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Review
for
Mid
Exam2Midterm
Exam
22014.12.150
ponitsFor
one
hourLabel
the
following
statements
as
either
true
(T)or
false
(F)Short
Response
Sectiontative
SectionCoverage
of
midexam2Lecture
5
(transient
conduction)-
Lecture
10(solutions)Lecture
11
(external
flow)
and
Lecture
12(internal
flow)
will
not
be
in
exam
2.You
can
turn
in
thei.e.
Dec.
4
(thursday)after
the
examTransient
conductionOverviewTransient
conduction (unsteady
state
conduction)a
heat
transfer
process
in
which
the
temperature
varies
with
both
time
andlocation
in
a
medium.is
initiated
whenever
a
steady-state
system
experiences
a
change
in
operatingconditions
and
proceeds
until
a
new
thermal
steady
state
is
achieved.The
temperature
variation
strongly
depends
on
Bi
For
Bi
<<1
For
moderate
to
large
values
of
Bi
For
Bi
>>
1To
use
the
lumped
capacitance
method
The
very thing
that
you
should s
to
calculate
the
Biot
number!!!
If
Bi
<
0.1,
the
error
with
using
the
lumped
capacitance
method
is
small1/
hAL
/
kA
RcondRconv
hL
kBiLumped
CapacitanceiWhen
is
the
steady
state?The
physical
meaning
of
t?When
t
=
t,
what
is
?
exp
hAs
t
exp
t
i
Ti
T
T
T
cV
t
Define:
thermal
time
constanttshA
cV
cV
1
RC
thermallumped
capacitance
hA
t
t
s
VchAst
Bi
FoL2cDimensionless
timeFo
tFourier
numberexpBi
Foi
T
Ti
T
Tytical
solution
to
the
Heat
Equation
for
aPlane
Wallwith
Symmetrical
Convection
ConditionsIf
the
lumped
capacitance
approximation
can
not
be
made,
consideration
mustbe
given
to
spatial,
as
wellas
temporal,
variations
in
temperature
during
thetransient
process.For
a
plane
wall
with
symmetrical
convectionconditions
and
constant
properties,
without
generation,
the
heatequation
andinitial/boundary
conditions
are:2T
1
Tx2
tT
x,0
Tix0
0Tx
h
T
L,t
T
xLk
Tx
Existence
of
seven
independent
variables:T
T
x,t,Ti
,T
,
k,,
hHow
may
the
functional
dependence
be
simplified?of
HeatEquation
andInitial/Boundary
Conditions:Dimensionless
temperature
difference:
*
T
T
i
Ti
T
xx
*
LDimensionless
space
coordinate:Dimensionless
time:t
*
tL
2
FoFo
the
FourierNumber
*
f
x
*,
Fo,
BiNon-dimensionalization
expBi
Foi
Ti
T
T
TRecall
Fo
in
the
result
oflumped
capacitance
methodT
T
x,t,Ti
,T
,
k,,
h112T
1
Tx2
tT
x,0
Tix0
0TxxLk
Tx
h
T
L,t
T
i
*Lx
*
xt
*
L2t
Fo
*
T
T
i
i
T
T2
(T
T
)
1
(T
T
)x2*(x*,0)
1
t2
1
x2
t2
(*i
)
1
(*i
)x2
t2
(*)
(*)x*2Fox
*
0*
*
0xx
*
1
*
Bi
*
(1,t
*)x
*The
BiotNumber:kBi
hLNumerical
Methods
for
Two-Dimensional,
Steady-State
ConductionProcedure:–Step
1:
Represent
the
physical
system
by
a
nodal
network
(ormesh,
grid).–Step
2:
to
obtain
a
finite-difference
equation
(algebraic)
foreach
node
of
unknown
temperature.Method
1:
Finite-difference
form
of
the
heat
equation
(mathematics)Method
2:
Theenergy
balance
method
(physics)–Step
3:
Solve
the
resulting
set
of
algebraic
equations
for
theunknown
nodal
temperatures.The
Nodal
Networkidentifies
discrete
points
at
which
the
temperature
is
to
bedetermined;
uses
anm,n
notation
to
designate
their
location.What
is
represented
by
thetemperature
at
a
nodal
point,as
for
example,
Tm,n?m
-
1/2n
-1/2deAverage
temperature
ofelement
volumeincrementl
or
ElementeNodal
network
x
incrementnodal
poionrt
noyCntorolvuomStep
2:
Develop
the
finite-difference
equationsMethod
1:
Finite
–difference
form
of
the
heat
equation02T
2T
qx,
y
m,n2T
T
Tm1/2,n
x
xx2
y2
kApproximatem
-
1/2m
+
1/2what
if
x
0?m1/2,n
x
Tm1,n
Tm
,nxm1/2,nx2
T
Tm
,n
Tm1,nxm1/2,nx
TxEin
Eg
0Consider
application
to
an
interior
nodal
point(one
that
exchanges
heat
by
conduction
with
four,equidistant
nodal
points):4x
y
0i1where,
for
example,Tm1,n
Tm,nqm1,nm,n
k
y
x?Est(assume
that
conduction
transfer
occurs
exclusively
through
lanes)Method
2
: The
Energy
Balance
MethodNo
need
to
derive
based
on
the
heat
i.e. erning
equation.As
aconvenience
that
obviates
the
need
topredetermine
the
direction
of
heatflow,
assume
all
heat
flows
are
into
the
nodal
region
of
interest,
and
express
allheat
rates
accordingly.
Hence,
the
energy
balance
es:Control
volumeSurfacem
-
1/2Nodes
at
surfaceConsider
an
external
corner
with
convection
heat
transfer.
(no
generation)qm1,nm,n
qm,n1m,n
qm,n
0withx
,ym1,nm,n1T
Tkkhx
2
T
2hx1
T
0m,nyk
2
Tm1,n
Tm,nxxk
2Tm,n1
Tm,nym,nhxT
T
2
hm,n
yT
T
2Example某二 态热传递。材料导热系数λ。导热材料的上表面温度恒定为t0。其余三面与温度tf的流体进行对流换热,表面对流换热系数hf。现若节点划分 ,各网格边长均为Δx。试由 展开法(Finite
–difference
method)写出节点1的方程,由热平衡法(EnergyBalance
Method)写出节点14的方程。Introduction
to
ConvectionFlow
and
Thermal
ConsiderationsWhen
a
moving
fluid
comes
into
contact
with
a
surface
at
sometemperature
difference
(e.g.
heated
surface,
cold
fluid)
the
fluid
willtransfer
heat
to/from
the
surface
in
a
process ogous
toconduction
(randommotion
of
the
fluid)advect
heat
away
from
the
point
of
contact
by
its
motion
(bulkmotion
ofthe
fluid)Advection
=
bulk
fluid
motion
onlyThe
combined
effect
of
these
two
phenomena
is
called
convectionRate
equationNewton’s
Law
of
Cooling21heat
flux[W/m2]q"
h
Ts
Theat
transfer
coefficient[W/m2-K]surface
temperature[K]fluid
temperature[K]q
Ah
Ts
Tnotes:the
heat
transfer
coefficientFunction
of
fluid
properties,
flow
conditions,
and
geometryin
order
to
study
convection
heat
transfer,
we
must
also
study
fluiddynamicsConvection
Heat
Transfer
CoefficientsLocal
Heat
Flux
and
Coefficient:qs
h
Ts
T
Average
Heat
Flux
and
Coefficient
for
a
Uniform
Surface
Temperature:q
hAs
Ts
T
q
A
qdAs
TssssAhdA
TsAssAh
1
hdAFor
a
flat
plate
in
parallel
flow:1LLoh
hdxWhatPARAMETERS
affect
h
?Fluid
properties
(temperature
dependent)Flow
conditionsGeometry…h
f
(u,
k,
cp
,
,,
,l....)23CLASSIFICATIONSMECHANISMFree
(Natural)
ForcedGEOMETRYInternal
ExternalSTATESingle-PhaseTwo-Phase24erning
equations
for
convection25MassMOMENTUMEnergy
x
y(u
u
u
v
u
)
dxdyConsult
fluid
dynamics
textbooks
pleaseConvection
term
of
MomentumBody
force
pressureViscousMomentum
equation
(Navier-Stokes
equation)(u
u
u
v
u
)
F
p
(
2u
2u
)xt
x
y
x
x2
y2ρvdxConvectionerning
equationsu
v
0;x
y
p
2u
2u
)x
(
x2y2(v
u
v
v
v
)
F
p
(
2v
2v
)y
x2
y2t
x
yy(u
u
u
v
u
)
Ft
x
yx2T
u
T
v
T
k2
2
T
Tt
x
y
cp
x
y
2
u
2if
with
viscous
dissipation
cp
yBoundary
layer
on
a
plate
in
parallelcoming
flowVelocity
and
thermal
boundary
layerPhysics,
characteristics,
and
definitionsBoundary
Layer
developmentHeat
transferVelocity
:,22Thermal
:2x
y2u
u
xpdpdx2T
2Tx2
y2Boundary
layer
approximations!Boundary
Layer
EquationsNow
it
could
be
solved
!33Consider
concurrent
velocity
and
thermal
boundary
layer
developmentforsteady,pressible
flow
with
constantfluid
properties
,
cp
,
k
andtwo-dimensional,negligible
body
forces.Example2
2对流换热的能量微分方程为(假设:流动是二维的;流体为不可压缩的
型流体;流体物性为常数、无内热源;粘性耗散产生的耗散热忽略不计)t
u
t
v
t
2t
2t
x
y
x
y
cp
分别说明其中各项所代表的物理意义基于上式写出稳态下、边界层内的能量方程。Solutions
for
the
flat
plate
in
parallelflow
(Laminar
flow
region)35RecNon-dimensionalization
and
similarityparameters3637u*
v*
0x*
y**
u*
*
u*
12u*u
x*v
y*
u
Lu
Lx*y*
v*
T
*
y*2y*2ReL1
1
2T
*u*
T
*PrSimilarity
parametersRePrNuSolution
(flat
plate
in
parallel
flow)39xNu
0.332Re1
2Pr1
3x1
1khxx
0.332
u
x
2
3
a
Example管内对流换热,关于
数Pr,以下正确的是:代表了粘性力与惯性力的相对大小代表了流动边界层与热边界层厚度的相对大小
c)其数值与温度相关,但是计算中在变化不大的情况下常取定性温度对应的数值d)在换热准则关系式涉及的三个准则数即Nu,Re,
Pr数中,Pr是唯一一个与传热相关的准则数。More
about
the
solutionswhen
to
usehow
to
usefunctional
form41Structure
of
a
procedure
for
solution
ofconvection
problems42Establish
the
geometry
of
the
situationDetermine
the
fluid,
and
evaluate
the
fluid
propertiesEstablish
the
boundary
conditions
( kind,
…)Establish
the
flow
regime
as
determined
by
the
Reynoldsnumber.Select
the
appropriate
equation,
taking
into
account
theflow
regime
and
fluid
property
restrictions
whi
ayapplyCalculate
the
value(s)
of
the
convection
heat
transfercoefficient
and/or
heat
transfer.Solution1
2
1
3Prx
xNu
0.332Re1
1khxx
0.332
u
x
2
3
a
When
can
you
use
this
correlation?Assumptions:
Steady,
pressible,
laminar
flow
withconstant
fluid
properties
and
negligible
viscous
dissipationand
recognizing
that
dp/dx
=0Classification:
Forced,
externalGeometry:
Flat
plate
in
parrellel
flowPr
>=
0.6,
Re
<
5*105Boundary:
isothermalThe
fluid
properties
to
deter
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