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Modern Engineering Thermodynamics

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128 CHAPTER 4: The First Law of <strong>Thermodynamics</strong> and Energy Transport Mechanisms<br />

spontaneously moving down a potential gradient (such as from high to a low temperature) and the reverse cannot<br />

spontaneously occur, no heat transfer process can be reversed in any way whatsoever.Therefore,allfinite<br />

heat transfer processes are irreversible.<br />

4.13 HEAT TRANSFER MODES<br />

Heat transfer is such a large and important mechanical engineering topic that most curricula have at least one<br />

required course in it. Heat transfer equations are always cast as heat transfer rate (i.e., _Q) equations. To determinetheamountofheatenergytransport<br />

that occurs as a system undergoes a process from one equilibrium<br />

statetoanotheryoumustintegrate _Q over the time interval of the process, or 1 Q 2 =<br />

Z 2<br />

1<br />

_Q dt. Normally, we<br />

choose processes in which _Q is constant in time so that the integral becomes simply 1 Q 2 = _Q ðt 2 − t 1 Þ = _QðΔtÞ,<br />

where Δt is the time required for the process to occur.<br />

Historically, the field has been divided into three heat transfer modes: conduction, convection, and radiation.<br />

These three modes are briefly described next.<br />

4.13.1 Conduction<br />

The basic equation of conduction heat transfer is Fourier’s law:<br />

<br />

_Q cond = −k t A dT <br />

dx<br />

(4.73)<br />

where _Q cond is the conduction heat transfer rate, k t is the thermal conductivity of the material, A is the crosssectional<br />

area normal to the heat transfer direction, and dT/dx is the temperature gradient in the direction of<br />

heat transfer. The algebraic sign of this equation is such that a positive _Q cond always corresponds to heat transfer<br />

in the positive x direction, and a negative _Q cond always corresponds to heat transfer in a negative x direction.<br />

Since this is not the same sign convention adopted earlier in this text, the sign of the values calculated from<br />

Fourier’s law may have to be altered to produce a positive when it enters a system and a negative when it leaves<br />

asystem.<br />

For steady conduction heat transfer through a plane wall (Figure 4.20), Fourier’s law can be integrated to give<br />

<br />

ð _Q cond Þ plane = − k t A T <br />

2 − T 1<br />

(4.74)<br />

x 2 − x 1<br />

and for steady conduction heat transfer through a hollow cylinder of length L, Fourier’s law can be integrated to give<br />

<br />

<br />

T<br />

ð _Q cond Þ cylinder<br />

= −2πLk inside − T outside<br />

t<br />

(4.75)<br />

lnðr inside /r outside<br />

Table 4.7 gives thermal conductivity values for various materials.<br />

Q<br />

T 1<br />

Q<br />

Q<br />

r i<br />

Q<br />

T 2<br />

T i<br />

r o<br />

x 1<br />

x 2<br />

T o<br />

x = 0<br />

(a) Plane wall<br />

(b) Cylindrical and spherical<br />

FIGURE 4.20<br />

Thermal conduction notation in plane, cylindrical, and spherical coordinates.

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