kuliah-3 fundamental of convection3
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Nazaruddin SinagaLaboratorium Efisiensi dan Konservasi Energi
Fakultas Teknik Universitas iponegoro
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2
Convection
Bulk movement of thermal energy in fluids
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3
Hot Water Baseboard Heating and
Refrigerators
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Cold air sinks
Where is thefreezercompartment put in
a fridge?
Freezercompartment
It is put at the top,because cool air
sinks, so it cools thefood on the way
down.
It is warmer at
the bottom, sothis warmer air
rises and aconvection
current is set up.
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Convection
What happens to the particles in a liquid or a gas when you
heat them?
The particles spread out and becomeless dense.
This effects fluid movement.
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Fluid movement
Cooler, more dense, fluids sinkthrough warmer, less dense fluids.
In effect, warmer liquids and gases rise up.
Cooler liquids and gases sinks
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Convectionis the process in which heat is carried from
place to place by the bulk movement of a fluid.
Convection currentsare set up when a pan of water is
heated.
Convection
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Why is it windy at the seaside?
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Theory of Convection Heat Transfer : Newtons
Law & Nusselts Technology
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Concept of Solid Fluid Interaction : Maxwells Theory
Diffuse reflection
U2
UU
U2
U1
U1
U2
Specular reflection
Perfectly smooth surface (ideal surface) Real surface
The convective heat transfer is defined for a combined solid and fluid
system.
The fluid packets close to a solid wall attain a zero relative velocity close to
the solid wall : Momentum Boundary Layer.
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The fluid packets close to a solid wall come to thermal
equilibrium with the wall.
The fluid particles will exchange maximum possible energy
flux with the solid wall.
A Zero temperature difference exists between wall and
fluid packets at the wall.
A small layer of fluid particles close the the wall come to
Mechanical, Thermal and Chemical Equilibrium With solid
wall.
Fundamentally this fluid layer is in Thermodynamic
Equilibrium with the solid wall.
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Physical Mechanism of
Convection Heat Transfer
Convection is the mechanism of heat transfer inthe presence of bulk fluid motion.
It can be classified as:
1) Natural or free convection:The bulk fluid motion is due to buoyant force caused by densitygradient between the hot and cold fluid regions. The temperature &velocity distributions of free convection along a vertical hot flatsurface is shown in figure below.
Ts
T T
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2) Forced convection :
The bulk fluid motion is caused by external means, suchas a fan, a pump or natural wind, etc.
u
U
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The properties of the flow fields
Due to the properties of fluid both velocity and thermalboundary layers are formed. Velocity boundary layer iscaused by viscosity and thermal boundary layer iscaused by both viscosity and thermal conductivity of the
fluid.
Internal versus external flow
- External flow : the solid surface is surrounded by the
pool of moving fluid- Internal flow : the moving fluid is inside a solid channel
or a tube.
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The properties of the flow fields
Laminar flow versus turbulent flow
- Laminar flow: the stream lines are approximately parallel toeach other
- Turbulent flow: the bulk motion of the fluid is superimposed
with turbulence
u
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Heat Transfer in Equilibrium Layer
The thickness of stagnant layer decides the magnitude of normal temperaturegradient at the wall.
And hence, the thickness of wall fluid layer decides the magnitude of convectiveheat transfer coefficient.
Typically, the convective heat transfer coefficient for laminar flow is relativelylow compared to the convective heat transfer coefficient for turbulent flow.
This is due to turbulent flow having a thinner stagnant fluid film layer on theheat transfer surface.
At the wall for fluid layer :
layermequilibriuAcross,
TThA
y
TAk wallfluidfluid
TT
yTk
hwall
wall
fluid
At Thermodynamic equilibrium
wallwallfluid TT ,
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Estimation of Heat Transfer
Coefficient
TT
yTk
h wall
wall
fluid
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0
''
y
Acrosss y
TkTThq
Non-dimensional Temperature:
TT
TT
s
Non-dimensional length:
L
yy *
0
*
0 *scaleLength
scaleeTemperatur
yy yy
T
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0
**
y
sfluids
yL
TTkTTh
fluidy k
hL
y
0
**
0* *
y
fluid
yL
kh
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This dimensionless temperature gradient at the wall is named as
Nusselt Number:
resistanceConvection
resistanceConduction
1
h
k
L
k
hLNu
fluid
fluid
fluidy k
hLy
Nu
0
**
Local Nusselt Number
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Average Nusselt Number
avgfluid
avg
avgk
LhNu
,
Estimation of heat transfer coefficient is basically
computation of temperature profile at the wall.
A general theoretical and experimental study isessential to understand how the stagnant layer is
developed.
The global geometry of the solid wall and flow
conditions will decide the structure of stagnant layer.
Basic Geometry : Internal Flow or External Flow.
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The governing parameters of convection
heat transfer
Newtons law of cooling
The main objective to study convection heat transfer is todetermine the proper value of convection heat transfercoefficient for specified conditions. It depends on thefollowing parameters:
- The Bulk motion velocity, u, (m/s)- The dimension of the body, L, ( m)
- The surface temperature, Ts,oC or K
- The bulk fluid temperature, T,oC or K
( )sQ hA T T
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The governing parameters of convection
heat transfer (Cont.)
- The density of the fluid, , kg/m3
- The thermal conductivity of the fluid, kf, (W/m.K)
- The dynamic viscosity of the fluid, , (kg/m.s)
- The specific heat of the fluid, Cp, (J/kg.K)
- The change in specific weight, , (kg/(m2s2) or (N/m3)
- The shape and orientation of the body, S
The convection heat transfer coefficient can be written as
h = f( u, L, Ts, T, , kf, , Cp, , S)
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It is impossible to achieve a correlation equation forconvection heat transfer in terms of 10 variables. A betterway to reduce the number of variables is required.
Dimensionless analysis
There are 11 parameters with 4 basic units (length, m), (mass,
kg), (temperature, oC or K) , and (time, s).
Applying the method of dimensional analysis, it can be
grouped into 11- 4 = 7 dimensionless groups, they are:
3 2
2( , , , , , )
p s
p
c ThL uL g L uF S
k k T c T
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1. Nusselt number : =
2. Eckert number : =
3. Reynods number : =
4. Temperature ratio: s =
5. Grashof number : =
6. S : shape of the surface
7. Prandtl number: =
hL
k
uL
3
2
g L
pc
k
2
p
u
c T
sT
T
LNu
ReL
LGr
Pr
kE
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The Governing Parameters of
Convection Heat Transfer
The convection heat transfercoefficient can be written as:
Nu= f( Ek, ReL, s, GrL, Pr, S)
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To find Reynolds numberChoosing density (), dimension (L), surface temperature (Ts), anddynamic viscosity () as the 4 basic parameters, and velocity (u) as the
input parameter. The dimensionless number is obtained by solving the 4constants, a, b, c, & d.
13
0
( ) ( ) ( ) ( )
3 1 0
0
0
1 01, 0, 1, 1
Re
a b c d
s
a b o c d
o
L
L T u
kg kg LL C
L sL sL a b d
kg a d
C c
s dd c a b
Lu
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Simply the dimensionless equations !!!
Now we have reduced the equation involving 11
variables into a 7 dimensionless group equation.
However, 7 dimensionless groups is still too large, we
need neglecting the unimportant dimensionlessgroups.
Eckert number is important for high speed flow. It can be
neglected for our application.
If the average fluid temperature is used for getting the fluid
properties, the temperature ratio can also be discarded.
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Nu= f( Ek, ReL, s, GrL, Pr, S)
After neglecting the two unimportant
dimensionless groups, the generalconvection equation is
(Re , Pr, , )L L LNu F Gr S
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Forced Convection: the density change is very small, theGrashoff number is neglected
Natural Convection: there is no bulk fluid motion induced byexternal means, u = 0, Reynolds number is disappeared.
(Re , Pr, )L LNu F S
( , Pr, )L LNu F Gr S
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The Physical Meaning of
The Dimensionless Numbers
Nusselt NumberIt is the ratio of convection heat transfer
rate to the conduction heat transfer rate.
Consider an internal flow in a channel of
height L and the temperatures at the lowerand upper surfaces are T1 & T2, respectively.
The convection heat transfer rate is
The conduction heat transfer rate is
The ratio
&Qcov
hA(T1T
2)
&Qcond
kA
L(T
1 T
2)
NuL
&Qcov
&Qcond
hA
kA
L
hL
k
u
T1
T2
L
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The Reynolds Number
It is the ratio of inertia force to viscous force of the
moving fluid.
- Inertia force
- The viscous force
- The ratio
3 2 2 2 2
2 ( )i
L LF ma L L L u
s s
2 2
v
u uF A L L uL
y L
ReLuL uL uL
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The Prandtl Number
It is the ratio of the momentum diffusivity to the thermal
diffusivity. The momentum diffusivity is the kinematic viscosity andit
controls the rate of diffusion of momentum in a fluid
medium.
Thermal difusivity controls how fast the heat diffuses in amedium. It has the form
The ratio of the two is called Prandtl number.
Pr p
p
c
k k
c
p
k
c
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The Thermal Expansion Coefficient
It is defined as
The negative sign results from the fact that, for gases, the
change of density with respect to temperature under constant
pressure process is always negative. From ideal gas law
For ideal gas, the thermal expansion coefficient is the inverse
of the absolute temperature
1( )p
T
0p RT dp RdT RTd ( )pd
dT T
1
T
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Grashoff Number
The Grashoff number represents the ratio of
the buoyant force to the viscous force.
3
2
g LGr
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Grashof number
The change of density is
Substituting into Grashof number
The subscript L means that the characteristic length of the
Grashof number. It may be the length of the surface. Forideal gas, GrLis
( ) ( )T T T T T
3 33
2 2 2
( ) ( )L
g T T L g T T Lg LGr
3
2
( )L
g T T LGr
T
Ts
T T
Buoyant force
Viscous force
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Chapter 1 Chee 318 37
Example
Air at 20C blows over a hot plate, which is maintained ata temperature Ts=300C and has dimensions 20x40 cm.
CT 20
q
CTS300
Air
The convective heat flux is proportional to
TTq Sx"
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Chapter 1 Chee 318 38
The proportionality constant is the convection heattransfer coefficient, h (W/m2.K)
)(" TThq Sx Newtons law of Cooling
For air h=25 W/m2.K, therefore the heat flux is qx= 7,000
W/m2
The heat rate, is qx= qx. A = qx. (0.2 x 0.4) = 560 W.
In this solution we assumed that heat flux is positive when heatis transferred from the surface to the fluid
How would this value change if instead of blowing air we hadstill air (h=5 W/m2.K) or flowing water (h=50 W/m2.K)
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The nd
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