A rigid
tank contains ammonia at -20oC with a quality of 0.50 kg vap/kg. Superheated ammonia vapor at 800
kPa and 80oC slowly and steadily enters the tank from a supply line through a pipe with a valve. |
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When the pressure in the tank reaches 600 kPa, the valve
is closed. At this
point, the last drop of liquid ammonia
in the tank vaporizes
and the tank contains only saturated ammonia vapor. |
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The total volume
of the tank is 350 L.
Determine...
a.) The final temperature of the ammonia in the tank
b.) The mass of ammonia that has entered the tank
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c.) The heat transfer between the tank and the surroundings that has taken place
during this process |
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Read : |
Part
(a) is straightforward because the vapor in the system is saturated at 800 kPa. We can then determine the initial and final mass of ammonia in the tank. A mass balance between the initial and final states of the system (the tank)
tells us that the mass added to the tank is just the final mass minus
the initial mass. This process is a transient process because the mass of ammonia inside the system (the tank)
changes with time. We will need to use the integral form of the transient 1st Law Equation to
answer part (c). |
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Given: |
V |
350 |
L |
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Pin |
800 |
kPa |
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0.35 |
m3 |
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Tin |
40 |
oC |
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T1 |
-20 |
oC |
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P2 |
600 |
kPa |
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x1 |
0.50 |
kg vap/kg total |
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x2 |
1.00 |
kg vap/kg total |
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Find: |
T2 |
??? |
oC |
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Q |
??? |
kJ |
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min |
??? |
kg |
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Diagram: |
The diagram in the
problem statement is adequate. |
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Assumptions: |
1 - |
Although this is a
transient process, it can be analyzed as a uniform flow problem because the
properties of the R-134a entering the tank are constant. |
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2 - |
Kinetic and potential
energies are negligible. |
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3 - |
No shaft work crosses
the boundary of the system, which consists of the content of the tank. |
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Equations
/ Data / Solve: |
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Part a.) |
The vapor inside the tank in the final state is saturated. Therefore, it is at the saturation temperature of ammonia at a pressure of 600 kPa. We can obtain this temperature from the NIST Webbook. |
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T2 |
9.285 |
oC |
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Part b.) |
The integral form of
the transient mass balance on the tank is : |
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Eqn 1 |
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We can determine the
intial and final mass of R-134a in the system using : |
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Eqn 2 |
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Our next step is to
determine the intial and final specific
volume of the ammonia. |
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In the initial state : |
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At -20oC : |
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P1 |
190.08 |
kPa |
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Eqn 3 |
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Vsat liq |
0.0015035 |
m3/kg |
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Vsat vap |
0.62373 |
m3/kg |
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V1 |
0.31262 |
m3/kg |
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The final state is simpler because the ammonia in the tank is a saturated vapor. |
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At 600
kPa : |
Vsat vap |
0.21035 |
m3/kg |
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V2 |
0.21035 |
m3/kg |
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Now, we can use Eqn 2 to to determine the initial and final mass of ammonia in the tank. |
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m1 |
1.12 |
kg |
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m2 |
1.66 |
kg |
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Plug these values back
into Eqn 1 to determine the mass of ammonia that was added to the tank during this process. |
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min |
0.544 |
kg |
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part c.) |
The integral form of the transient energy balance equation
for a single-input, single-output system in which kinetic and potential energies are negligible is : |
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Eqn 4 |
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In our process, no shaft
work occurs and there is no mass leaving
the system, so Eqn 4 can be simplified and solved for Q : |
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Eqn 5 |
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We can determine U2 and U1 much as we determined V2 and V1 in part (b). |
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The NIST
Webbook, using the default reference state, tells that in the initial state : |
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At -20oC : |
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Usat liq |
89.095 |
kJ/kg |
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Usat vap |
1299.9 |
kJ/kg |
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Eqn 6 |
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U1 |
694.52 |
kJ/kg |
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The final state is simpler because the ammonia in the tank is a saturated vapor. |
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At 600
kPa : |
Usat vap |
1326.1 |
kJ/kg |
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U2 |
1326.1 |
kJ/kg |
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Next, we need to
determine Hin. First, we need to
determine the state of
the system. |
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Tsat(Pin) |
17.848 |
oC |
Tin > Tsat, therefore we must
consult the Superheated Ammonia Tables. |
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From the NIST Webbook, we can obtain : |
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Hin |
1521.3 |
kJ/kg |
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Now, we can plug
values back into Eqn 5 to
evaluate Q : |
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Q |
600.83 |
kJ |
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Verify: |
None of the assumptions
made in this problem solution can be verified. |
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Answers : |
T2 |
9.3 |
oC |
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Q |
601 |
kJ |
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min |
0.544 |
kg |
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