Process Heat Transfer Lec 3: Heat Conduction Equation
Transcript of Process Heat Transfer Lec 3: Heat Conduction Equation
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Steady-State Conduction without Thermal Energy Generation
Process Heat Transfer
Lec 3: Heat Conduction Equation
Dr. Zayed Al-Hamamre
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One-Dimensional, Steady-State Conduction without Thermal Energy Generation
o Plane Wall
o Tube and cylinders
o Spherical shell
Content
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• Specify appropriate form of the heat equation.
• Solve for the temperature distribution.
• Apply Fourier’s law to determine the heat flux.
Simplest Case: One-Dimensional, Steady-State Conduction with No Thermal Energy
Generation.
• Common Geometries:
– The Plane Wall: Described in rectangular (x) coordinate. Area
perpendicular to direction of heat transfer is constant (independent of x).
– The Tube Wall: Radial conduction through tube wall.
– The Spherical Shell: Radial conduction through shell wall.
Methodology of a Conduction Analysis
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Consider a plane wall between two fluids of different temperature:
The Plane Wall
• Implications:
Heat Equation:
• Boundary Conditions: ,1 ,20 , s sT T T L T
• Temperature Distribution for Constant k :k
For steady-state conditions with no distributed
source or sink of energy within the wall
the heat flux is a constant, independent of x
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• Heat Flux and Heat Rate:
Thermal Resistances and Thermal Circuits:
o Conduction in a plane wall:
o Convection
:o Thermal circuit for plane wall with adjoining fluids:
The Plane Wall
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Composite Wall with Negligible Contact Resistance:
The Plane Wall
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Overall Heat Transfer Coefficient (U) :
A modified form of Newton’s Law of Cooling to encompass multiple resistances
to heat transfer.
Where
The Plane Wall
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Series – Parallel Composite Wall:
The Plane Wall
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Series – Parallel Composite Wall:
The Plane Wall
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• Note departure from one-dimensional conditions
for .
• Circuits based on assumption of isothermal
surfaces normal to x direction or adiabatic
surfaces parallel to x direction provide
approximations for qx .
Series – Parallel Composite Wall:
The Plane Wall
∦kF kG
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The Plane Wall
Series – Parallel Resistances :
Thermal Resistance for Unit Surface Area:
,t condL
Rk
,1
t convRh
Units: W/KtR 2m K/WtR
,1
t radr
Rh
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The Plane Wall
Contact Resistance:
In composite systems, the temperature drop
across the interface between materials may
be appreciable.
This temperature change is attributed to what
is known as the thermal contact resistance
,,
t ct c
c
RR
A
,
A Btc
x
T TR
q
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Contact Resistance:
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To reduce the heat loss rate, a person wears special sporting gear (snow suit and wet suit) made
from a nanostructured silica aerogel insulation with an extremely low thermal conductivity of
0.014 W/m K. Consider surroundings conditions (air or water) are at 10oC. The emissivity of the
outer surface of the snow and wet suits is 0.95. What thickness of aerogel insulation is needed to
reduce the heat loss rate to 100 W (a typical metabolic heat generation rate) in air and water?
What are the resulting skin temperatures?
Example
For air
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Example cont.
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Example cont.
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Example cont.
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• Heat Equation:
Cylindrical tube and shell
• Temperature Distribution for Constant k :
Given that
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• Heat Flux and Heat Rate:
Conduction Resistance:
Why is it inappropriate to base the thermal resistance on a unit surface area?
K/W
Cylindrical tube and shell
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Composite Wall with Negligible Contact Resistance
Cylindrical tube and shell
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Cylindrical tube and shell
This definition is arbitrary, and the overall coefficient may also be defined in terms
of A4 or any of the intermediate areas.
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1-
22Process Heat Transfer
Cylindrical tube and shell
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Cylindrical tube and shell
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Critical Thickness of Insulation
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Example
Insulation thickness is
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Example cont.
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• Heat Equation
Spherical Shell
• Temperature Distribution for Constant k :
= 0.0
But
1/,1 ,1 ,2
1 2
1
1 /s s s
r rT r T T T
r r
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• For Composite Shell:
and
and
Spherical Shell
for steady-state conditions with no heat generation and no heat loss
from the sides
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A 3-m internal diameter spherical tank made of 2-cm-thick stainless steel (k 15 W/m · °C) is
used to store iced water at T1 = 0°C. The tank is located in a room whose temperature is T2 =
22°C. The walls of the room are also at 22°C. The outer surface of the tank is black and heat
transfer between the outer surface of the tank and the surroundings is by natural convection and
radiation. The convection heat transfer coefficients at the inner and the outer surfaces of the tank
are h1 80 W/m2 · °C and h2 10 W/m2 · °C, respectively. Determine (a) the rate of heat transfer
to the iced water in the tank and (b) the amount of ice at 0°C that melts during a 24-h period.
Example
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Example cont.
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Example cont.
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Example cont.
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the amount of ice that will melt during a 24-h period is
Example cont.
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Example
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Assessment of thermal barrier coating (TBC) for protection of turbine blades. Determine
maximum blade temperature with and without TBC.
Schematic:
Example cont.
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With a heat flux of
ANALYSIS: For a unit area, the total thermal resistance with the TBC is
Example cont.
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Example cont.