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A series of solved problems related to thermodynamics, focusing on the carnot cycle and its applications in heat engines and heat pumps. It explores concepts like efficiency, coefficient of performance, and the relationship between temperature, heat transfer, and work. The problems provide practical examples and demonstrate the application of thermodynamic principles in real-world scenarios.
Typology: Exercises
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C.V. House. For constant 20°C the heat pump must provide
C.V. Heat pump. Definition of the coefficient of performance and the fact that
the maximum is for a Carnot heat pump.
Substitute into the first equation to get
0.6 (TH - TL ) = [ 0.5 * TH / (TH - TL ) ] 1 =>
(TH - TL )^2 = (0.5 / 0.6) TH * 1 = 0.5 / 0.6 *293.15 = 244.
TH - TL = 15.63 => TL = 20 - 15.63 = 4.4 °C
QH = Qleak = 0.6( TH − TL (^) )= W
= QH / W = QH / (^) ( QH − QL )= 0.5 carnot = 0.5*T / TH ( (^) H −TL)
Question: Consider a Carnot cycle heat engine
operating in outer space. Heat can be rejected from
this engine only by thermal radiation, which is
proportional to the radiator area and the fourth power
of absolute temperature, Q rad
~ KAT
4
. Show that for
given engine work output and given T H
, the radiator
area will be minimum when the ratio T L
/T H
= 3/4.
4 4 4 1
net H L L L H L L
H L H H L H H
− ^ − = (^) = (^) − (^) = (^) ^ −
^
3 4
4
net L L
H H H
A const KT T T
3 4 4
net
H
A x x const
KT
L
H
where x T
x x
−
( )
( ) (^ )
( )
( )
( )
( )
2 3 2 3 2 3
3 4 2 3 4 3 4 3 4
dA x^ x^ x^ x^ x^ x A dx (^) x x x x x x x x
( )
( )
2 3 4
dA x Ax dx (^) x x
x =
3
4
L
H
T
T
=
q m
= qH = 250 kJ /kg TH = 600 K TL = 300 K P 3 = 75 kPa
Cv =0.717 kJ /kgK R =0.287 kJ /kgK
3 3 3 3
v m kg P
Solution:
From the first law of thermodynamics for a closed system
q = du +w
Between the states 2 and 3 we have an adiabatic process
from the equation of state for an ideal gas
P =RT /v
dv w RT v
v 0
dv q C dT RT v
dT dv C R T v
2
1
H H^ ln
v q RT v
2
1
ln (^) H / (^) H 250 / 0.287 *600 1.
v q RT v
v 1 = v 2 / exp(1.4518) = 0.2034 / exp(1.4518) =0.
in Carnot Cycle
3 4
2 1
v (^) v
v v
= v 4 = v 1 * v 3 / v 2 = 0.04763*1.148 / 0.2034 =0.
P 1 = RT 1 / v 1 = 0.287 *600 / 0.04763 = 3615 kPa
P 2 = RT 2 / v 2 = 0.287 *600 / 0.2034 =846.6kPa
P 4 = RT 4 / v 4 = 0.287 *300 / 0.2688 =846.6kPa