Environmental Engineering Reference
In-Depth Information
Second group losses.
As results from formula (2.4.48) the external exergy loss
δB
1
−
0
is equal to the escaping exergy of three unabsorbed emissions at tempera-
tures
T
1
=
T
S
,
T
2
and
T
3
reflected to the environment. By multiplying these emissions
respectively by the exergy/energy ratio the three losses can be expressed as follows:
B
1
−
1
=
Q
1
−
1
ψ
S
(2.4.54)
B
2
−
1
=
Q
2
−
1
ψ
2
(2.4.55)
B
3
−
1
=
Q
3
−
1
ψ
3
(2.4.56)
where
ψ
S
,
ψ
2
and
ψ
3
are calculated from formula (2.2.45) for
T
S
,
T
2
and
T
3
, respec-
tively, and
Q
1
−
1
,
Q
2
−
1
and
Q
3
−
1
are the sums of the unabsorbed portion of the
respective emissions of surfaces 1, 2 and 3. Thus, heat
Q
1
−
1
represents energy portions
from many reflections of emission
E
1
of temperature
T
S
, at the concave surface 2, and
arriving in surface 1:
Q
1
−
1
=
E
1
ϕ
1
−
2
ρ
2
ϕ
21
+
E
1
ϕ
12
ρ
2
ϕ
2
−
2
ρ
2
ϕ
2
−
1
+
E
1
ϕ
12
ρ
2
ϕ
2
−
2
ρ
2
ϕ
2
−
2
ρ
2
ϕ
2
−
1
+···
(2.4.57)
The portions in equation (2.4.57) can be expressed as the sum of the terms of the
infinite geometric progression with the common ratio
φ
2
−
2
·
ρ
2
, thus
1
Q
1
−
1
=
E
1
ϕ
1
−
2
ρ
2
ϕ
2
−
1
(2.4.58)
1
−
ϕ
2
−
2
ρ
2
φ
2
−
1
of emission
E
2
of surface 2 which
directly arrives at surface 1 and the portions in results of many reflections of emission
E
2
at surface 2, arriving at surface 1:
Heat
Q
2
−
1
(
T
2
) represents the portion
E
2
·
Q
2
−
1
=
E
2
ϕ
2
−
1
+
E
2
ϕ
2
−
2
ρ
2
ϕ
2
−
1
+
E
2
ϕ
2
−
2
ρ
2
ϕ
2
−
2
ρ
2
ϕ
2
−
1
+
...
(2.4.59)
and
1
Q
2
−
1
=
E
2
ϕ
2
−
1
(2.4.60)
1
−
ϕ
2
−
2
ρ
2
φ
3
−
1
of emission
E
3
of surface 3 which
arrives at surface 1 as the direct radiation, and the portions as a result of many
reflections of emission
E
3
at surface 2:
Heat
Q
3
−
1
(
T
3
) represents the portion
E
3
·
Q
3
−
1
=
E
3
ϕ
3
−
1
+
E
3
ϕ
3
−
1
ρ
2
ϕ
2
−
1
+
E
3
ϕ
3
−
1
ρ
2
ϕ
2
−
2
ρ
2
ϕ
2
−
1
+
E
3
ϕ
3
−
1
ρ
2
ϕ
2
−
2
ρ
2
ϕ
2
−
2
ρ
2
ϕ
2
−
1
+
...
(2.4.61)
and
E
3
ϕ
3
−
1
1
Q
3
−
1
=
+
ϕ
3
−
2
ρ
2
ϕ
2
−
1
(2.4.62)
−
1
ϕ
2
−
2
ρ
2
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