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Materials Engineering Science<br />

MESc. 5025<br />

Instructor: Herve Marand<br />

Chapter 6.<br />

<strong>Heat</strong> <strong>Transfer</strong>


• There are three modes of heat transfer:<br />

– Conduction<br />

– Convection<br />

– Radiation<br />

<strong>Heat</strong> <strong>Transfer</strong><br />

• In its simplest form, the rate of heat transfer is equal to the product<br />

of a driving force and a thermal conductance.<br />

• Thermal conductances vary for each mode of heat transfer<br />

• Conduction:<br />

Conduction is accomplished via two mechanisms:<br />

– Molecular Interactions:<br />

Molecules in high energy levels (high T) impart energy to<br />

adjacent molecules at lower energy levels.<br />

This type of heat transfer necessitates the presence of molecules<br />

of solid, liquid or gas and the existence of T gradient.


– <strong>Heat</strong> <strong>Transfer</strong> via Free Electrons:<br />

This second conduction heat transfer mechanism is observed<br />

primarily in metallic solids. The concentration of free electrons<br />

varies considerably for metallic alloys and is very low for nonmetals.<br />

The previous statement implies that the ability of solids<br />

to conduct heat via this mechanism varies directly with the free<br />

electron concentration (pure metals conduct heat the best). This<br />

conduction mechanism also relies on the existence of a<br />

temperature gradient.<br />

• Theoretical Treatment of <strong>Heat</strong> <strong>Transfer</strong> by Conduction<br />

A quantitative expression relating the rate of heat transfer, the<br />

temperature gradient and the nature of the conducting medium<br />

is attributed to Fourier (1822)<br />

q x dT<br />

= − k temperature<br />

A dx gradient along x<br />

<strong>Heat</strong> flux= heat thermal<br />

flow rate per unit conductivity<br />

area in direction x of material<br />

A: area normal to<br />

heat flow


• Units:<br />

quantity S.I. unit non-S.I. unit<br />

q Watt or J.s-1 Btu/hr<br />

A m 2 ft 2<br />

dT/dx K.m -1 °F.ft -1<br />

k W. K -1 .m -1 Btu.hr -1 .ft -1 .°F -1<br />

• Unit Conversion Factor:<br />

1 Watt = 1 J.s -1 = 3.414 Btu.hr -1<br />

1 Btu = 1054 Joules<br />

• For isotropic materials and steady state conditions, the<br />

Fourier equation can be generalized as:<br />

q<br />

A<br />

= − k∇ T<br />

k = k e + k i<br />

- sign accounts for heat<br />

transfer from hot to cold<br />

molecular interactions<br />

free electrons<br />

⎛<br />

⎜<br />

⎜<br />

∇ = ⎜<br />

⎜<br />

⎜<br />

⎝<br />

⎞<br />

⎟<br />

x<br />

⎟<br />

⎟<br />

y⎟<br />

⎟<br />

z ⎠<br />

is the<br />

gradient<br />

vector


• In most solids, the principal mode of thermal energy<br />

assimilation is by increase in vibrational energy of the<br />

atoms. Atoms in solids are constantly vibrating at very<br />

high frequencies and with relatively small amplitudes. The<br />

atomicvibrations of adjacent atoms are coupled through the<br />

atomic bonding. These vibrations are coordinated in such<br />

a way that traveling lattice waves are produced. (These<br />

may be thought of as elastic waves or simply sound waves<br />

(short wavelength and high frequency), which propagate<br />

through a crystal at the velocity of sound. The vibrational<br />

thermal energy for an ordered material consist of a series<br />

of elastic waves (with a distribution of frequencies). Only<br />

certain energies are allowed (quantization of the<br />

vibrational energy). A single quantum of vibrational<br />

energy is called a phonon. Note that phonon waves can<br />

scatter free electrons during electronic conduction, thus<br />

they control the temperature dependence of electronic<br />

conduction


• In metals, the free electron mechanism of heat transport is<br />

much more efficient than the phonon mechanism, because<br />

phonons are more easily scattered than free electrons and<br />

electrons ahave higher velocities.<br />

• Thermal energy associated with phonons is transported in<br />

the direction of their motion (net movement of phonons<br />

from high to low temperature regions)<br />

• Free electrons in hot regions have higher kinetic energy<br />

tham these in cold regions. When they migrate to colder<br />

regions, their kinetic energy is transferred to atoms as<br />

vibrational energy (collision of electrons with phonons).<br />

• Thermal conductivities of common pure metals or alloys<br />

range from 20 to ca. 400 W.m -1 .K -1 . When impurities are<br />

are present in a metal or alloying is used, the impurity<br />

atoms act as scattering centers for the electrons, decreasing<br />

the efficiency of electron motion (i.e. k e)


• In ceramics k e


• Polymers:<br />

Thermal conductivity for most polymers is of the order of<br />

0.3 W.m -1 .K -1 . Energy transfer is accomplished by the<br />

vibrations and rotations of chain backbone and side chain<br />

bonds.<br />

The magnitude of the thermal conductivity increases with<br />

the degree of crystallinity.<br />

Polymers are used as low temperature thermal insulators<br />

(porous polymershave enhanced insulative properties).<br />

• Gases:<br />

Thermal conductivity is low but increases with<br />

temperature due to increased Brownian motion resulting in<br />

a higher frequency of contact and increase in molecular<br />

exchange rates. For dilute gases (low pressure, P


Kinetic Theory of Gases:<br />

assumes ideal gas behavior.<br />

Chapman-Erskog Theory:<br />

accounts for pairwise interactions<br />

based on the Lennard-Jones potential.<br />

T: absolute temperature<br />

m: molecular mass<br />

M: molar mass<br />

d: molecular diameter<br />

k b: Boltzmann constant<br />

Ω k, σ: related to Lennard-Jones potential<br />

k =<br />

k =<br />

1<br />

3 / 2 d 2<br />

1.9891 ⋅10 −4<br />

Ω k 2<br />

k<br />

3<br />

T<br />

b<br />

m<br />

T<br />

M<br />

see viscosity<br />

section for<br />

discussion on Ω k<br />

Chapman-Erskog theory accounts better than the Kinetic<br />

Theory for the temperature dependence of interactions.


Anisotropicity of the Thermal Conductivity<br />

• In general, in crystalline materials, the simplified Fourier<br />

equation is not rigorously valid asthe thermal conductivity<br />

may be different in different directions in the crystal.<br />

• The scalar k must be replaced by the tensor k (3x3). The<br />

Tensor is symmetrical (Onsager’s principle)<br />

˜<br />

k =<br />

˜<br />

k =<br />

⎛<br />

⎜<br />

⎜<br />

⎝<br />

k11 k21 k31<br />

k12 k22 k32<br />

k13 k23 k33<br />

⎛ k1 0 0 ⎞<br />

⎜ ⎟<br />

0 k2 0<br />

⎜<br />

⎟<br />

⎝ 0 0 k3⎠<br />

⎞<br />

⎟<br />

⎟<br />

⎠<br />

where: -k ij = rate of heat transfer per<br />

unit cross section parallel to the axis<br />

defined by “i” from a temperature<br />

gradient along the “j”-axis<br />

if the crystal axes are matching the<br />

laboratory axes<br />

Note: that q and ∇ T<br />

will generally not be parallel unless the crystal<br />

is cubic (i.e. k1=k2=k3)


Example Calculation #1<br />

• Steam is transported through a 11/2 “ mild steel pipe. The inside<br />

and outside pipe wall temperatures are 205°F and 195°F,<br />

respectively. OD = 1.9” ; ID = 1.5”; k = 24.8 Btu.hr -1 .ft -1 .°F -1<br />

– 1) Find the heat loss for 10 feet of pipe<br />

– 2) FInd the heat flux based upon inside and outside surface<br />

areas.<br />

• <strong>Heat</strong> is transferred radially. The applicable scalar form of the<br />

Fourier rate equation is:<br />

qr = −kA<br />

For the steady state case, qr is constant<br />

dT ⎫<br />

dr ⎬<br />

A = 2 rL<br />

⎪<br />

⇒ qr = −k( 2 rL)<br />

⎪ ⎭<br />

dT<br />

dr<br />

rodr<br />

To<br />

qr ∫ = −2 kL ∫ dT ⇒ qr ln<br />

r<br />

ro ⎛ ⎞<br />

⎜ ⎟ = −2 kL( To − Ti )<br />

⎝ ⎠<br />

r i<br />

T i<br />

r i


( )<br />

qr = 2 kL Ti − To ln r ⎛ o ⎞<br />

⎜ ⎟<br />

⎝ ⎠<br />

q r<br />

A i<br />

qr<br />

A o<br />

=<br />

=<br />

r i<br />

65, 000<br />

⋅ 1.5 ⎛ ⎞<br />

⎜ ⎟ ⋅10<br />

⎝ 12 ⎠<br />

65, 000<br />

⋅ 1.9 ⎛ ⎞<br />

⎜ ⎟ ⋅10<br />

⎝ 12 ⎠<br />

= 2 ⋅ 3.14 ⋅ 24.8 ⋅ 10 ⋅10<br />

ln 1.9 ⎛ ⎞<br />

⎜ ⎟<br />

⎝ 1.5 ⎠<br />

The heat flux is q/A (rate of heat loss per unit area)<br />

= 16, 700 Btu/hr.ft 2<br />

= 13,150 Btu/hr.ft 2<br />

= 65, 000 Btu/hr


Example Calculation #2<br />

• For steady state heat conduction through a wall with<br />

dimensions and surface temperatures shown below, express:<br />

T 0<br />

x=0<br />

– 1) the heat flow rate for a constant thermal conductivity k.<br />

– 2) the heat flow rate, when the thermal conductivity of the<br />

wall material varies linearly with temperature k = k 0(1+βT).<br />

x<br />

x=L<br />

T L<br />

• 1)<br />

• 2)<br />

q x dx = −kAdT<br />

L<br />

q x ∫ dx = −kA ∫ dT<br />

0<br />

T L<br />

T 0<br />

( )<br />

q x L = −kA T L − T 0<br />

q x = kA<br />

L T ( L − T0) q x = −k0 ( 1 + T)A<br />

dT<br />

dx<br />

q x = k0 A<br />

L 1 + 2 T0<br />

⎡<br />

⎢ + TL<br />

⎣<br />

( )<br />

⎤<br />

⎥ ⎦<br />

TL − T0<br />

[ ]


Convection<br />

• Convection <strong>Heat</strong> <strong>Transfer</strong>: involves the exchange of heat<br />

between a fluid and a surface or an interface.<br />

• Two kinds of convection exist:<br />

– Forced convection in which fluid motion past a surface<br />

is caused by an external agency<br />

– Free convection in which density changes in the fluid<br />

which result from energy exchange lead to a natural<br />

(i.e.unassisted) fluid motion.<br />

• Newton (1701) first expressed the basic rate equation for<br />

convective heat transfer (Newton’s law of cooling).<br />

rate of convective<br />

heat transfer (Btu/hr)<br />

q = hA( Tsurf − T ) fluid temperature<br />

driving force<br />

convective heat<br />

transfer coefficient<br />

(Btu.hr -1 .ft -2 .°F -1 )<br />

area normal to the<br />

direction of heat flow


• Regardless of the flow phenomenon involved, it is known that<br />

directly adjacent to the interface, the energy transfer mechanism is<br />

that of conduction. The surface conductive layers of fluid control<br />

the heat transfer rate and determine the value of “h”, which is<br />

justifiably often called the “film coefficient”. The only difficulty in<br />

describing convective phenomena lies in the evaluation of “h”.<br />

• If we write : q = KΔT where K is the thermal conductance.<br />

K convection = hA<br />

K conduction hollow cylinder =<br />

K conduction plane wall = kA<br />

L<br />

2 kL<br />

ln r ⎫<br />

⎪<br />

⎪<br />

⎪<br />

⎪<br />

⎬ Btu / hr.°F<br />

⎛ o ⎞ ⎪<br />

⎜ ⎟<br />

⎝ ri ⎠ ⎪<br />

⎪<br />

⎪<br />

⎭ ⎪


• Range of values for “h” allows the convective mechanism<br />

to be understood<br />

– mechanism h (Btu.hr -1 .ft -2 .°F -1 )<br />

condensing water vapor 1,000 to 20,000<br />

boiling water 500 to 5,000<br />

forced convection (H 2O) 50 to 3,000<br />

forced convection (air) 5 to 100<br />

free convection 1 to 10


Example Calculations #3<br />

Given the steel pipe with conditions described in Example #1, with<br />

10°F air surrounding the pipe and 210°F steam flowing on the<br />

inside, evaluate the convective heat transfer coefficients on each of<br />

the pipe surfaces and indicate the operating mechanisms.<br />

1) q r/A i = 16,700 Btu.hr -1 .ft -2<br />

T steam - T surface = 210 -205°F<br />

h = 16,700 / 5 = 3,340 Btu.hr -1 .ft -2 .°F -1<br />

Steam is condensing on the inside of the pipe<br />

2) q r/A o = 13,150 Btu.hr -1 .ft -2<br />

T surface - T air = 195 -10°F<br />

h = 13,150 / 185 = 71 Btu.hr -1 .ft -2 .°F -1<br />

Air must be in forced convection


Thermal Radiation<br />

• <strong>Heat</strong> transfer by radiation requires no medium for<br />

propagation. Radiant exchange between surfaces is in fact<br />

maximum when no material occupies the intervening<br />

space. This type of energy transfer by radiation is an<br />

electromagnetic phenomenon and the exact nature still not<br />

completely understood.<br />

• A perfectly emitting or absorbing body is called a black<br />

body. The rate at which it emits radiant energy is given by<br />

the Stephan-Boltzmann law of Thermal radiation:<br />

radiant emission in Btu/hr<br />

q<br />

A<br />

= T 4<br />

Absolute<br />

Temperature<br />

area of emitting surface in ft 2 Stephan-Boltzmann constant

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