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M.Sc.-II(Physics)�Thermal Properties

ISSUES TO ADDRESS...

• How do materials respond to the application of heat?

• How do we define and measure...

-- heat capacity?

-- thermal expansion?

-- thermal conductivity?

-- thermal shock resistance?

• How do the thermal properties of ceramics, metals, � and polymers differ?

Chapter 19 -

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Heat Capacity

2

• Quantitatively: The energy required to produce a unit rise in � temperature for one mole of a material.

heat capacity

(J/mol-K)

energy input (J/mol)

temperature change (K)

Two ways to measure heat capacity:� Cp : Heat capacity at constant pressure.

Cv : Heat capacity at constant volume.

Cp usually > Cv

• Heat capacity has units of

The ability of a material to absorb heat

Chapter 19 -

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Dependence of Heat Capacity on Temperature

3

Heat capacity...

-- increases with temperature

-- for solids it reaches a limiting value of 3R

• From atomic perspective:

-- Energy is stored as atomic vibrations.

-- As temperature increases, the average energy of � atomic vibrations increases.

Adapted from Fig. 19.2, Callister & Rethwisch 8e.

R = gas constant

3R

= 8.31 J/mol-K

Cv = constant

Debye temperature

(usually less than T

room

)

T (K)

θ

D

0

0

Cv

Chapter 19 -

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Atomic Vibrations

Atomic vibrations are in the form of lattice waves or phonons

4

Adapted from Fig. 19.1, Callister & Rethwisch 8e.

Chapter 19 -

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Specific Heat: Comparison

5

increasing cp

• Why is cp significantly

larger for polymers?

Selected values from Table 19.1, Callister & Rethwisch 8e.

Polymers

Polypropylene

Polyethylene

Polystyrene

Teflon

cp (J/kg-K)

at room T

Ceramics

Magnesia (MgO)

Alumina (Al2O3)

Glass

Metals

Aluminum

Steel

Tungsten

Gold

1925

1850

1170

1050

900

486

138

128

cp (specific heat): (J/kg-K)

Material

940

775

840

Cp (heat capacity): (J/mol-K)

Chapter 19 -

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Thermal Expansion

6

Materials change size when temperature � is changed

linear coefficient of

thermal expansion (1/K or 1/ºC)

Tinitial

Tfinal

initial

final

Tfinal > Tinitial

Chapter 19 -

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Atomic Perspective: Thermal Expansion

7

Adapted from Fig. 19.3, Callister & Rethwisch 8e.

Asymmetric curve:

-- increase temperature, � -- increase in interatomic � separation � -- thermal expansion

Symmetric curve:

-- increase temperature, � -- no increase in interatomic � separation � -- no thermal expansion

Chapter 19 -

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Coefficient of Thermal Expansion: Comparison

8

• Q: Why does α

generally decrease

with increasing

bond energy?

Polypropylene

145-180

Polyethylene

106-198

Polystyrene

90-150

Teflon

126-216

Polymers

Ceramics

Magnesia (MgO)

13.5

Alumina (Al2O3)

7.6

Soda-lime glass

9

Silica (cryst. SiO2)

0.4

Metals

Aluminum

23.6

Steel

12

Tungsten

4.5

Gold

14.2

α(10-6/°C)�at room T

Material

Selected values from Table 19.1, Callister & Rethwisch 8e.

Polymers have larger α values because of weak secondary bonds

increasing α

Chapter 19 -

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Thermal Expansion: Example

Ex: A copper wire 15 m long is cooled from �40 to -9ºC. How much change in length will it experience?

9

  • Answer: For Cu

rearranging Equation 19.3b

Chapter 19 -

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Thermal Conductivity

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The ability of a material to transport heat.

temperature

gradient

thermal conductivity (J/m-K-s)

heat flux

(J/m2-s)

• Atomic perspective: Atomic vibrations and free electrons in � hotter regions transport energy to cooler regions.

T2

T2 > T1

T1

x1

x2

heat flux

Fourier’s Law

Chapter 19 -

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Thermal Conductivity: Comparison

11

increasing k

Polymers

Polypropylene

0.12

Polyethylene

0.46-0.50

Polystyrene

0.13

Teflon

0.25

vibration/rotation of chain molecules

Ceramics

Magnesia (MgO)

38

Alumina (Al2O3)

39

Soda-lime glass

1.7

Silica (cryst. SiO2)

1.4

atomic vibrations

Metals

Aluminum

247

Steel

52

Tungsten

178

Gold

315

atomic vibrations and motion of free electrons

k (W/m-K)

Energy Transfer�Mechanism

Material

Selected values from Table 19.1, Callister & Rethwisch 8e.

Chapter 19 -

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Thermal Stresses

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• Occur due to:

-- restrained thermal expansion/contraction

-- temperature gradients that lead to differential � dimensional changes

Thermal stress

= σ

Chapter 19 -

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Example Problem

13

-- A brass rod is stress-free at room temperature (20ºC).

-- It is heated up, but prevented from lengthening.

-- At what temperature does the stress reach -172 MPa?

T0

0

Solution:

Original conditions

Tf

Step 1: Assume unconstrained thermal expansion

0

Δ

Step 2: Compress specimen back to original length

0

σ

σ

Δ

Chapter 19 -

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Example Problem (cont.)

14

0

σ

σ

The thermal stress can be directly calculated as

Noting that εcompress = -εthermal and substituting gives

20 x 10-6/ºC

Answer: 106ºC

100 GPa

20ºC

Rearranging and solving for Tf gives

-172 MPa (since in compression)

Chapter 19 -

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Thermal Shock Resistance

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• Occurs due to: nonuniform heating/cooling

• Ex: Assume top thin layer is rapidly cooled from T1 to T2

Tension develops at surface

Critical temperature difference

for fracture (set σ = σf)

set equal

• Large TSR when is large

Temperature difference that

can be produced by cooling:

σ

rapid quench

resists contraction

tries to contract during cooling

T2

T1

Chapter 19 -

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Thermal Protection System

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• Application:

Space Shuttle Orbiter

Silica tiles (400-1260ºC):

-- large scale application

-- microstructure:

Fig. 19.2W, Callister 6e. (Fig. 19.2W adapted from L.J. Korb, C.A. Morant, R.M. Calland, and C.S. Thatcher, "The Shuttle Orbiter Thermal Protection System", Ceramic Bulletin, No. 11, Nov. 1981, p. 1189.)

Fig. 19.3W, Callister 5e. (Fig. 19.3W courtesy the National Aeronautics and Space Administration.)

Fig. 19.4W, Callister 5e. (Fig. 219.4W courtesy Lockheed Aerospace Ceramics

Systems, Sunnyvale, CA.)

reinf C-C

(1650ºC)

Re-entry T

Distribution

silica tiles

(400-1260ºC)

nylon felt, silicon rubber

coating (400ºC)

~90% porosity!

Si fibers

bonded to one

another during

heat treatment.

100 μm

Chapter-opening photograph, Chapter 23, Callister 5e (courtesy of the National Aeronautics and Space Administration.)

Chapter 19 -

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THERMAL DIFFUSIVITY

It measures the ability of a material to conduct thermal energy relative to its ability to store thermal energy.It has the SI unit of m²/s. Thermal diffusivity is usually denoted by α

The formula is:

α = k/(c x rho )

where

k is thermal conductivity (W/(m·K))

rho is density (kg/m³)

c is specific heat capacity (J/(kg·K))

Chapter 19 -

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Summary

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The thermal properties of materials include:

Heat capacity:

-- energy required to increase a mole of material by a unit T

-- energy is stored as atomic vibrations

Coefficient of thermal expansion:

-- the size of a material changes with a change in temperature

-- polymers have the largest values

Thermal conductivity:

-- the ability of a material to transport heat

-- metals have the largest values

Thermal shock resistance:

-- the ability of a material to be rapidly cooled and not fracture

-- is proportional to

Chapter 19 -

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ANNOUNCEMENTS

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Core Problems:

Self-help Problems:

Reading:

Chapter 19 -