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Ahmet Çelik
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Chapter 2: Introduction to Conduction

MECH302

Source files used: late Heat Transfer (03), Heat Transfer (04), Heat Transfer (05); textbook Chapter 2 as support. No worked examples are included.

1. Big Picture

Chapter 1 introduced conduction with Fourier’s law. Chapter 2 answers the next question:

How do we find the temperature distribution inside a solid?\text{How do we find the temperature distribution inside a solid?}

This is Biddle’s repeated conduction logic:

First find T(x,y,z,t), then use Fourier’s law to find heat transfer.\boxed{\text{First find }T(x,y,z,t),\text{ then use Fourier’s law to find heat transfer.}}

In Chapter 1, simple wall problems already had known surface temperatures, so heat transfer could be found directly. In Chapter 2, we learn how to pose conduction problems using the heat diffusion equation plus boundary and initial conditions.

The chapter is not mainly about solving every PDE by hand. It is about knowing what equation applies and what conditions must be specified for the problem to be well posed.


2. Core Ideas

2.1 Temperature Distribution Comes First

In conduction, heat flux depends on the temperature gradient:

qx=kdTdxq_x''=-k\frac{dT}{dx}

So if we do not know how temperature varies with position, we cannot calculate heat flux. Chapter 2 gives the governing equation that determines TT.

The general sequence is:

Physical problem → assumptions → heat diffusion equation → boundary/initial conditions → temperature distribution → Fourier’s law → heat rate or heat flux


2.2 Thermal Conductivity kk

Thermal conductivity measures how easily a material conducts heat.

  • Large kk: metal-like behavior, temperature drop is small for a given heat flow.
  • Small kk: insulation-like behavior, temperature drop is large for a given heat flow.

Units:

[k]=W/(m\cdotK)[k]=\text{W/(m\cdot K)}

Biddle emphasizes using property tables correctly. Metals, nonmetals, building materials, insulation materials, liquids, and gases appear in different appendices/tables. Some tabulated values, especially thermal diffusivity, may be written in scaled form such as α×106\alpha\times10^6. Read the table heading carefully.


2.3 Thermal Diffusivity α\alpha

Thermal diffusivity is:

α=kρcp\alpha=\frac{k}{\rho c_p}

where:

  • kk: thermal conductivity, W/(m·K),
  • ρ\rho: density, kg/m³,
  • cpc_p: specific heat, J/(kg·K),
  • α\alpha: thermal diffusivity, m²/s.

Physical meaning:

thermal diffusivity=ability to conduct heatability to store heat\text{thermal diffusivity} = \frac{\text{ability to conduct heat}}{\text{ability to store heat}}

Large α\alpha means the material responds quickly to thermal changes. Small α\alpha means the material responds slowly because it stores energy strongly or conducts poorly.

Do not confuse thermal diffusivity α\alpha with absorptivity α\alpha from radiation. Same Greek letter, different context.


2.4 Heat Generation

Some solids generate heat internally. Examples:

  • electrical resistance heating,
  • nuclear fuel,
  • chemical reaction,
  • volumetric energy generation in a material.

The volumetric generation term is usually written:

q˙\dot{q}'''

with units:

W/m3\text{W/m}^3

Generation changes the temperature distribution. With no generation and constant kk, a 1D steady plane wall has a linear temperature profile. With generation, the profile becomes curved.


2.5 Boundary and Initial Conditions

A conduction differential equation is not enough by itself. Biddle emphasizes that a problem is properly posed only when the governing equation and the correct boundary/initial conditions are specified.

For a second-order spatial equation, you need two boundary conditions per spatial direction. If time appears, you also need an initial condition.

Typical boundary conditions:

  1. specified surface temperature,
  2. specified heat flux,
  3. insulated or symmetry boundary,
  4. convection boundary,
  5. radiation boundary,
  6. interface between two materials.

3. Main Governing Equations and Formulas

3.1 Thermal Diffusivity

α=kρcp\alpha=\frac{k}{\rho c_p}

Use when transient conduction appears or when comparing how quickly materials respond thermally.


3.2 General Heat Diffusion Equation: Cartesian Coordinates

For constant properties:

2Tx2+2Ty2+2Tz2+q˙k=1αTt\frac{\partial^2 T}{\partial x^2}+\frac{\partial^2 T}{\partial y^2}+\frac{\partial^2 T}{\partial z^2}+\frac{\dot{q}'''}{k}=\frac{1}{\alpha}\frac{\partial T}{\partial t}

where:

  • TT: temperature,
  • x,y,zx,y,z: spatial coordinates,
  • q˙\dot{q}''': volumetric heat generation, W/m³,
  • kk: thermal conductivity,
  • α\alpha: thermal diffusivity,
  • tt: time.

Use this for transient, multidimensional conduction with constant properties.

Special cases:

Steady state:

Tt=0\frac{\partial T}{\partial t}=0

No generation:

q˙=0\dot{q}'''=0

One-dimensional, steady, no generation:

d2Tdx2=0\frac{d^2T}{dx^2}=0

One-dimensional, steady, with generation:

d2Tdx2+q˙k=0\frac{d^2T}{dx^2}+\frac{\dot{q}'''}{k}=0

3.3 Cylindrical Heat Diffusion Equation

For constant properties:

1rr(rTr)+1r22Tϕ2+2Tz2+q˙k=1αTt\frac{1}{r}\frac{\partial}{\partial r}\left(r\frac{\partial T}{\partial r}\right) +\frac{1}{r^2}\frac{\partial^2 T}{\partial \phi^2} +\frac{\partial^2 T}{\partial z^2} +\frac{\dot{q}'''}{k} =\frac{1}{\alpha}\frac{\partial T}{\partial t}

Common radial-only steady form:

1rddr(rdTdr)+q˙k=0\frac{1}{r}\frac{d}{dr}\left(r\frac{dT}{dr}\right)+\frac{\dot{q}'''}{k}=0

If no generation:

1rddr(rdTdr)=0\frac{1}{r}\frac{d}{dr}\left(r\frac{dT}{dr}\right)=0

Use cylindrical coordinates for pipes, tubes, rods, wires, and cylinders.


3.4 Spherical Radial Heat Diffusion Equation

For radial conduction in a sphere with constant properties:

1r2ddr(r2dTdr)+q˙k=1αTt\frac{1}{r^2}\frac{d}{dr}\left(r^2\frac{dT}{dr}\right)+\frac{\dot{q}'''}{k}=\frac{1}{\alpha}\frac{\partial T}{\partial t}

Steady, no generation:

1r2ddr(r2dTdr)=0\frac{1}{r^2}\frac{d}{dr}\left(r^2\frac{dT}{dr}\right)=0

Use for spheres and spherical shells.


3.5 Fourier’s Law in Vector Form

q=kT\vec q''=-k\nabla T

In Cartesian components:

qx=kTx,qy=kTy,qz=kTzq_x''=-k\frac{\partial T}{\partial x},\qquad q_y''=-k\frac{\partial T}{\partial y},\qquad q_z''=-k\frac{\partial T}{\partial z}

Use after TT is known.


3.6 Boundary Condition: Specified Temperature

Ts=T0T_s=T_0

Use when the surface is maintained at a known temperature.

Example language:

  • “surface is kept at 100°C,”
  • “wall is maintained at T1T_1,”
  • “constant surface temperature.”

3.7 Boundary Condition: Specified Heat Flux

kTn=qs-k\frac{\partial T}{\partial n}=q_s''

where nn is the outward normal direction.

Use when a known heat flux is imposed at the surface, such as a heater attached to a wall.

For adiabatic or insulated surfaces:

qs=0q_s''=0

so

Tn=0\frac{\partial T}{\partial n}=0

This same mathematical condition also appears at a symmetry plane.


3.8 Boundary Condition: Convection

kTn=h(TsT)-k\frac{\partial T}{\partial n}=h(T_s-T_\infty)

Use when conduction inside the solid reaches a surface and then heat leaves by convection to a fluid.

This is one of the most important boundary conditions in the course. It connects conduction in the solid to convection at the surface.


3.9 Boundary Condition: Radiation

kTn=εσ(Ts4Tsur4)-k\frac{\partial T}{\partial n}=\varepsilon\sigma\left(T_s^4-T_{\text{sur}}^4\right)

Use when a surface loses or gains heat by radiation to surroundings.

Temperatures must be in K.


3.10 Interface Conditions

For perfect contact between materials A and B:

Temperature continuity:

TA=TBT_A=T_B

Heat flux continuity:

kATAn=kBTBnk_A\frac{\partial T_A}{\partial n}=k_B\frac{\partial T_B}{\partial n}

Use at material interfaces.

If thermal contact resistance is specified, use the Chapter 3 contact resistance model instead of perfect temperature continuity.


4. Problem-Solving Workflow

  1. Identify the geometry. Plane wall, cylinder, sphere, or multidimensional shape.
  2. Choose coordinates. Cartesian for plane walls/rectangles; cylindrical for pipes/tubes; spherical for spheres.
  3. List assumptions. Steady/transient, 1D/2D/3D, generation/no generation, constant properties.
  4. Simplify the heat diffusion equation. Remove terms that do not apply.
  5. Write boundary conditions. Use physical information from the problem statement.
  6. Write initial condition if transient. Usually T(x,y,z,0)=TiT(x,y,z,0)=T_i.
  7. Solve or recognize the required method. Analytical solution, resistance method, transient chart, or numerical method.
  8. Use Fourier’s law after temperature is known. Do not skip directly to heat rate unless a resistance/rate formula applies.

5. Decision Rules / Decision Trees

5.1 Which Governing Equation?

Plane wall / rectangular coordinates? → Cartesian heat equation

Pipe, tube, rod, cylinder? → Cylindrical heat equation

Sphere or spherical shell? → Spherical heat equation

5.2 Which Terms Stay?

Steady state? → remove time derivative

No generation? → remove q˙/k\dot{q}'''/k term

1D in x only? → keep only d2T/dx2d^2T/dx^2

Radial cylinder only? → keep only (1/r)d/dr(rdT/dr)(1/r)\,d/dr(r\,dT/dr)

5.3 Boundary Condition Selection

Surface temperature given? → T=specified valueT=\text{specified value}

Surface heat flux given? → kdT/dn=qs-k\,dT/dn=q_s''

Insulated surface? → dT/dn=0dT/dn=0

Symmetry line/plane? → dT/dn=0dT/dn=0

Surface exposed to fluid with hh and TT_\infty? → kdT/dn=h(TsT)-k\,dT/dn=h(T_s-T_\infty)

Surface exchanges radiation? → kdT/dn=εσ(Ts4Tsur4)-k\,dT/dn=\varepsilon\sigma(T_s^4-T_{\text{sur}}^4)

5.4 When Is a Problem Properly Posed?

Spatial second-order equation? → need two boundary conditions per spatial coordinate

Transient problem? → need initial condition

Boundary conditions missing? → cannot solve uniquely


6. Important Tables / Correlations Needed

6.1 Property Table Use

Biddle’s table-use logic:

Material/Property NeedWhere to Look Conceptually
Metalsmetallic property tables
Nonmetallic solidsnonmetallic property tables
Building materials and insulationstructural/insulation tables
Liquidsliquid property tables
Gasesgas property tables

Key warning: when a table heading says α×106\alpha \times 10^6, the listed number is not α\alpha. It means:

α=(listed number)×106 m2/s\alpha=(\text{listed number})\times10^{-6}\ \text{m}^2/\text{s}

6.2 Common Material Behavior

Material TypeTypical Behavior
Metalshigh kk, conduct heat well
Insulationlow kk, large temperature drop for small heat rate
Liquidsmoderate thermal properties; convection often important
Gaseslow kk; convection coefficients often small

7. Key Takeaways

  • In conduction, find TT first, then use Fourier’s law.
  • Thermal conductivity kk measures conduction ability.
  • Thermal diffusivity α=k/(ρcp)\alpha=k/(\rho c_p) measures how fast temperature responds.
  • The heat diffusion equation is simplified based on assumptions.
  • Boundary conditions are physical statements translated into math.
  • A convection boundary condition connects conduction inside the solid to convection outside.
  • An insulated boundary and a symmetry boundary both give zero normal temperature gradient.
  • For radiation boundary conditions, use K.
  • Read property tables carefully, especially scaled columns.