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Lecture Notes for CO2 (Part 1) 1 D STEAD STATE HEAT CONDUCTION Wan Azmi bin Wan Hamzah Universiti Malaysia Pahang Week   3

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Lecture Notes for CO2 (Part 1)1 D STEADY STATE HEAT

CONDUCTION

Wan Azmi bin Wan HamzahUniversiti Malaysia Pahang

Week  – 3

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Course Outcome 2 (CO2)

Students should be able to understand and

evaluate one-dimensional heat flow and indifferent geometries

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Lesson Outcomes from CO2 (Part 1)

To derive the equation for temperature

distribution in various geometries 

Thermal Resistance concept  – to derive 

expression for various geometries 

To evaluate the heat transfer using thermal

resistance in various geometries

To evaluate the critical radius of insulation

To evaluate heat transfer from the rectangular fins

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BOUNDARY AND INITIAL CONDITIONS A heat transfer problem must equipped with a description of the thermal

conditions at the bounding surfaces of the medium.

Boundary conditions: The mathematical expressions of the thermalconditions at the boundaries.

The initial condition specified at time t =  0, ,

which is a mathematical expression for thetemperature distribution of the medium

initially.

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• Specified Temperature Boundary Condition

• Specified Heat Flux Boundary Condition

• Convection Boundary Condition

• Radiation Boundary Condition

• Interface Boundary Conditions

• Generalized Boundary Conditions 

Boundary Conditions

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• Specified Temperature Boundary Condition

• Specified Heat Flux Boundary Condition

• Convection Boundary Condition

• Radiation Boundary Condition

• Interface Boundary Conditions

• Generalized Boundary Conditions

Boundary Conditions

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1 Specified Temperature Boundary Condition

For one-dimensional heat transfer througha plane wall of thickness L, the specified

temperature boundary conditions can be

expressed as

where T 1 and T 2 are the specified

temperatures at surfaces at x = 0 and

 x = L, respectively.

The specified temperatures can be

constant, which is the case for steady

heat conduction, or may vary with time.

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• Specified Temperature Boundary Condition

• Specified Heat Flux Boundary Condition

• Convection Boundary Condition

• Radiation Boundary Condition

• Interface Boundary Conditions

• Generalized Boundary Conditions

Boundary Conditions

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2 Specified Heat Flux Boundary Condition

The heat flux in the positive x -direction anywhere in the

medium, including the boundaries

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Special Case 1: Insulated Boundary

 A well-insulated surface is a surface with

heat flux is zero. Then the boundary

condition on a perfectly insulated surface

(at x = 0,) can be expressed as

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Special Case 2: Thermal Symmetry

Two surfaces of thickness L exposed to the same

thermal conditions, and thus the temperature

distribution in one half of the plate is the same as

that in the other half.

Thus, the heat transfer in this plate possesses

thermal symmetry about the center plane at x = L/2.

Therefore, the center plane can be viewed as an

insulated surface, and the thermal condition at

this plane of symmetry can be expressed as

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• Specified Temperature Boundary Condition

• Specified Heat Flux Boundary Condition

• Convection Boundary Condition

• Radiation Boundary Condition

• Interface Boundary Conditions

• Generalized Boundary Conditions

Boundary Conditions

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3 Convection Boundary Condition

The convection boundary conditions on both surfaces in the

figure can be expressed as:

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• Specified Temperature Boundary Condition

• Specified Heat Flux Boundary Condition

• Convection Boundary Condition

• Radiation Boundary Condition

• Interface Boundary Conditions

• Generalized Boundary Conditions

Boundary Conditions

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4 Radiation Boundary Condition

The radiation boundary conditions in the figure

can be expressed as

Radiation boundary condition on a surface:

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• Specified Temperature Boundary Condition

• Specified Heat Flux Boundary Condition

• Convection Boundary Condition

• Radiation Boundary Condition

• Interface Boundary Conditions

• Generalized Boundary Conditions

Boundary Conditions

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5 Interface Boundary Conditions

Interface boundary conditions are based

on

(1) two bodies must have the sametemperature at the area of contact

(2) an interface surface cannot store any

energy, and thus the heat flux  on the two

sides of an interface must be the same.

The boundary conditions at the interface

of two bodies A and B in perfect contact at

 x =  x 0 can be expressed as

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• Specified Temperature Boundary Condition

• Specified Heat Flux Boundary Condition

• Convection Boundary Condition

• Radiation Boundary Condition

• Interface Boundary Conditions

• Generalized Boundary Conditions 

Boundary Conditions

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6 Generalized Boundary Conditions

In general, however, a surface may involve convection,

radiation, and specified heat flux simultaneously.The boundary condition in such cases is again obtained

from a surface energy balance, expressed as

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HEAT GENERATION IN A SOLID

Many practical heat transfer applications

involve the conversion of some form of energy

into thermal energy in the medium.

The process involve internal heat generation, 

which explain by a rise in temperature

throughout the medium.

Some examples of heat generation are

- resistance heating  in wires,

- chemical reactions in a solid, and

- nuclear reactions in nuclear fuel rods

where electrical, chemical, and nuclear

energies are converted to heat, respectively.

Heat generation in an electrical wire of outer

radius r o and length L can be expressed as

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The main parameters involve are surface

temperature T s and the maximum temperature

T max that occurs in the medium in steady  

operation. Thus, the energy balance become:

and

Thus, Eq. 2.66

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When inner medium of cylinder generate

heat and transfer the heat to the outer

surface as shown in Fig. 2-55

where and

become

Where T0 is centerline temperature ofcylinder, which is the maximum

temperature

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For plane wall

and sphere

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VARIABLE THERMAL CONDUCTIVITY, k (T )

When the variation of thermal conductivity with

temperature in a specified temperature interval is

large, it may be necessary to account for thisvariation to minimize the error.

When the variation of thermal conductivity with

temperature k (T ) is known, the average value of

the thermal conductivity in the temperature range

between T 1 and T 2 can be determined from

Th i ti i th l d ti it f t i l ith

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temperature coefficient

of thermal conductivity.

The average value of thermal conductivity

in the temperature range T 1 to T 2 in this

case can be determined from

The average thermal conductivity  in this

case is equal to the thermal conductivity

value at the average temperature.

The variation in thermal conductivity of a material with

temperature can be approximated as a linear function and

expressed as

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Problem 1

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When a long section of a compressed air line passes

through the outdoors, it is observed that the moisture in

the compressed air freezes in cold weather, disrupting

and even completely blocking the air flow in the pipe. Toavoid this problem, the outer surface of the pipe is

wrapped with electric strip heaters and then insulated.

Consider a compressed air pipe of length L= 6 m, inner

radius r 1 =3.7 cm, outer radius r 2= 4.0 cm, and thermal

conductivity k=14 W/m·°C equipped with a 300-W strip

heater. Air is flowing through the pipe at an averagetemperature of -10°C, and the average convection heat

transfer coefficient on the inner surface is h=30 W/m2·°C.

 Assuming 15 percent of the heat generated in the strip

heater is lost through the insulation, (a) express the

differential equation and the boundary conditions for

steady one-dimensional heat conduction through thepipe, (b) obtain a relation for the

in the pipe material by solving the differential equation,

and (c) evaluate the inner and outer surface

temperatures of the pipe.

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 A spherical container of inner radius r 1=2 m, outer radius r 2=2.1 m, and

thermal conductivity k=30 W/m·°C is filled with iced water at 0°C. The

container is gaining heat by convection from the surrounding air at 25°C with

a heat transfer coefficient of h=18 W/m2·°C. Assuming the inner surface

temperature of the container to be 0°C, (a) express the differential equation

and the boundary conditions for steady one-dimensional heat conduction

through the container, (b) obtain a relation for the variation of temperature in

the container by solving the differential equation, and (c) evaluate the rate of

heat gain to the iced water.

Problem 2

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Solution

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P bl 3

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In a food processing facility, a spherical container of inner radius r 1=40 cm,

outer radius r 2=41 cm, and thermal conductivity k=1.5 W/m·°C is used to store

hot water and to keep it at 100°C at all times. To accomplish this, the outer

surface of the container is wrapped with a 500-W electric strip heater andthen insulated. The temperature of the inner surface of the container is

observed to be nearly 100°C at all times. Assuming 10 percent of the heat

generated in the heater is lost through the insulation, (a) express the

differential equation and the boundary conditions for steady one-dimensional

heat conduction through the container, (b) obtain a relation for the variation of

temperature in the container material by solving the differential equation, and(c) evaluate the outer surface temperature of the container. Also determine

how much water at 100°C this tank can supply steadily if the cold water enters

at 20°C.

Problem 3

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Solution

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