THERMODYNAMICS FIRST LAW OF THERMODYNAMICS – CLOSED SYSTEM heat
Chapter 4 The First Law of Thermodynamics: Control Volumes
description
Transcript of Chapter 4 The First Law of Thermodynamics: Control Volumes
Chapter 4Chapter 4 The First Law of The First Law of Thermodynamics:Thermodynamics:Control VolumesControl Volumes
4-1-1 Conservation of Mass principle
4-1 Thermodynamic analysis of 4-1 Thermodynamic analysis of Control VolumeControl Volume
CVei mmm
4-1-2 Conservation of Energy principle for Control Volume
The net energy change in energy of CV
Total energy crossing boundary
+ Total energy of mass entering CV=
-Total energy of mass leaving CV
4-1-3 Flow Work
PAF
FLW flow PAL PV
pvw flow
4-1-4 Total Energy of a Flowing Fluid
On a unit-mass basis, the energy stored in fluid: pekeue
gzue 2
2V
Considering the flow work, we have
pvw The total energy of a flowing fluid (denoted θ): epv
)( pekeupv
4-1-5 Enthalpy
Internal energy and flow work usually transferred at the same time in flowing fluid, so we define pvuh
Professor J. Kestin proposed in 1966 that the term θ be called methalpy (from metaenthalpy, which means beyond enthalpy)
pekeh
4-2 The Steady-Flow Process4-2 The Steady-Flow Process4-2-1 Definition of Steady-Flow ProcessA process during which a fluid flows
through a control volume steadily
4-2-2 Characteristics of Steady-Flow Process
1. No properties in the control volume change with time
2. No properties changes at the boundaries of the control volume with time
3. The heat and work interactions between a steady flow system and its surroundings do not change with time
4-2-3 Energy Equation of Steady-Flow ProcessFrom the above discussion we can
conclude that:
2. The net change in energy of CV is Zero
mmm ei .1
Energy Equation of Steady-Flow
Total energy crossing boundary per unit time
=
Total energy of mass leaving CV per unit time
-Total energy of mass entering CV per unit time
0)2
()2
(22
ee
eeii
ii gzhmgzhmWQVV
)2
()2
(22
ii
iiee
ee gzhmgzhmWQVV
mmm ie since
)2
()2
(22
ii
iee
e gzhmgzhmWQ VV
Using subscript 1and subscript 2 for denoting inlet and exit states
)](2
[ 12
21
22
12 zzghhmWQ
VV
)(2 12
21
22
12 zzghhwq
VV
Dividing the equation by m yields
wzghq
2
or2V
wzgpvuq
2
2V
Work
3-3 Some Steady-Flow Engineering 3-3 Some Steady-Flow Engineering devicesdevices
3-3-1 Nozzles and Diffusers
q = Δh + ΔV2 / 2 + gΔz + w
q = 0 Δz = 0 w = 0
212
2
1then hh V
)(2 21 hh V
3-3-2 Steam Turbine
from q = Δh + ΔV2 / 2 + gΔz + ws
if q = 0; Δc = 0; Δz = 0
then ws = -Δh
= h1 - h2
3-3-3 Throttling Valves
From q = Δh + ΔV2 / 2 + gΔz + ws
as q = 0; ws = 0; z = 0 ; ΔV2 / 2 =0
then Δh =0
That is h1 = h2
3-3-4 Mixing Chambers
From q = Δh + ΔV2 / 2 + gΔz + ws
as q = 0; ws = 0; z = 0 ; ΔV2 / 2 =0
then Δh =0
That is ∑hin = ∑ hexit
3-3-5 Heat exchangers
From q = Δh + ΔV2 / 2 + gΔz + ws
as q = 0; ws = 0; Δ z = 0;ΔV2 / 2 =0
Δh =0
That is ∑hin = ∑ hexit
3-4 Unsteady-Flow Processes3-4 Unsteady-Flow Processes3-4-1 Model
1. The net energy transferred to the system:
dQ , e1dm1 , p1v1dm1
2. The net energy transferred out of the system:
dWs , e2dm2 , p2v2dm2
3-4-2 Conversation of Energy
)()( 2222211111 dmvpdmedWdmvpdmedQdE
])2
1([ 11111
211 dmvpdmgzudQdE V
])2
1([ 11
2111111 dmgzdmvpdmudQdE V
])2
1([ 22222
222 dmvpdmgzudW V
])2
1([ 22
2222222 dmgzdmvpdmudW V
])2
1([ 11
2111 dmgzcdmhdQdE
1121122
222 )
2
1()
2
1( dmgzchdmgzchdWdEdQ s
])2
1([ 22
2222 dmgzcdmhdW
Divide dτ on each side
)2
1()
2
1( 1
21112
2222 gzchmgzchmW
EQ
)1( )2
1()
2
1( 1
21112
2222 gzchmgzchm
EWQ
3-5 Uniform-Flow Processes3-5 Uniform-Flow Processes
1. At any instant during the process, the state of control volume is uniform
2. The fluid properties may differ from one inlet or exit to another, but the fluid flow at an inlet or exit is uniform and steady
The end of this chapter
Thanks for your attention!