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Chapter 1 Chee 318 1 Reminder: The General Balance Equation mulation = Creation Destruction + Flow in Flow Rate Equation Rate of Rate of Rate of tion = Creation – Destruction + Flow in – Flow out Applicable to any extensive property: mass, energy, entropy, momentum, electric charge
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Page 1: Chapter1_3

Chapter 1 Chee 318 1

Reminder: The General Balance Equation

Accumulation = Creation – Destruction + Flow in – Flow out

Rate Equation

Rate of Rate of Rate of Rate of Rate of Accumulation = Creation – Destruction + Flow in – Flow out

Applicable to any extensive property: mass, energy, entropy, momentum, electric charge

Page 2: Chapter1_3

Chapter 1 Chee 318 2

Reminder: System and Control Volume

• A system is defined as an arbitrary volume of a substance across

whose boundaries no mass is exchanged. The system may

experience change in its momentum or energy but there is no transfer

of mass between the system and its surroundings. The system is

“closed”.

• A control volume is an arbitrary volume across whose boundaries

mass, momentum and energy are transferred. The control volume

may be stationary or in motion. Mass can be exchanged across its

boundaries. Useful in fluid mechanics, heat and mass transfer

Page 3: Chapter1_3

Chapter 1 Chee 318 3

Reminder: Approaches for Analysis of Flow

In analyzing fluid motion we may take two paths:

1. Working with a finite region (=the control volume), making a

balance of flow in versus flow out and determining flow effects

such as forces, or total energy exchange. This is the control

volume method. This approach is also called “macroscopic” or

“integral method of analysis”.

2. Analysing the detailed flow pattern at every point (x,y,z) in the

field. This is the differential analysis, sometimes also called

“microscopic”.

Page 4: Chapter1_3

Chapter 1 Chee 318 4

Conservation of Energy

• Energy conservation on a rate basis:

Control Volume (CV)

Surroundings, S

Boundary, B (Control Surface, CS)

-Accumulation (Storage)

-GenerationAdditionthrough inlet

Lossthrough outlet

stst

outgin Edt

dEEEE

inE outE

gEstE

Inflow and outflow are surface phenomena Generation and accumulation are volumetric phenomena

Units W=J/s(1.1)

Page 5: Chapter1_3

Chapter 1 Chee 318 5

The Energy Balance

Page 6: Chapter1_3

Chapter 1 Chee 318 6

The Energy Balance

Rate of Energy Flow into CV: ininint WqmzgV

u

in2

2

Rate of Energy Flow out of CV: outoutoutt WqmzgV

u

out2

2

Rate of Energy Accumulation: CV

zg

Vum

dt

dt 2

2

ut :internal energy, V: velocity, z: potential energy, q: heat rate, W: work

Page 7: Chapter1_3

Chapter 1 Chee 318 7

The Energy Balance

02

2

2

2

outoutout

out

t

ininint

WqmzgV

u

WqmzgV

u

in

Substituting in equation (1.1) and assuming steady-state conditions:

Convention

inoutoutnet

outininnet

WWW

qqq

,

,q is positive when transferred from surroundings to system.

W is positive when transferred from system to surroundings

Page 8: Chapter1_3

Chapter 1 Chee 318 8

The Energy Balance

• For steady-state conditions the energy balance reduces to:

022

22

outnetout

out

tint WqmzgV

umzgV

u ,

in

(1.2)

The net work is:

inout, ]m ) [(]m ) [(P PWW shaftoutnet

Injection Work

The work term is divided in two contributions: Flow work, associated to pressure forces (=p, where is the specific volume) and (shaft) work done by the system.

Page 9: Chapter1_3

Chapter 1 Chee 318 9

Steady-Flow Energy Equation

pui t

0

22

22

shaft

out

Wq

zgV

pumzgV

pum

in

Recall:

m

VA

VAm

c

c

Mass flow rate (kg/s)

Volumetric flow rate (m3/s)

Units of [J/s]

Enthalpy per unit mass:

and )()( outinpoutin TTcii

Page 10: Chapter1_3

Chapter 1 Chee 318 10

Simplified steady-flow energy equation

• For steady state conditions, no changes in kinetic or potential energy, no thermal energy generation, neglible pressure drop:

)( inoutp TTCmq

Page 11: Chapter1_3

Chapter 1 Chee 318 11

Example (Problem 1.36 textbook)In an orbiting space station, an electronic package is housed in a compartment having a surface area As=1 m2, which is exposed to space. Under normal operating conditions, the electronics dissipate 1kW, all of which must be transferred from the exposed surface to space.

(a) If the surface emissivity is 1.0 and the surface is not exposed to the sun, what is its steady-state temperature?

(b) If the surface is exposed to a solar flux of 750 W/m2 and its absorptivity to solar radiation is 0.25, what is its steady-state temperature?

Page 12: Chapter1_3

Chapter 1 Chee 318 12

Surface Energy Balance

For a control surface:

0

0

"""

radconvcond

outin

qqq

or

EE

T

x

T1

T2

T

qcond”qrad”

qconv”

Page 13: Chapter1_3

Chapter 1 Chee 318 13

Example (Problem 1.55 textbook)The roof of a car in a parking lot absorbs a solar radiant flux of 800 W/m2, while the underside is perfectly insulated. The convection coefficient between the roof and the ambient air is 12 W/m2.K.

a) Neglecting radiation exchange with the surroundings, calculate the temperature of the roof under steady-state conditions, if the ambient air temperature is 20°C.

b) For the same ambient air temperature, calculate the temperature of the roof it its surface emissivity is 0.8

Page 14: Chapter1_3

Chapter 1 Chee 318 14

Chapter 1: Summary

Modes of Heat Transfer:

Conduction Convection Radiation

dx

dTkqx " )("

TThq Sx)( 44"

sursrad TTq

)( sursrrad TTAhq

qx”(W/m2) is the heat flux qx (W=J/s) is the heat rate

Energy Balances – written on a rate basis (J/s):

Conservation of Energy for a Control Volume Surface Energy Balance (does not consider volumetric phenomena)