problem and solution thermo 2, Summaries of Thermodynamics

solution Problem changing volume at constant pressure

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College of Engineering
Spring Session- 2016 THERMODYNAMICS II - ME 272
Dr. Saeed J. Almalowi, [email protected]
ME 272-College of Engineering-Taibah University
PROBLEM 2.1 STATEMENT
A piston-cylinder device contains 0.05 kg of steam at 1 MPa and 300oC. Steam now expands to a
final state of 200 kPa and 150oC, doing work. Heat losses from the system to the surrounding are
estimated to be 2 kJ during this process. Assuming the surrounding to be To = 25oC and Po =100
kPa,
Determine
a. The exergy of the steam at the initial and the final state,
b. The exergy change of the steam,
c. The useful work,
d. The exergy destroyed, and
e. The second law efficiency?
Fig.2.1 A Piston-Cylinder
Ans. [X1=35 kJ, X2=25.4 kJ, Wu=5.3 kJ, Xdestroyed=4.3 kJ, and ฮทII =55.2 %]
Solution:
X1= m(u1โˆ’uo)+mPo(ฮฝ1โˆ’ฮฝo)โˆ’mTo(s1โˆ’so)+1
2mV1
2+mgz1
X2= m(u2โˆ’uo)+ mPo(ฮฝout โˆ’ฮฝo)โˆ’mTo(s2โˆ’so)+1
2mV2
2+mgz2
State
Description of state
Internal energy
kJ/kg
Entropy
kJ/kg.K
Specific Volume
m3/kg
State (1) P1= 1000 kPa
T1=300oC
T1>Tsat. @ P1=1000 kPa
Superheated steam
u1=2794
s1=7.122
v1=0.2579
State(2) P2 =200 kPa,
T2=150oC
T2>Tsat. @ P2=200 kPa
Superheated steam
u2=2577
s2=7.279
v2=0.9597
Surrounding State:
Dead state* To=25oC,
P0=100 kPa
Compressed Liquid
uo=104.7
so= 0.3669
vo=0.001003
pf3
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Spring Session- 2016 THERMODYNAMICS II - ME 272 Dr. Saeed J. Almalowi, [email protected] PROBLEM 2.1 STATEMENT

A piston-cylinder device contains 0.05 kg of steam at 1 MPa and 300oC. Steam now expands to a final state of 200 kPa and 150oC, doing work. Heat losses from the system to the surrounding are estimated to be 2 kJ during this process. Assuming the surrounding to be To = 25oC and Po = kPa,

Determine

a. The exergy of the steam at the initial and the final state, b. The exergy change of the steam, c. The useful work, d. The exergy destroyed, and e. The second law efficiency?

Fig.2.1 A Piston-Cylinder

Ans. [X1=35 kJ, X 2 =25.4 kJ, Wu=5.3 kJ, Xdestroyed=4.3 kJ, and ฮทII = 55.2 %]

Solution:

X 1 = m(u 1 โˆ’ uo) + mPo(ฮฝ 1 โˆ’ ฮฝo) โˆ’ mTo(s 1 โˆ’ so) +

2 mV^1

(^2) + mgz 1

X 2 = m(u 2 โˆ’ uo) + mPo(ฮฝout โˆ’ ฮฝo) โˆ’ mTo(s 2 โˆ’ so) +

2 mV^2

(^2) + mgz 2

State Description of state Internal energy kJ/kg

Entropy kJ/kg.K

Specific Volume m^3 /kg State (1) P 1 = 1000 kPa T 1 =300oC

T 1 >Tsat. @ P1=1000 kPa Superheated steam

u 1 =2794 s 1 =7.122 v 1 =0.

State(2) P 2 =200 kPa, T 2 =150oC

T 2 >Tsat. @ P 2 =200 kPa Superheated steam

u 2 =2577 s 2 =7.279 v 2 =0.

Surrounding State: Dead state* To=25oC, P 0 =100 kPa

Compressed Liquid uo=104.7 so= 0.3669 v o=0.

Spring Session- 2016 THERMODYNAMICS II - ME 272 Dr. Saeed J. Almalowi, [email protected] Dead state is the state has an equilibrium with its surrounding (environment).

Xheat โˆ’ Xwork โˆ’ Xdestroyed = โˆ†Xsys = X 2 โˆ’ X 1

a. X 1 = 0.05 ร— [(2794 โˆ’ 104.7) + 100 ร— (0.2579 โˆ’ 0.001003) โˆ’ 298 ร— (7.122 โˆ’ 0.3669)] = 35.0kJ

b. X 2 = 0.05 ร— [(2577 โˆ’ 104.7) + 100 ร— (0.9597 โˆ’ 0.001003) โˆ’ 298 ร— (7.279 โˆ’ 0.3669)] = 25.4kJ

๐‘. โˆ†๐‘‹ = ๐‘‹ 2 โˆ’ ๐‘‹ 1 = 25.4 โˆ’ 35.0 = โˆ’9.58 ๐‘˜๐ฝ

Wu = Wsys โˆ’ Wsurr, Wsurr = mPo(v 2 โˆ’ v 1 ) = 0.05 ร— 100 ร— (0.9597 โˆ’ 0.2579) = 3.509 kJ

Wsys = Q + m(u 1 โˆ’ u 2 ) = โˆ’2 + 0.05 ร— (2794 โˆ’ 2577) = 8.85 kJ

Wu = 8.85 โˆ’ 3.509 = 5.341 kJ

d. Xdestroyed = X 2 โˆ’ X 1 โˆ’ Wu = 9.58 โˆ’ 5.341 = 4.239 kJ

Xdestroyed = To [m(s 2 โˆ’ s 1 ) +

Q

To^ ] = 298 ร— [0.05 ร— (7.279 โˆ’ 7.122) +^

298 ] = 4.33 kJ

e. Wrev = Xdestroyed + Wu = X 1 โˆ’ X 2 = 9.58 kJ, Wrev > Wu, [Producing devic], ฮทII =

Wu Wrev =

PROBLEM 2.2 STATEMENT

Steam enters a turbine steadily at 3MPa and 450oC at rate of 8 kg/s and exits at 0.2 MPa and 150C. The steam is losing heat to the surrounding air at 100 kPa and 25oC at a rate of 300 kW, and the kinetic and potential energy changes are negligible. Determine

a. The actual power output, b. The maximum possible power, c. The second โ€“ law efficiency, d. The exergy destroyed, and e. The exergy of the steam at the inlet condition?

Solution:

๐‘‹ฬ‡in = mฬ‡(hin โˆ’ ho) โˆ’ mฬ‡To(sin โˆ’ so) +

2 mฬ‡Vin

(^2) + mฬ‡gzin, where Vo = 0, zo = 0