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