Microsoft Word - Cengel and Boles TOC _2-03-05_.doc

(ff) #1
external to the system. A second-law analysis of these cycles reveals where
the largest irreversibilities occur and where to start improvements.
Relations for exergyand exergy destructionfor both closed and steady-
flow systems are developed in Chap. 8. The exergy destruction for a closed
system can be expressed as

(9–30)

where Tb,inand Tb,outare the temperatures of the system boundary where
heat is transferred into and out of the system, respectively. A similar relation
for steady-flow systems can be expressed, in rate form, as

(9–31)

or, on a unit–mass basis for a one-inlet, one-exit steady-flow device, as

(9–32)

where subscripts iand edenote the inlet and exit states, respectively.
The exergy destruction of a cycleis the sum of the exergy destructions of
the processes that compose that cycle. The exergy destruction of a cycle can
also be determined without tracing the individual processes by considering
the entire cycle as a single process and using one of the relations above.
Entropy is a property, and its value depends on the state only. For a cycle,
reversible or actual, the initial and the final states are identical; thus sesi.
Therefore, the exergy destruction of a cycle depends on the magnitude of
the heat transfer with the high- and low-temperature reservoirs involved and
on their temperatures. It can be expressed on a unit–mass basis as

(9–33)

For a cycle that involves heat transfer only with a source at THand a sink at
TL, the exergy destruction becomes

(9–34)

The exergies of a closed system fand a fluid stream cat any state can be
determined from

(9–35)

and

(9–36)

where subscript “0” denotes the state of the surroundings.

c 1 hh 02 T 01 ss 02 

V^2
2

gz¬¬ 1 kJ>kg 2


f 1 uu 02 T 01 ss 02 P 01 vv 02 

V^2
2

gz¬¬ 1 kJ>kg 2


xdestT 0 a

qout
TL



qin
TH

b¬¬ 1 kJ>kg 2


xdestT 0 aa

qout
Tb,out

a

qin
Tb,in

b¬¬ 1 kJ>kg 2


XdestT 0 sgenT 0 asesi

qin
Tb,in



qout
Tb,out

b¬¬ 1 kJ>kg 2


X

#
destT 0 S

#
genT 01 S

#
outS

#
in^2 T 0 aa
out

m#sa
in

m#s

Q

#
in
Tb,in



Q

#
out
Tb,out

b¬¬ 1 kW 2


T 0 c1S 2 S 12 sys

Qin
Tb,in



Qout
Tb,out

d¬¬ 1 kJ 2


XdestT 0 SgenT 01 ¢SsysSinSout 2

528 | Thermodynamics

Free download pdf