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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