12
Heat and mass transfer Fins Yashawantha K M, Dept. of Marine Engineering, SIT, Mangaluru Page 1 FINNED SURFACES Introduction: Convection: Heat transfer between a solid surface and a moving fluid is governed by the Newton’s cooling law: where Ts is the surface temperature and T is the fluid temperature. Therefore, to increase the convective heat transfer, one can Increase the temperature difference between the surface and the fluid. Increase the convection coefficient h. This can be accomplished by increasing the fluid flow over the surface since h is a function of the flow velocity and the higher the velocity, the higher the h. Example: a cooling fan. Increase the contact surface area A. Example: a heat sink with fins. Many times, when the first option is not in our control and the second option (i.e. increasing h) is already stretched to its limit, we are left with the only alternative of increasing the effective surface area by using fins or extended surfaces. Fins are protrusions from the base surface into the cooling fluid, so that the extra surface of the protrusions is also in contact with the fluid. Most of you have encountered cooling fins on air-cooled engines (motorcycles, portable generators, etc.), electronic equipment (CPUs), automobile radiators, air conditioning equipment (condensers) and elsewhere. Temperature distribution and Heat transfer in fins (rectangular or circular) 4 Governing differential equation: Let us take small element dx on a rectangular fin with uniform cross sectional area A ) ( T s T ) ( = T s T hA Q conv Q dx x Q x Q + + = dx dT A k x Q = dx dx T d A k dx dT A k dx dx dT A k dx d dx dT A k dx x Q 2 2 = + = +

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Page 1: Fins

Heat and mass transfer Fins

Yashawantha K M, Dept. of Marine Engineering, SIT, Mangaluru Page 1

FINNED SURFACES

Introduction:

Convection: Heat transfer between a solid surface and a moving fluid is governed by the

Newton’s cooling law: where Ts is the surface temperature and T� is the

fluid temperature. Therefore, to increase the convective heat transfer, one can

• Increase the temperature difference between the surface and the fluid.

• Increase the convection coefficient h. This can be accomplished by increasing the fluid

flow over the surface since h is a function of the flow velocity and the higher the velocity,

the higher the h. Example: a cooling fan.

• Increase the contact surface area A. Example: a heat sink with fins.

Many times, when the first option is not in our control and the second option (i.e. increasing h) is

already stretched to its limit, we are left with the only alternative of increasing the effective

surface area by using fins or extended surfaces. Fins are protrusions from the base surface into

the cooling fluid, so that the extra surface of the protrusions is also in contact with the fluid.

Most of you have encountered cooling fins on air-cooled engines (motorcycles, portable

generators, etc.), electronic equipment (CPUs), automobile radiators, air conditioning equipment

(condensers) and elsewhere.

Temperature distribution and Heat transfer in fins (rectangular or circular)

4

Governing differential equation:

Let us take small element dx on a rectangular fin with uniform cross sectional area A

)(∞

−TsT

)(∞

−= TsThAQ

convQ

dxxQ

xQ +

+=

dx

dTAk

xQ −= dx

dx

TdAk

dx

dTAkdx

dx

dTAk

dx

d

dx

dTAk

dxxQ

2

2

−−=

−+−=+

Page 2: Fins

Heat and mass transfer Fins

Yashawantha K M, Dept. of Marine Engineering, SIT, Mangaluru Page 2

This equation is called, one dimensional fin equation for fins of uniform cross section(second

order, linear, ordinary equation)

The solution is,

Where C1 and C2 are constants

C1 and C2 are constant are determined by the application of the two boundary condition, one

specified for the fin tip.

x= 0 at T=Tb and the other boundary condition there are several possibities

1. Infinitely long fin

2. Fin insulated at its end (i. negligible heat loss from the end of the fin)

3. Fin loosing heat from its end by convection

4. Fin with specified temperature at its end

convQ

dxxQ

xQ +

+=

( )∞

−+−−=− TTdxPhdxdx

TdAk

dx

dTAk

dx

dTAk )(

2

2

( )∞

−= TTsAh

convQ ( )

∞−= TTdxPh

convQ )( dxpermeterAs )(=

( )∞

−= TTdxPhdxdx

TdAk )(

2

2

( )∞

−= TTKA

Ph

dx

Td2

2

( )∞

−= TTmdx

Td 22

2

KA

Phm =

KA

Phm =2

0)(2)(2

2

=− xmdx

xdθ

θ ∞−= TTxlet )(θ

dx

dT

dx

xd=

)(θ

mxmx eCeCx 21)( += −θ

mxCmxCx sinhcosh)( 21 +=θ

Page 3: Fins

Heat and mass transfer Fins

Yashawantha K M, Dept. of Marine Engineering, SIT, Mangaluru Page 3

Infinitely long fin

Assuming that fin tip is insulated

Boundary conditions,

Heat transfer rate

(Refer HMTDB Page No-50)

∞= T

LT

0)(2)(2

2

=− tmdx

tdθ

θ

mxmx eCeCt 21)( += −θ

bTTatx == 0

∞==∞= T

LTTatx

∞−= TTb bθ

0=L

θ

1Cb=θ

bTTatx == 0 ∞−= TT

b bθ

∞==∞= T

LTTatx 0=

∞= 20 C 02 =C

mxeb

x −= θθ )(

mxe

b

x −=θθ )(

mxeT

bT

TT−=

∞−∞

0

)(

0 =−=

=−=

xdx

xdAk

xdx

dTAkQ

θ

)( bmAkQ θ−−=

mxe

b

x −=θθ )(

mx

b ex −=θθ )(

mx

b emdx

xd −−= θθ )(bmAkQ θ=

)( ∞−= TTKA

hPAkQ b

)( ∞−= TThPKAQ b

Page 4: Fins

Heat and mass transfer Fins

Yashawantha K M, Dept. of Marine Engineering, SIT, Mangaluru Page 4

Fin of finite length with insulated tip (short fin with end insulated)

Boundary conditions,

bTTatx == 0 ∞−= TT

b bθ

0==dx

datLx

θ

( )∞

−= TTmdx

Td 22

2

KA

Phm =

KA

Phm =2

0)(2)(2

2

=− xmdx

xdθ

θ ∞−= TTxlet )(θ

dx

dT

dx

xd=

)(θ

mxCmxCx sinhcosh)( 21 +=θ

bTTatx == 0 ∞−= TT

b bθ

1Cb=θ

( ) ( )mxmCmxmbdx

tdcoshsinh

)(2+= θ

θ

( ) ( )mLmCmLmb

sinhcosh0 2+= θ

( )( )mL

mLbCcosh

sinh

2

θ−=

( )( )

mxmL

mLbmx

bt sinh

cosh

sinhcosh)(

−+=

θθθ

( )( )

mxmL

mLmx

b

tsinh

cosh

sinhcosh

)(

−=

θθ

( ) ( )( )mL

mxmLmLmx

b

t

cosh

sinhsinhcoshcosh)( −=

θθ

( )( )mL

xLm

b

t

cosh

cosh)( −=

θθ

( )( )mL

xLm

TbT

TT

cosh

cosh −=

∞−∞

Page 5: Fins

Heat and mass transfer Fins

Yashawantha K M, Dept. of Marine Engineering, SIT, Mangaluru Page 5

(Refer HMTDB Page No 50)

Heat transfer rate

(Refer HMTDB Page No 50)

Heat transfer can also be find out by,

(Refer the method of last derivation)

( )( )mL

xLm

TbT

TT

cosh

cosh −=

∞−∞

0

)(

0 =−=

=−=

xdx

xdAk

xdx

dTAkQ

θ

( )( )[ ]

0

sinhcosh

=

−−−=

x

xLmmmL

bAkQθ

( )( )mL

xLm

b

x

cosh

cosh)( −=

θθ

( )( )

−=

mL

xLmx b

cosh

cosh)( θθ

( )( )[ ] )10(sinh

cosh

)(−−= xLmm

mL

b

dx

xd θθ

( )( )[ ]xLmm

mL

b

dx

xd−−= sinh

cosh

)( θθ( )mL

mL

bAmkQ sinhcosh

θ=

( ) mLTbTAmkQ tanh∞−=

( ) mLTbThPKAQ tanh∞−=

∫ ∞−=L

o

TxTdxPhQ ))(()(

Page 6: Fins

Heat and mass transfer Fins

Yashawantha K M, Dept. of Marine Engineering, SIT, Mangaluru Page 6

Fins with convection at the tip

Boundary conditions

Solution for the second order differential equation

0)(22

)(2=− xm

dx

xdθ

θ

0)( θθ =

∞−= T

bTx 0=xat

0)()(

=+ xLh

dx

xdk θ

θLxat =

)(sin2

)(cos1

)( xmhCxmhCx +=θ

)(sin2

)(cos1

)( xmhCxmhCx +=θ0

)( θθ =∞

−= TbTx 0=xat

010+=Cθ

)(sin2

)(cos0

)( xmhCxmhx +=θθ

0)()(

=+ xLh

dx

xdk θ

θ Lxat =

)(cos2

)(sin0

)(xmhmCxmhm

dx

xd+=θ

θ

LxxA

Lh

Lxdx

xdkA

==

=− )(

)(θ

θ

[ ] [ ] 0)(sin)(cos)(cos)(sin 2020 =+++ LmhCLmhLhlmhmCLmhmk θθ

0)()(

=+ xLh

dx

xdk θ

θLxat =

[ ] [ ] 0)(sin)(cos)(cos)(sin 2020 =+++ LmhChLmhhLmhmCkLmhmk LLθθ

[ ] [ ] 0)(sin)(cos)(cos)(sin 2200 =+++ LmhChLmhmCkLmhhLmhmk LLθθ

+−=

+ )(sin)(cos)(cos)(sin 20 Lmh

km

Lh

LmhCLmhkm

Lh

Lmhθ

10C=θ

Page 7: Fins

Heat and mass transfer Fins

Yashawantha K M, Dept. of Marine Engineering, SIT, Mangaluru Page 7

)(sin)(cos

)(cos)(sin0

2

Lmhkm

Lh

Lmh

Lmhkm

Lh

Lmh

C

+

+

−=

θ

)(sin

)(sin)(cos

)(cos)(sin

)(cos0

)( 0 xmh

Lmhkm

Lh

Lmh

Lmhkm

Lh

Lmh

xmhx

+

+

−= θθθ

)(sin

)(sin)(cos

)(cos)(sin

)(cos

0

)(xmh

Lmhkm

Lh

Lmh

Lmhkm

Lh

Lmh

xmhx

+

+

−=θθ

)(sin)(cos

)(sin)(cos)(sin)(sin)(cos)(cos

0

)(

Lmhkm

Lh

Lmh

xmhLmhkm

Lh

LmhLmhkm

Lh

Lmhxmhx

+

+−

+

=θθ

)(sin)(cos

)(sin)(cos)(sin)(sin)(cos)(sin)(cos)(cos

0

)(

Lmhkm

Lh

Lmh

xmhLmhkm

Lh

xmhLmhxmhLmhkm

Lh

Lmhxmhx

+

+−

+

=θθ

[ ]

)(sin)(cos

)(sin)(cos)(cos)(sin)(sin)(sin)(cos)(cos

0

)(

Lmhkm

Lh

mLh

xmhLmhkm

Lh

xmhLmhkm

Lh

xmhLmhxmhLmhx

+

−+−

=θθ

[ ] [ ]

)(sin)(cos

)(sin)(cos)(

0

)(

Lmhkm

Lh

mLh

xLmhkm

Lh

xLmh

TbT

TxTx

+

−+−

=∞−∞−

=θθ

Page 8: Fins

Heat and mass transfer Fins

Yashawantha K M, Dept. of Marine Engineering, SIT, Mangaluru Page 8

Heat transfer rate

Dividing )(cos Lmh in the equation

(HMTDB Page No 50)

0

)(

0 =−=

=−=

xdx

xdAk

xdx

dTAkQ

θ

[ ] [ ]

+

−+−

=

)(sin)(cos

)(sin)(cos

)( 0

mLhkm

Lh

Lmh

xLmhkm

Lh

xLmh

x θθ

[ ] [ ]

)(sin)(cos

)1)((cosh)1)((sin)(

0

Lmhkm

hLmh

xLmmkm

hxLmhm

dx

xd

L

L

+

−−+−−= θ

θ

( )

+

+

∞−=

)(tan1

)(tan

Lmhkm

h

km

hmLh

TbTAk

LPhQ

L

L

[ ] [ ]

0

)(sin)(cos

)1)((cosh)1)((sin

0

=+

−−+−−−=

x

Lmhkm

Lh

Lmh

xLmmkm

Lh

xLmhm

AkQ θ

[ ] [ ]

)(sin)(cos

)(cosh)(sin

0

Lmhkm

hLmh

mLmkm

hmLhm

AkQL

L

+

−−−= θ

+

+

=

)(sin)(cos

)(cosh)(sin

0

Lmhkm

hLmh

Lmkm

hmLh

AmkQL

L

θ

( )

+

+

∞−=

)(sin)(cos

)(cosh)(sin

Lmhkm

hLmh

Lmkm

hmLh

TbTAk

LPhQ

L

L

Page 9: Fins

Heat and mass transfer Fins

Yashawantha K M, Dept. of Marine Engineering, SIT, Mangaluru Page 9

Fin of finite length with specified temperature at its end

Temperature distribution

Boundary conditions

0)(22

)(2=− xm

dx

xdθ

θ

0== xatbTT

LxatLTT ==

∞−= T

bT

∞−= T

LT

)(sin2

)(cos1

)( xmhCxmhCx +=θ

)(sin2

)(cos1

)( xmhCxmhCx +=θ

0== xatbTT

∞−= T

bT

1C

b=θ

)(sin2

)(cos1

)( xmhCxmhCx +=θ

LxatLTT ==

∞−= T

LT

)(sin2

)(cos mLhCLmhbL

+=θθ

)(sin

)(cos

2 mLh

LmhbLCθθ −

=

)(sin)(sin

)(cos)(cos)( xmh

mLh

LmhbLxmh

bx

−+=

θθθθ

[ ])(sin

(sin)(cos)(sin)(cos)(

mLh

xmhLmhbL

mLhxmhbx

θθθθ

−+=

)(sin

)(sin)(cos)(sin)(sin)(cos)(

mLh

xmhLmhb

xmhL

mLhxmhbx

θθθθ

−+=

Page 10: Fins

Heat and mass transfer Fins

Yashawantha K M, Dept. of Marine Engineering, SIT, Mangaluru Page 10

Heat transfer

(HMTDB Page No 50)

Fin efficiency

The fin efficiency is defined as the ratio of the energy transferred through a real fin to

that transferred through an ideal fin. An ideal fin is thought to be one made of a perfect or

infinite conductor material. A perfect conductor has an infinite thermal conductivity so that the

entire fin is at the base material temperature.

For long fin

(HMTDB Page No 50)

)(sin

)(sin)(sin)(

mLh

xmhL

xLmhbx

θθθ

+−=

∫ ∞−=

L

o

TxTdxPhQ ))(()(

dxxL

o

PhQ )(θ∫=

dxmLh

xmhL

xLmhb

L

o

PhQ

+−∫=

)(sin

)(sin)(sin θθ

Lom

xmhL

m

xLmhb

mLh

PhQ

+

−−= )

)(cos))(cos

)(sin

θθ

[ ])1)(cos()cos1()(sin

−+−−= LmhL

mLhbmLhm

PhQ θθ

[ ])1)(cos()1(cos)(sin

−+−= LmhL

mLhbmLhm

PhQ θθ

[ ])1(cos)()(sin

−+= mLhLbmLhm

PhQ θθ

PkAhmLh

mLh

LT

LTT

bTQ

)(sin

)1(cos)()(

∞−+

∞−=

∞−= T

bT

∞−= T

LT

idealQ

realQ

=η)(

)(

∞−

∞−

=T

bTLPh

TbThPkA

mL

1=

kA

hPm =

Page 11: Fins

Heat and mass transfer Fins

Yashawantha K M, Dept. of Marine Engineering, SIT, Mangaluru Page 11

For Short fin (tip is insulated)

(HMTDB Page No 50)

Fin Effectiveness

How effective a fin can enhance heat transfer is characterized by the fin effectiveness

which is as the ratio of fin heat transfer and the heat transfer without the fin. For an adiabatic fin:

for long fin

For Short fin (tip is insulated)

idealQ

realQ

=η)(

)tanh()(

∞−∞

−=

TbTLPh

mLTbThPkA

mL

mL)tanh(=

)(f

ε

finwithoutQ

finwithQ

f=ε

)(

)(

∞−

∞−

=T

bTAh

TbThPkA

hA

Pk=

)(

)tanh()(

∞−∞

−=

TbTAh

mLTbThPkA

)tanh(mLhA

Pk==

finwithoutQ

finwithQ

f=ε

kA

hPm =

kA

hPm =

Page 12: Fins

Heat and mass transfer Fins

Yashawantha K M, Dept. of Marine Engineering, SIT, Mangaluru Page 12

REFERENCES

1. Heat transfer-A basic approach, Ozisik, Tata McGraw Hill, 2002

2. Heat transfer , J P Holman, Tata McGraw Hill, 2002, 9th edition

3. Principles of heat transfer, Kreith Thomas Learning, 2001

4. Heat and Mass Transfer Data Book, C.P Kothandarman , S Subramanyan, new age

international publishers ,2010, 7th edition

5. Fundamental of Heat and Mass transfer, M Thirumaleshwar,Pearson,2013

6. Pradeep Dutta, “HEAT AND MASS TRANSFER”, Web based course material under the

NPTEL, Phase 1, 2006.