Convective Heat Transfer

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Transcript Convective Heat Transfer

HEAT TRANSFER Final Review

Heat Transfer # 1 Su Yongkang School of Mechanical Engineering

Final Review Session

Heat Transfer # 2 Su Yongkang School of Mechanical Engineering

Viscous Flow

•

The Navier-Stokes Equations

Nonlinear, second order, partial differential equations.

   

u

t

u

u

x

v

u

y

w

u

z

    

p

x

 

g x

     2

u

x

2   2

u

y

2   2

u

z

2      

v

t

u

v

x

v

v

y

w

v

z

    

p

y

 

g y

     2

v

x

2   2

v

y

2   2

v

z

2      

w

t

u

w

x

v

w

y

w

w

z

    

p

z

 

g z

     2

w

x

2   2

w

y

2   2

w

z

2   

u

x

 

v

y

 

w

z

 0 •

Couette Flow, Poiseuille Flow.

Heat Transfer # 3 Su Yongkang School of Mechanical Engineering

Convection

• Basic heat transfer equation

q

h A s

(

T s

T

 )

h

 average heat transfer coefficient • Primary issue is in getting convective heat transfer coefficient,

h h

 1

A s

A s h dA s

or, for unit width :

h

 1

L

L

0

h dx

•

h

relates to the conduction into the fluid at the wall

h x

 -

k f

T s

T

y

y T

   0 Heat Transfer # 4 Su Yongkang School of Mechanical Engineering

Convection Heat Transfer Correlations

• Key is to fully understand the type of problem and then make sure you apply the appropriate convective heat transfer coefficient correlation

External Flow

For laminar flow over flat plate

T

 ,

U

 y

dP

 0

dx

T

s

Nu x

h x k x

 0.332

Re 1 2 x Pr 1 3

N u x

h x k x

 0.664

Re 1 2 x Pr 1 3 For mixed laminar and turbulent flow over flat plate

h x

 1

L

 

xc

h lam

0

dx

 

L xc h turb dx

 

Nu L

  0.6

0.037

Re  Pr  60 4 L 5  10 5  Re

L

Eq.

7.41

5   10 8 871  Pr 1  Re 3 x, c  5  10 5  Heat Transfer # 5 Su Yongkang School of Mechanical Engineering

External Convection Flow

For flow over cylinder

Overall Average Nusselt number Nu D

h k D

C

Re

m D

Pr 1 3   Pr Pr

s

  1 4

Table 7.2 has constants C and m as f(Re)

For flow over sphere

Nu D

h k D

 2  (0.4

Re 1

D

2  0.06

Re 2

D

3 ) Pr 0 .

4    

s

  1 4

For falling liquid drop

Nu D

 2  0.6

Re 1

D

2 Pr 1 3 Heat Transfer # 6 Su Yongkang School of Mechanical Engineering

Convection with Internal Flow

• Main difference is the constrained boundary layer   r o • Different entry length for laminar and turbulent flow • Compare external and internal flow: –

External flow :

Reference temperature:

T

 is constant –

Internal flow :

Reference temperature:

T m

transfer is occurring!

will change if heat • •

T m

increases if heating occurs (

T s > T m

)

T m

decreases if cooling occurs (

T s < T m

) Heat Transfer # 7 Su Yongkang School of Mechanical Engineering

Internal Flow (Cont’d)

T •

For constant heat flux:

T s

(

x

)

T m

(

x

) •

T m

,

x

q

conv

c p

 x 

T in

,

thermal

x

x fd

For constant wall temperature

T if T s  T i T

T s

if T s  T i

T m T m T s

x • Sections 8.4 and 8.5 contain correlation equations for Nusselt number

q conv

A s h

T LM

Heat Transfer x # 8 Su Yongkang School of Mechanical Engineering

Free (Natural) Convection

•

Unstable, Bulk fluid motion Stable, No fluid motion

Grashof number

in natural convection is analogous to the Reynolds number in forced convection

Gr L

g

 

T s

  2

T

 

L

3  Buoyancy forces Viscous forces

Gr L

Re 2

L

 1

Natural convection can be neglected

Gr L

Re 2

L

 1

Natural convection dominates

Heat Transfer # 9 Su Yongkang School of Mechanical Engineering

Free (Natural) Convection

Rayleigh number :

For relative magnitude of buoyancy and viscous forces

Ra x

Gr x

 Pr For vertical surface, transition to turbulence at

Ra x

 10 9 • Review the basic equations for different potential cases, such as vertical plates, vertical cylinders, horizontal plates (heated and cooled) • For horizontal plates, discuss the equations 9.30 9.32. (P513) • Please refer to problem 9.34.

Heat Transfer # 10 Su Yongkang School of Mechanical Engineering

T A

,

out

Heat Exchangers

T B

,

in

(shell side)

Example: Shell and Tube:

T B

,

out

•

Cross-counter Flow

Two basic methods discussed:

1. LMTD Method

T A

,

in

(tube side)

2.

q

UA

T out

ln  

T in

 

T o T i

UA

T LMTD

-NTU Method

q

 

q

max

or q

 : 

C

min 

T h

,

i

T c

,

i

 NTU 

UA overall

,

HX C

min 

where

:

q

 max 

q q

max

C

min 

T h

,

i

T c

,

i

  

f

NTU

,

C r

 C r 

C C

min max  C r  1  Heat Transfer # 11 Su Yongkang School of Mechanical Engineering

Discussion on the U

Notice!

• Equation 11.5

Example 11.1

1

UA

  1

U i A i

1

h i A i

 

U o R f

 ,

i

1 

A i A o

ln(

D o

/ 2 

kL D i

) 

R f

 ,

o A o

 1

h o A o

• For the unfinned, concentric, tubular heat exchangers.

• When the inner tube surface area is the reference calculating area.

1

U i

 1

h i

R f

 ,

i

 ln(

D o

/ 2 

kL D i

)

A i

R f

 ,

o A i A o

A i h o A o

• When the inner tube surface area is the reference calculating area.

1

U o

 1

h o

R f

 ,

o

 ln(

D o

/ 2 

kL D i

)

A o

R f

 ,

i A o A i

A o h i A i

Heat Transfer # 12 Su Yongkang School of Mechanical Engineering

Discussion on the problems

Heat Transfer # 13 Su Yongkang School of Mechanical Engineering