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Introduction of Heat Transfer (Week4 21 & 23 Sept)

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(1)

Introduction of Heat Transfer (Week4 21 & 23 Sept)

(Week4, 21 & 23 Sept)

Ki-Bok Min, PhD

Assistant Professor

Department of Energy Resources Engineering S l N i l U i i

Seoul National University

(2)

Content of last lecture

• Heat Conduction

– Thermal conductivity Thermal conductivity Th l diff i it

x y z

q  iq  jq  kq    k T

– Thermal diffusivity

p

k

c

– Derivation of Heat Diffusion equation

T T T T

p

T T T T

k k k q c

x x y y z zt

 

– Solution methods

(3)

Today

• Steady state one-dimensional conduction

– A plane wallA plane wall

– Radial conduction in cylindrical coordinate

• Thermal conductivity measurement method

– Steady state methody – Transient method

(4)

Feed back on homework #1

• Distinction of formal and informal words.

– Like, a little bit, …

• Avoid using subjective, emotional words

– Veryy

• Proper tense (시제)

T t b ifi h l i

• Try to be more specific when you explain

– Use numbers if possible, take examples

B f bl f f il f l th

• Maintain a critical attitude

• 한국말을 영어로 직역하려고 하지말고, 이에 적합한 영어

Because of many problems of fossil fuel energy, the importance of renewable energy is increased.

,

표현이 무얼까라고 생각할 것.

• Run the spelling check – MS Word

(5)

Feed back on homework #1

• Why is the earth hot?

• Why is there a thermal gradient?

• Why is there a thermal gradient?

• Decay of radioactive element.

H t i t i f th th

• Hot interior of the earth

(6)

Feed back on homework #1

• What about the disadvantage of geothermal energy?

• Why don’t we use it now? Economic feasibility???

• Why don t we use it now? Economic feasibility???

• What about the safety of power plant in tectonic boundaries?

• Why doesn’t Korea build a geothermal power plant?

(7)

Homework #2

(8)

Thermal Resistance (열저항)

• Thermal resistance for conduction in a plane wall

– From Fourier’s lawFrom Fourier s law

Th h t

,1 ,2

s s

x x

T T

q q A kA dT kA

dx L



 

– Through rearrangement,

,1 ,2

s s

d

T T L

R

e Es,1 Es,2 L

R I A

Analogy with electrical resistance

– From Newton’s law of cooling (convection)

, t cond

x

R q kA I A

Thermal resistance for conduction 전도열저항

– From Newton s law of cooling (convection),

s

q q A hA T T

,

s 1

t conv

T T

R hA

, t conv

q hA

Thermal resistance for conduction 대류열저항

(9)

1D steady state solutions Pl ll

Plane wall

– 1D, steady state, no heat generation,

d dT 0 d k d

 

– From constant heat fluxdx dx

( )

T C C

– Applying BC,

1 2

( )

T x C x C

,1 ,2

(0) s ( ) s

T T and T L T

,2 ,1

s s

T T

C T and C

2 s,2 1

C T and C

L

(10)

Conduction

Stead state one dimensional cond ction Steady-state one dimensional conduction

– Temperature distribution,

,2 ,1 ,1

( ) ( s s ) x s

T x T T T

L

– Conduction heat transfer rate,

,2 ,1 ,1

s s s

L

( )

dT kA

qx  kA (Ts,1 Ts,2)

q kA T T

dx L

 

(11)

1D steady state solutions

Composite all (la ered rock) Composite wall (layered rock)

– Equivalent thermal conductivity for a series composite wall (layered rock).

1 1 n Li

k L

k L

n Li

1

eq i i

k L

k

1 i

1 1 LA LB LC

A B C

eq A B C

k L k k k

Tn T1

T0

A1

L1 A2 L2

A3 L3

An Ln

Tn T1

T0

k11 k22 k33 knn

(12)

1D steady state solutions

di l d ti i li d i l ll radial conduction in cylindrical wall

– 1D, Steady state, no heat generation,

1 T 0

krkr   0 r r r

(2 )

r

T T

q  kA  krL

– Heat transfer rate is a constant in the di l di ti

r r r

radial direction.

– Assuming constant k,

1 2

( ) ln

T r C r C

ln ln

Ts,1 C1 lnr1 C and T2 s,2 C1 ln r2 C2 T C r C and T C r C

(13)

1D steady state solutions

di l d ti i li d i l ll radial conduction in cylindrical wall

– Temperature distribution

associated with radial conduction through a cylindrical wall

through a cylindrical wall

,1 ,2

,2

1 2 2

( ) ln

ln( / )

s s

s

T T r

T r T

r r r

 

 

– Heat transfer rate is,1 2   2

,1 ,2

2

l ( / )

s s

r

Lk T T

q

– Thermal resistance

2 1

ln( / ) qr

r r

2 1

ln( / )r r R,

t cond 2

R Lk

(14)

1D steady state solutions

SSummary

(15)

Hydraulic conductivity measurement

Two groups of methods (Beardsmore & Cull 2001) Two groups of methods (Beardsmore & Cull, 2001)

• Steady-state method

– Divided-bar apparatusDivided bar apparatus

• Transient method

– Needle probe

(16)

Hydraulic conductivity measurement St d St t M th d

Steady State Method

– Use a ‘divided-bar apparatus’

– Measure the ‘k’ directly qx k T2 T1

L

 

y

– Takes long time to achieve thermal equilibrium More accurate than ‘transient method’

x L

– More accurate than ‘transient method’

– Rock sample in discs or cylindrical shape

– Top and bottom sections of the bar maintained at constant but different temperatures (warm

d t th t ! Wh ?) end at the top! Why?).

Beardsmore and Cull, 2001

(17)

Hydraulic conductivity measurement T i t M th d

Transient Method

– “Needle probe method” is the best known method.

– k can be deducted from the rate at which its T changed in

response to an applied heat response to an applied heat source.

Measure the thermal diffusivity – Measure the thermal diffusivity

(α)and thermal conductivity is calculated  need to know ρρ and cp.

p

k

c

Single needle probe Dual-needle probe

– Less accurate than ‘steady state’

method

p

Beardsmore and Cull, 2001

(18)

Hydraulic conductivity measurement

T i t M th d (2) l

Transient Method (2) - an example

– With a line source of heat and a temperature sensor packed closely

packed closely,

l / 4



ln( ) /

k Q t T

– Ql : applied heat per unit length(W/m)

t : time (second) t : time (second) T: Temperature (K)

Fi d li it d bt i k – Find a linearity and obtain k

P= V x I = 5 x 0.25 = 1.25W Q=P/0 1(cm)=12 5W/m Q P/0.1(cm) 12.5W/m

Gradient between 60 & 200 sec is ~3.449 K = 12.5/4π x 3.449 = 3.43 W/mK

Data from Beardsmore and Cull, 2001

(19)

Heat Diffusion Equation

• Verbal description of heat diffusion equation

– The rate at which the temperature at a point is changing with time The rate at which the temperature at a point is changing with time is proportional to the rate at which the temperature gradient at that point is changing in the direction of heat flow. (Middleton and

il k 1999) wilcock, 1999)

p

T T T T

k k k q c

x x y y z zt

 

(20)

Last lecture

• Steady state one-dimensional conduction

– A plane wallA plane wall

– Radial conduction in cylindrical coordinate

• Thermal conductivity measurement method

– Steady state methody – Transient method

Ti d d ( i ) d i

• Time dependent (transient) conduction

• Convective heat transfer, thermal expansion & thermal stress Convective heat transfer, thermal expansion & thermal stress

(very briefly)

(21)

Conduction T i t t t Transient state

• If a solid body is suddenly subjected to a change in

environment, some time must elapse before an equilibrium temperature condition will prevail in the body. Transient

heating/cooling process takes place before equilibrium ( t d t t )

(steady state).

• Transient (or unsteady) problem: ( y) p

– Arise when boundary conditions are changed

E ) if f t t i lt d t t t h i t i – E.g.) if surface temperature is altered, temperature at each point in

the system will also begin to change  The change will continue until a steady state temperature distribution is reached

until a steady state temperature distribution is reached.

(22)

Time dependent conduction i i fi it h lf bl

semi-infinite half space problem

• A single identifiable surface + a solid extends to infinity

• A sudden change of conditions is imposed at this surface  A sudden change of conditions is imposed at this surface  transient, 1D conduction occur within the solid.

S i i fi it lid (h lf ) id f l id li ti

• Semi-infinite solid (half-space) provides a useful idealization for many practical problems.

2 2

1

T T

x t

(23)

Time dependent conduction i i fi it h lf bl

semi-infinite half space problem

• Derivation for case (1)

 

2 0

( , ) 2

exp( )

4

s

i s

T x t T x

u du erf erf

T T t

( s i) k T T q s q t

(24)

Semi-infinite half space problem D i ti (1)

Derivation (1)

– Existence of similarity variable, η

– Partial differential equation with x, t  ordinary differential q y equation with η

4 x

t

– We first transform the pertinent differential operator,

1 4

T dT dT

x d x t d

2 2

2 2

1 4

T d T d T

x d x x t d

 

2 4

T dT x dT

t d t t t d

 

(25)

Semi-infinite half space problem D i ti (2)

Derivation (2)

– Substituting into 1D diffusion equation,

2T 1 T

2

T 2 T

Boundary conditions become;

x2 t

T2 2 T

 

– Boundary conditions become;

( 0) s T T (0, ) s

T t T

( , )

( 0)

T x t Ti

T x T

 

T(   ) Ti

( , 0) i

T x T Both the IC and the interior BC correspond to the single requirement

(26)

Semi-infinite half space problem D i ti (3)

Derivation (3)

– Now T is uniquely defined by η. Let’s solve T now. T(η) may be obtained by separating variables, such that

( / )

d T

– By integration,

( / )

( / ) 2 d T

T d

 

 

y g ,

I t ti d ti

2 2

1 1

ln( / ) dT exp( )

dT d C or C

d

  

– Integrating a second time,

T C1

exp(u du2) C2 where u is dummy.

0

( 0) s T T

2

2 s

C T

2 1

0

exp( ) s

T C

u du T

(27)

Semi-infinite half space problem D i ti (4)

Derivation (4)

( ) i

T    T 1 2

0

exp( )

i s

T C u du T

C1 2(Ti Ts) 2 2

( ) ( ) ( )

T t T T d T

– Note that error function is defined as;

x

2 0

( , ) ( i s) exp( ) s

T x t T T u du T

– For example,

– The final solution can be also described as;

2 0

( ) 2 exp( )

x

erf x u du

erf (0) 0, erf ( ) 1

;

 

( , ) 2 2

exp( )

4

T x t Ts x

u du erf erf

T T t

0 4

i s

T T t

(28)

Semi-infinite half space problem D i ti (5)

Derivation (5)

– Surface heat flux may be obtained by applying Fourier’s law,

( )

( )

T d erf d

q  k  k T T  

0 0

( )

s i s

x

q k k T T

x d dx

   

2 2 1

( ) exp( )

s s i 4

q  k T T

4 0

s s i

t

( s i)

s

k T T q t

 

t

(29)

Time dependent conduction i i fi it h lf bl

semi-infinite half space problem

( , )

4

s

i s

T x t T x

T T erf t

( s i)

s

k T T

q t

 

1/ 2 2

0 0

2 ( / )

( ) q t exp x q x x

T x t( , ) T    exp  erfc

4 4

T x t Ti erfc

k t k t

 

( ) 2

T x t T x hx h t x h t

2

( , )

4 exp 2

s

i s

T x t T x hx h t x h t

erf erfc

T T t k k t k

 

(30)

Time dependent conduction i i fi it h lf bl

semi-infinite half space problem

(31)

Time dependent conduction i i fi it h lf bl

semi-infinite half space problem

– For granite from Forsmark, Sweden

Sweden,

– k = 3.58 W/mK, ρ: 1000 kg/m3, cp: 796 (J/kg·K)  α = 4.5x10-6 m2/sec

m2/sec

– Homework#2 Q3. Reproduce this graph.

(32)

Time dependent conduction

ith fi d T t b th d a cases with fixed T at both ends

tT=0.1

– Thermal relaxation time: a characteristic time for heat to diffuse th h th l (Middl t d Wil k 1999) d thi k f

Middleton and Wilcock, 1999

through the layer(Middleton and Wilcock,1999). d: thickness of layer, α: diffusivity. tTd2 /

(33)

Convective heat transfer

• What will be the factors that make these two cases different?

Saturated Porous media - Fluid NOT flowing

T0=100°C TL=15°C

Saturated Porous media Fluid Flowing

T0=100°C TL=15°C

- Fluid Flowing

• These will be covered after we deal with fluid flow in rock

(34)

Summary

• Transient conduction problem

– Temperature changes with timeTemperature changes with time

• Coupled process associated with thermal transfer

– Convective heat transfer

– Thermal expansion and thermal stressp

Fl id fl i k k

• Fluid flow in rock - next week

– Porous rock – Fractured rock

(35)

References used for this lecture

• Beardsmore and Cull, 2001, Crustal Heat Flow – A guide to measurement and modelling, Cambridge Univ Press

• Somerton WH, 1992, Thermal properties and temperature- related behavior of rock/fluid systems, Elsevier

related behavior of rock/fluid systems, Elsevier

• Middleton GV and Wilcock PR, 1999, Mechanics in the Earth

d E i t l S i C b id U i P

and Environmental Sciences, Cambridge Univ Press

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