Download Solution Manual for Thermodynamics for · PDF fileAn object feels cool if its...
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Download Solution Manual for Thermodynamics
for Engineers 1st Edition by Kroos and Potter
Link download full: https://digitalcontentmarket.org/download/solution-
manual-for-thermodynamics-for-engineers-1st-edition-by-kroos-and-
potter/
Chapter 1
Solutions
1.1 (B) The utilization of energy is not of concern in our study. If you use
energy to power your car, or your car seat is your own decision. 1.2 (C) All properties are assumed to be uniformly distributed throughout the
volume. 1.3 (D)
1.4 (B) When the working fluid crosses the boundary, it is a control
volume, as during intake and exhaust. The ice plus the water forms
the system of (C). The entire atmosphere forms the system of (D).
1.5 (C) An extensive property doubles if the mass doubles. Temperature is the
same for the entire room or half the room.
1.6 (D) A process may be very fast, humanly speaking, but molecules move
very rapidly so an engine operating at 4000 rpm is not
thermodynamically fast. All sudden expansion processes and
combustion processes are non-equilibrium processes. Air leaving a
balloon is thermodynamically slow.
1.7 (B) If force, length, and time had been selected as the three primary
dimensions, the newton would have been selected and mass expressed in
terms of the other three. But, in Thermo-dynamics, the newton is
expressed as kg·m/s2.
1.8 (D) W = J/s = N ⋅ m/s = (kg ⋅ m/s 2 ) ⋅ m/s = kg ⋅ m
2 /s
3
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1.9 (A) 34 000 000 000 N = 34 × 109 N = 34 GN (or 34 000 MN.)
1.10 (A) ρ = m = 10 kg = 1250 kg/m3
V 8000×10−6m
3
v = V = 1
= 1 = 0.0008 m3 /kg
m ρ 1250 kg/m3
SG = ρHg 1250 kg/m3 = 1.25
=
ρ 3
water 1000 kg/m
1.11 (D) We must know if the surface is horizontal, vertical, on an angle? The
surface cannot be assumed to be horizontal just because it is drawn that
way on the paper. (Sometimes problems
aren’t fair. This is an example of such a problem.)
1.12 (C) P = Fn = 36cos30° kN = 1559
kN/m2 or 1560 kPa
A 200 cm2 ×10
−4 m
2/cm
2
1.13 (A) Use Eq. 1.13 to convert to pascals:
p = ρ gH = (13.6 × 1000 kg/m3 ) × 9.81 m/s
2 × 0.42 m
= 56 030 kg/m ⋅ s2 or 56.03×10
3
N/m2
or
56.03 kPa
1.14 (C) ∑ F = 0 PA + Kx = mg
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P × π × 0.052 + 400× 0.2 = 40× 9.81. ∴ P = 39 780 N/m
2 or 39.8 kPa
gage
The atmospheric pressure acts down on the top and up on the bottom of
the cylinder and hence cancels out.
1.15 (B) We do not sense the actual temperature but the temperature gradient
between our skin and the water. As our skin heats up, the water feels
cooler so we increase the water temperature until it feels warm again.
This is done until out skin temperature ceases to change. An object
feels cool if its temperature is less than out skin temperature. If that’s
the case, a temperature difference occurs between our skin and the
object over a very small distance, creating a temperature gradient
(Tskin − Tobject ) / x .
1.16 (B) The energy equation states that at the position of maximum
compression, the kinetic energy of the vehicle will be zero and the
potential energy of the spring will be maximum, that is,
12 m V 2 = 12 Kx2 . (The velocity must be expressed in m/s.)
1 80×1000 2 1 K = 98.8×106 N/m or 100
× 2000 × = × K × 0.12. MN/m 2
3600 2
If the mass is in kg, the velocity in m/s, and x in meters, K will be
in N/m. But, check the units to make sure. Get used to always using N, kg, m, and s and the units will work out.
You don’t have to always check all those units. It takes time and on a
multiple-choice test, there are usually problems left over when time runs
out.
1.20 True. Thermodynamics presents how energy is transferred, stored, and
transformed from one form to another. If you use it to dry your hair,
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power your car, or store it in a battery, we don’t really care. Just use it
any way that allows you to enjoy life!
1.21 Energy derived from coal is not sustainable since coal will eventually
not be available, even though that may take 500 years. If an energy
source is not available indefinitely, it is not sustainable.
1.22 Consult the Internet.
1.23 A large number of engineers were required when the industrial
revolution occurred.
1.24 Trains were traveling the rails in the mid-1800s so mechanical engineers
were needed, not to drive the trains, but to design them! Coal was mined
with a pick and shovel until the late 1800’s. Power plants and
automobiles also came near the end of the 1800’s.
1.25 It’s CO2 and it keeps things very cold. Check it out on the Internet.
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1.26 i) A system, ii) a control volume, iii) a system, iv) a system. No fluid
crosses the boundary of a system. Fluid crosses the boundary of a control
volume.
1.27
1.28 The number of
molecules in a cubic meter
of air at sea level is (3 ×
1016
) × 10 9 = 3 ×10
25 .
V
π
3 r 3 =3×10102512
molecules/mmolecules 3 . ∴ r = 0.00002 m or 0.02 mm
1.29 Catsup is not a fluid. It is a pseudo plastic or a shear-thinning liquid,
whatever that is! A fluid always moves if acted upon by a shear. A
plastic can resist a shear but then moves when the shear is sufficiently
large. Catsup is like that: first it won’t move, then it suddenly comes.
1.30 From Wikipedia, 1 stone = 6.35 kg (= 14 lbm). ∴6.3 stones = 6.3× 6.35 = 40 kg
1.31 The units using Newton’s 2nd
law are simpler:
lbf = slug × sft2 is simpler than lbf = lbm ×
32.232.2 ft-lbm/lbf ft/s2 -s2
The system and
c.v. are identical
The system
is the air
inside plus
that which
has exited.
The c.v.
extends to
the exit of
the balloon
nozzle.
Before
Control surface
After
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The conversion between mass and weight does not require the use of a
gravitational constant when using the slug as the mass unit in the English
system.
1.32 Volume is extensive since it increases when the mass is increased, other
properties remaining constant.
0.000998 − 0.001008
1.33 % change = × 100 = − 0.992% or
−1 % 0.001008
1.34 ρ ice = = v 0.01747
1 1 = 57.2 lbm/ft3 . ρwater = 62.4 lbm/ft
3 . So, ice is lighter than water at
32ºF, so ice floats. If ice was heavier than water, it would freeze from the
bottom up. That would be rather disastrous. Fish as well as skaters
would have a problem. You can speculate as to the consequences.
1.35 SGHg = = 13.6
1000
kg m
W = γ V = 13 600 3 × 9.81 2 × 2 m3 =
266 800 N m s
W = 266 800 N × 0.2248 lbf = 59,980 lbf
N
1.36 a ) ρ = = 1 = 0.2
kg/m
1 3, m = ρV = 0.2× 2 = 0.4 kg, W = mg = 0.4× 9.8 =
3.92 N
v 5 b ) v = 1
= 1
= 0.5 m
3 /kg, m = ρV = 2× 2 = 4 kg,
W = mg = 4× 9.8 = 39.2 N ρ 2 c ) v = V =
2 = 0.002 m3 /kg, ρ = 1 = 500 kg/m3, W = mg
= 1000× 9.8 = 9800 N m 1000
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d ) m = W
= 1000 = 102 kg, ρ = m = 102
= 51
kg/m3 , v = 1
= 1 = 0.0196 m3 /kg g 9.8
V 2 ρ 51
1 1 = 0.02
lbm/ft3, m = ρV = 0.02× 20 = 0.4 lbm,
1.37 a ) ρ = =
v 50
W = m g
= 0.4 lbm × 32.2
ft/s2
= 0.4 lbf
gc 32.2 ft-lbm/lbf-s2
b ) v = 1
= 1
= 50 ft
3 /lbm, m = ρV = 0.02× 20 = 0.4 lbm,
ρ 0.02
g 32.2 ft/s2
W = m = 0.4 lbm × =
0.4 lbf gc
c ) W = m g = 1000 lbm × 32.2 ft/s2 2 = 1000 lbf
gc 32.2 ft-lbm/lbf-s
v = V = 20
= 0.02 ft3 /lbm, ρ = 1 = 1 = 50 lbm/ft3
m 1000 v 0.02
d ) m = W g g c = 500 lbf × 32.2 32.2 ft-lbm/lbf ft/s2 -s
2 = 500 lbm
v = V
= 20
= 0.04 ft
3 /lbm, ρ = 1 = 1 = 25 lbm/ft
3
m 500 v 0.04
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3
This problem should demonstrate the difficulty using English units with
lbm and lbf! Note that lbm and lbf are numerically equal at sea level
where g = 32.2 ft/s2, which will be true for problems of interest in our
study. In space travel, g is not 32.2 ft/s2.
1.38 ρ = 1 = 1 = 0.25 kg/m
3 , SG = ρx = 0.25 = 0.00025 , m = V = 8
m3
= 2 kg
v 4 ρwater 1000 v 4 m /kg
m
2.)
W = mg = 2 kg × 9.81s 2 = 19.62 N . (We used N = kg·m/s
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1 1 ρ
1.39 v = ρ = 0.2 = 5 ft3 /lbm , SG = ρwaterx =62.40.2 lbm/ft
lbm/ft33 = 0.00321
= ρV = 0.2× 20 = 4 lbm, W = m g = 4 lbm × 32.2
ft/s2 = 4 lbf
m
gc 32.2 ft-lbm/lbf-s2
1.40 Only (ii) can be considered a quasi-equilibrium process. Process (i) uses
a temperature distribution in the room to move the heated air to other
locations in the room, i.e., the temperature is not uniform. When the
membrane in process (iii) is removed, a sudden expansion occurs, which
cannot be considered a quasi-equilibrium process.
1.41 From Table B-1 in the Appendix, we observe that. So,
i) SG = 1.225 kg/m3 = 0.001225
1000 kg/m3
0.6012×1.225 kg/m3
ii) SG = = 0.000 736
1000 kg/m3
0.3376×1.225 kg/m3
iii) SG = = 0.000 414
1000 kg/m3
1.42 From Table B-1 in the Appendix, we observe find the local
atmospheric pressure. First, cm
2 × 9.81 m = 206 000 N/m
2 or 206 kPa
gage P = 2.1 kg × 1002
g cm2 m
2 s
2
(We used N = kg·m/s2.)
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i) P = 206 kPa + 101 kPa = 307
kPa ii) P = 206 kPa + 101×
0.887 kPa = 296 kPa iii) P = 206 kPa +
101× 0.5334 kPa = 260 kPa
(We could have used Patm = 101.3 kPa or even 100 kPa since extreme
accuracy is not of interest)
1.43 Refer to Fig. 1.6 and Eq. 1.14. The pressure in the tire would be P2 and
P1 would be open to the atmosphere:
P 334 000 N/m
2
gage cm2 m2 s2 m2
P 50 m or 2500
mm
2 1 2 m3 s2 m
N kg m 2
1.44 P = ρ gh. 100 000 m2 = 786m3 × 9.81 s2 × h. ∴ h = 13.0 m (We
used N = kg·m/s .)
1.45 P = 10 atm ⋅ 100 kPa
= 1000 kPa. ∴ P = 1000 kPa − 100 kPa =
900 kPa
atm g
1.46 P = ρ g h = 1000 kg × 9.81 m
× 0.25 m = 2453 Pa = 2.45
kPa gage water m3 s2
P = ρHg g hHg . 2453 = (1000× 13.6)× 9.81× hHg . ∴ hHg = 0.0184m
or 0.724 in.
1.47 A measured pressure is a gage pressure.
− P = ρ g h . 334 000 N = ( 1000 × 13 . 6 ) kg × 9 . 81 m × h . ∴ h = 2 .
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a) P = ρ gh = 13 600 × 9. 81× 0.10 = 13 340 Pa or 13.34 kPa gage
b) P = ρ gh = 13 600 × 9. 81× 0.28 = 37 360 Pa or
37.36 kPa gage
P =P +P P =P +P
1.48 a) abs gage atm = 5 + 0.371×
14.7 = 10.45 psia or 1505 psfa
b) abs gage atm = 20 + 0.371× 14.7 = 25.45 psia or 3665 psfa
1.49 Consult the Internet
1.50 Consult the Internet
1.51 T ( °R ) = T( °F) + 460 = 120 + 460 = 580°R
1.52 T ( °C) = T(K) − 273 = 3 − 273 = −270°C
1.53 T ( °R) = T(° F) + 460 = 400 + 460 = 860°R
1.54 T (K) = 37 + 273 = 310 K
1.55 Use Eq. 1.20:
a) R = R e β ( T0 −T )/T0T = 3000e4220(25 − 60)/ 298 ×333 = 677 Ω
0
b) R = R e β ( T0 −T
)/T0T = 3000e4220(25 −120)/ 298 ×393 = 97.8 Ω
0
c) R = R e β ( T0 −T
)/T0T = 3000e4220(25 −180)/ 298 ×453 = 23.6 Ω
0
1.56 Use V = β V T .
0.00018 2 4 3
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H = 0.00018× 3 π × 0.003 × 20. ∴ a) π 4
H = 0.016 m or 16 mm
b) π 4 H = 0.00018× 3 π × 0. 32 mm
0.000182 4
c) π 4 H =
0.00018× 3 π × 0.
1.57 V = 60 mi × 5280 ft/mi = 88 ft/s , KE = m V 2
hr 3600 s/hr 2gc
= 2500 lbm × 88
2 = 300,600 ft-lbf
2 × 32.2 ft-lbm/lbf-s2
6 © 2015 Cengage Learning. All Rights Reserved. May not be scanned,
copied or duplicated, or posted to a publicly accessible website, in
whole or in part.
or 300,600 ft-lbf = 386 Btu
778 ft-lbf/Btu
The English unit on energy is most often the Btu (some authors use
BTU).
1.58 KE + PE = 12 m V 2 + mgh = 12 × 5000 × 802 + 5000 × 9.81× 1000
= 65× 106 N ⋅ m = 65 MJ
1.59 At 10 000 m, g = 9.81 − 3.32 × 10−6
× 10 000 = 9.777 m/s2
Wsurface = mg = 140 000 × 9.81 = 1.373×106 N
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W10 km = mg = 140 000 × 9.777 = 1.369 ×106 N
10 000 10 000
PE = ∫ mgdh = ∫ 140 000(9.81− 3.32 ×10−6
h ) dh
0 0
−6 10 0002 10 − 0.0023×1010
= 1.371× 1010 N
m or 13.71 GJ
Solutions to Final Exam
1. A
2. D W = N ⋅ m/s = ( kg ⋅ m/s 2 )m/s = kg ⋅ m
2 /s
3
3. C Sum forces in the vertical direction (be sure and use Pa and not kPa):
∑ F = 0. PA − W − Kx = 0
x 254 m or 25.4 cm
If absolute pressure is used, the atmospheric pressure acting on the top of
the cylinder must be included.
4. A
5. B Since the temperature is below the boiling point (120.2°C from Table
C-2) of water at 0.2 MPa, refer to Table C-1 and use hf = 461 kJ/kg.
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6. D The specific volume at 160°C is vg = 0.307 m3/kg (Table C-1). From
Table C-3 we search at 800°C and
observe at 1.6 MPa that v = 0.309 m3/kg. So, P2 = 1.59 MPa. (No
careful interpolation is needed.)
7. C The volume is assumed to be constant (it doesn’t blow up like a
balloon!). The ideal gas law is used: P1V1 = mRT1 and P2 V 2 =
mRT2 so P1 / P2 = T1 / T2 . Then, using absolute temperatures and
pressures (assume atmosphere pressure of 100 kPa since it is not
specified),
539 kPaor 439 kPa gage
P2 433
8. B If the pressure is constant, the work is mP(v2 – v1). The result is
W = mP ( v 2Units: kg − v1 ) = 8⋅× kN800 ⋅× m( 03. =2608 kN −⋅ 0m
. 2404) = 131 kJ
= kJ m2 kg
9. A First, find the height H of the piston above the cylinder bottom:
m = ρ AH . 688 m
The temperature when the piston hits the stops in this constant-pressure
process is
T = T V2 = 473× 1.188A = 333 K or 59.9°C
2 1 V 1.688A
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1
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10. A For this constant pressure process, the heat transfer is
Q = mC p T = 2 × 1.0 × ( 400 − 20) = 760 kJ
11. B The temperature at the final state must be known. It is T = T P2 =
673× = 168 K. So
2 1 P 400
1
Q = mC v T = 2 × 0. 717 × ( 673 − 168) = 724 kJ
12. C For an isothermal process Q = W = mRT ln V 2 / V1 so the heat
transfer is
Q = mRT ln V2 = 1. 0 × 0. 287 × 473× ln 1
= −94.1 kJ
V 2
1
13. D The heat from the copper enters the water:
mc C p , c Tc = mw C p , w Tw . 10 × 0.39 × (200 − T2 ) = 50 × 4.18× (T2 −
10). T2 = 13.5°C
14. A Only A does not have a fluid flowing in and/or out.
15. C The density is found from Table C-3 using ρ = 1/ v :
m = ρ AV = 1 AV = 1
× (π × 0. 142 ) × 2
= 1.89 kg/s v 0.06525
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16. C The power required by a pump involving a liquid is
P2 − P1 6000 − 20
W = m = 5 ×
= 29.9 kW or 40.1 hp ρ 1000
17. D Equate the expression for the efficiency of a Carnot engine to the
efficiency in general:
TL Wout 10
η = 1− = . Qin = = 29.6 kJ/s TH Qin 1 − 313 /
473
Qout = Qin − W = 29. 6 − 10 = 19.6 kJ/s
18. A The maximum possible efficiency would be ηmax = 1 − TL = 1 −
283 = 0.237 . Consequently,
TH 371
Wout 2000
= 0.237. Wout, max
= 0.237 × + 10 = 10.2 kW. The engine is improbable.
Qin 60
B If COP > 1, A is violated. If COP = 1, C occurs. The condition that
W > QL is very possible.
20. D The heat transfer from the high
temperature reservoir is Q H = Q L + W = 20 + 8 = 28 kJ/s.
The
efficiency of the engine is
thus η = W =
8
= 0.286. The Carnot efficiency
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yields
QH 28
η T = 410 K or 137°C
H
TH
Obviously the temperatures must be absolute.
21. C The entropy change of the copper is mCplnT2/T1 and that of the
water is Q/T. Hence,
mcu C p ,cu T
T 2 + Q = m C ln T 2 +
S = m C ln
net cu p ,cu T1 Twater cu p,cu T1 Twater
= 10 × 0.39ln 293
+ = 0.123 kJ/K
373 293
The copper loses entropy and the water gains entropy. Make sure the
heat transfer to the water is positive.
22. C The maximum work occurs with an isentropic process: s1 = s2 =
7.168 kJ/kg·K. The enthalpy at the turbine exit and the work are found
as follows (use Tables C-3 and C-2):
s2 = s1 = 7. 168 = 0. 6491+ x 2 ( 7.502). ∴ x2 = 0.869
∴ h2 = 192 + 0.869 × 2393 = 2272 kJ/kg and wT = h = 3658 − 2272
= 1386 kJ/kg
The copper loses entropy and the water gains entropy. Make sure the
heat transfer to the water is positive.
23. A The minimum work occurs with an isentropic process for which
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T2 = T1 ( P2 / P1)k −1/ k = 300× 60.2587 = 477 K
∴ wC = C p (T2 − T1) = 1.0 × ( 477 − 300) = 177 kJ/kg
24. D The maximum possible turbine work occurs if the entropy is constant,
as in Problem 22 which is 1386 kJ/kg. The actual work is wT = h1 − h2
= 3658 − 2585 = 1073 kJ/kg . The efficiency is then
η = w = 10731386 = 0.774 or
77.4% T w
T , s
25. D The heat that leaves the condenser enters the water:
mw C p , w Tw = ms ( h1 − h2 ). mw × 4.18× 20 = 4 ×
( 2609.7 − 251). ∴ mw = 113 kg/s
26. B Heat transfer across a large temperature difference, which occurs in
the combustion process, is highly irreversible. The losses in A, C¸ and D
are relatively small.
27. B The combustion process is not reversible.
28. A The rate at which heat is added to the boiler is
Q B = m( h3 − h2 ) = 2 × ( 3434 − 251) = 6366 kJ/s
29. C The turbine power output is
WT = m( h3 − h4 ) = 2 × ( 3434 − 2609. 7) = 1648 kW
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30. D The rate of heat transfer from the condenser is
QC = m( h4 − h1) = 2 × ( 2610 − 251) = 4718 kJ/s
31. B The required pump horsepower follows:
P 5000 − 20 WP = m = 2 ×= 9.96 kW or 13.35
hp ρ 1000
k−1
32. C First, find the temperature at state 2: T2 =
T
1 V1
= 293× 80.4 =
673 K. Then
V2
q 2 -3 = C v (T3 − T2 ) = 0. 717 × (1473 − 673) = 574 kJ/kg
33. A The efficiency of the Otto cycle is
1 1
η = 1− k−1 = 1− = 0.435 or 43.5%
r 8
34. A The work output can be found using the efficiency and the heat
input:
w net = ηqin = 1 − 1
q
2-3 = 1 − 1 × 574
= 250
kJ/kg
rk−1 80 . 4
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35. D The heat input is provided by the combustor:
qin = C p (T3 − T2 ) = 1.0 × (1073 − 513) = 560 kJ/kg
36. B The pressure ratio for the assumed isentropic process is
P 2 =T 2 k /( k−1) = 513 3 .5 = 7.1
T1
293
P1
37. A The back-work ratio is found to be w comp C p (T2
− T1) = 240 − 20 = 0.44 or 44%
BWR = =
w C (T − T ) 800 − 300
T p 3 4
38. C The efficiency is the net work divided by the heat input:
T
η = w −wcomp = C p (T
3 − T4 ) − C p (T2 − T1) = 800 − 300 − (
240 − 20)
= 0.5
qin
C p (T3 − T2 ) 800 − 240
39. D The vapor pressure, using Pg = 5.628 kPa from Table C-1, is Pv =
Pgφ = 5.628× 0.9 = 5.065 kPa.
Then we have
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Pv = 0 . 622 ×
5.065 ω = 0.622
Pa 100 − 5.065
40. C Locate state 1 at 10°C and 60% humidity. Move at constant ω (it is
assumed that no moisture is added. If it were, the amount of water would
be needed) to the right until T2 = 25°C. There the chart is read to provide
the humidity as φ = 24%.
= 0 . kg 0332 w /kg a