the
sphere and 6D2 for the box:
i.e. 52.36% of the radiation from the box goes to the sphere. The other
47.64% travels between different faces of the box.
(b) Rule of summation: F11 + F12 + F13
= 1
Surface 1 is perfectly flat: F11 = 0
By symmetry F12 = F13
F12 = 0.5 = F13
Rule of reciprocity: A1F12 = A2F21
For unit length of duct, areas are L for surfaces 2 and 3, and LÖ
2 for 1:
i.e. 70.71% of the radiation from the bottom face of the enclosure goes
to the side face. The other 29.29% goes to the diagonal partition.
(c) Using formulae for coaxial parallel discs:
Surface 1 is perfectly flat: F11 = 0
Rule of summation: F11 + F12 + F13
= 1
F12 = 1 - 0 - 0.17157 = 0.82843
Rule of reciprocity: A1F12 = A2F21
For circular cylinder, areas are 0.25p D2
for surface 1 and p D2 for surface
2:
i.e. 20.71% of the radiation from the side face of the cylinder goes to
each of the end faces. The other 58.58% goes back to the side face.
Radiation tutorial problems
-
Two parallel square plates, each with sides measuring 2.00 metres, are
separated by a distance of one metre. The plates may be considered as black
bodies at temperatures of 500°C and 1000°C respectively. The plates
are placed in a large room at 20.0°C. Ignoring heat transfer from the
rear of the plates, determine the net rate of radiative heat transfer to
or from each plate and the net rate of heat transfer to the surroundings.
[561 kW from hot plate, 167
kW to cold plate, 394 kW to surroundings]
-
A circular plate of 1m diameter is heat treated by mounting it opposite
a hemi-spherical dome of the same diameter. The temperature of the plate
is 400°C and that of the dome is 850°C. Both surfaces may be assumed
to be perfectly black. The distance between the plate and the bottom of
the dome is 0.50 m. The surfaces are mounted in large surroundings at 15°C.
Ignoring heat transfer from the rear of the plate, determine the net rate
of radiative heat transfer to the plate.
[18 kW]
-
Two 2 m square black parallel plates are placed a metre apart and the sides
of the resulting box enclosed by well insulated walls. The upper plate
is at 1000°C and the lower one at 500°C. Determine the mean
temperature of the side walls.
It is found that in fact there is a heat loss through the side walls
of 10 kW/m2. Determine the mean temperature of the insulated
walls for this case and the net amount of heat transferred to the lower
plate.
[832°C, 771°C, 412
kW]
-
A vessel for producing steam contains water at 100°C and is
mounted on insulated walls 1.00 m above a heater. Both the heater and the
vessel have diameters of 1.50 metres and the heater is at 1500°C.
Determine the rate of radiative heat transfer to the vessel assuming
the vessel and heating surfaces to be black.
What is the percentage reduction in radiative heat transfer to the vessel
if the cylindrical sides of the system are open to surroundings at 10.0°C?
[656 kW, 55.6%]