R DI TIVE TR NSFER BETWEEN TWO OR MORE SURF CES Prepared by Nurhaslina bt che radzi FKK, UITM
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 1/18
R DI TIVE TR NSFER
BETWEEN TWO OR MORE
SURF CES
Prepared byNurhaslina bt che radzi
FKK, UITM
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 2/18
• This chapter focus on radiative exchange between two or moresurfaces.
• This exchange depends strongly on the surface geometries andorientations as well as on their radiative properties andtemperatures.
• To compute radiation exchange between any two surfaces, theconcept of a view factor must first introduce.
RADIATIVE TRANSFER BETWEEN TWO ORMORE SURFACES
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 3/18
VIEW FACTOR RELATIONS
• The view factor Fij is defined as the fraction of the radiation leaving surface i that isintercepted by surface j
• For radiation exchange between two surfaces of areas Ai and Aj, the view factors arerelated by reciprocity relation :
A iFij = A jF ji
• An example might be the floor and ceiling of a room
the view factor, F12 :
F12 = fraction of energy
leaving A 1 reaching A 2 A 1F12 = A 2F21
• For an enclosure consisting of N surfaces, the view factor are related by summationrule :
∑ Fij = 1
• For all radiant leaving the inner surface (1) must reach the outer surface (2), the viewfactor are related by inspection:
F12 = 1
• For several common geometries, view factors may be determined using Table 13.1 and
13.2 and Figure 13.4 through 13.6.
N
j = 1
A 1
A 2
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 4/18
• Consider a simple, two surfaces enclosure involving the sphericalsurfaces
• To calculate radiation exchange in an enclosure of N surface a total
of N2 view factors is needed
N2 = 22 = 4 view factors
F11 , F12 , F21 , F22
• From figure, since all radiation leaving the inner surface (1) mustreach the outer surface (2), by inspection:
F12 = 1 or by summation rule
* concave surface, it see itself Fii ≠ 0
* convex/plane surface
Fii = 0
F11 + F12 = 1 F11 = 0
F12 = 1
A 1
A 2
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 5/18
• From the reciprocity relation,
A 1F12 = A 2F21
F21 = A 1 F12
A 2
F21 = A 1
A 2
• From the summation rule,F21 + F22 = 1
F22 = 1 – F21
= 1 – F21
= 1 – A 1/A 2
• Additive rule for view factor relation
Fij = ∑ Fik A jF(j)I = ∑ A k Fki A j = ∑ A k n
k = 1
n
k = 1
n
k = 1
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 6/18
Example - PROBLEM 13.1Determine F12 and F21 for the following configurations using thereciprocity theorem and other basic shape factor relations. Do not usetable or charts
a) Long duct (L)
b) Small sphere of area A 1 under a concentric hemisphere of area A 2 = 2A 1
c) Long duct. What is F22 for this case?
d) Long inclined plates (point B is directly above the center of A 1)
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 7/18
e) Sphere lying on infinite plane
f) Hemisphere – disk arrangement
g) Long open channel (L)
h) Long concentric cylinders (L)
A 1
A 2
D1
D2
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 8/18
Radiation Exchange Between Opaque, Diffuse,Gray Surfaces in an Enclosure
• Analyzing radiation exchange in an enclosure is assumed to beisothermal and to be characterized by a uniform radiosity and auniform irradiation
Net radiation Exchange at a Surface
• The term qi , which is the net rate at which radiation leaves surface i,represents the net effect of radiative interactions occuring at the
surface
• The net radiation may be expressed as
qi
= A i
(Ji
– Gi
) (1)
Ji A i Gi A i
qi
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 9/18
Ji = Radiosity
= Ei + ρiGi
• The net radiation may also be expressed as
qi = A i(Ei – αiGi) (2)
Ei = Emissive power
Gi = Absorbed irradiation
For an opaque surface , αi = 1 - ρi , αi = absorptivity
ρi = 1 - αi εi = emmisivity
= 1 - εi ρi = reflectivity
Ji = εiE bi + (1 – εi)Gi qi = A i Ji – Ji – εiE bi
1 - εi
qi = E bi- Ji , E bi – Ji = driving potential (3)
(1 – εi)/ εi A i (1 – εi) = surface radiative resistance
εi A i
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 10/18
for black surface , εi = 1
* (1 - εi ) = 0
εi A i
* Ji = E bi blackbody radiation exchange
Radiation Exchange Between Surfaces
• To determine surface radiosity, Ji , it is necessary to considerradiation exchange between the surfaces of the enclosure
• From reciprocity relation :
A iGi = ∑ A iFijJ j
qi = A i (Ji - ∑FijJ j) (4)
• From the summation rule,
qi = A i (∑Fij Ji - ∑FijJ j)
qi = ∑ A i Fij (J j – J j) = ∑qij (5)
J j – J j = driving potential
(A i Fij )-1 = space/geometrical resistance
N
j = 1 N
j = 1
N
j = 1
N
j = 1N
j = 1
N
j = 1
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 11/18
• Combining equations (3) and (5)
E bi – Ji = ∑ Ji – J j
(1 – ξ i)/ ξ i A i (A iFij)-1
qi = ∑ Ji – J j
(A iFij)-1
Blackbody Radiation Exchange
• Equation (5) reduces to
qi = ∑ A iFij σ (Ti4 – T j
4)
• When all surfaces of the enclosure are black, there is no reflectionand radiosity is composed solely of the emitted energy
N
j = 1
N
j = 1
N
j = 1
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 12/18
BLACKBODY RADIATION EXCHANGE
• Consider radiation exchange between two black surfaces of arbitraryshape
• Defining qi j as the rate at which radiation leaves surfaces i and isintercepted by surface j
qi j = (A i Ji)Fij
for black surface , Ji = E bi
qi j = A iFij E bi
q j i = A jF ji E bj
A i , Ti A j , T j
ni n j
Ji = E bi
J j = E bj
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 13/18
• The net radiative exchange between the two surface is
qij = qi j - q j i
= A iFij E bi - A jF ji E bj
from Stefan – Boltzman Law : E b = σT4 and
from Reciprocity Relation : A iFij = A jF ji
The net rate at which radiation leaves surface i and intercepted bysurface j may be defined as
qij = A iFij σ (Ti4 – T j
4)
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 14/18
RPOBLEM 13.7
Consider the right-circular cylinder of diameter D, length L andthe areas A 1 , A 2 and A 3 representing the base, inner and topsurfaces
a) Show that the view factor form F12= 2H[(1 + H2)1/2 – H] , where
H = L/D
b) Show that the view factor for the inner surface to itself has theform F22 = 1 + H – (1 + H2)1/2
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 15/18
PROBLEM 13.8
Consider the parallel rectangles shown schematically. Show that the view factor F12 can be expressed as
F12 = 1 [A (14) F(14)(23) - A 1F13 - A 4F42]
2A i
where all view factors on the right-hand side of the eqn. Can beevaluated from Figure 13.4 (see Table 13.2) for aligned parallelrectangles.
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 16/18
PROBLEM 13.10
The reciprocity relation, the summation rule and Equations 13.5to 13.7 can be used to develop view factor relations that allow forapplications of Figure 13.4 and/or Figure 13.6 to more complexconfigurations. Consider the view factor F14 for surfaces 1 and 4 ofthe following geometry. These surfaces are perpendicular but do
not share a common edge.
a) Obtain the following expression for the view factor F14 :
F14 = 1 [(A 1+A 2)F(12)(34) + A 2F23 – (A 1+A 2)F(12)3 – A 2F(2)(34)]
b) If L1 = L2 =L4 = w/2 and L3 = w , what is the value of F14
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 17/18
PROBLEM 13.11
Determine the shape factor, F12 for the rectangles shown
a) Perpendicular rectangles without a common edge
b) Parallel rectangles of unequal areas
13
2 4
6m
6m
6m3m
(x)
(z)
(y)
Figure 13.6
8/10/2019 Chapter 13 Heat Transfer
http://slidepdf.com/reader/full/chapter-13-heat-transfer 18/18
PROBLEM 13.30
Two plane coaxial disks are separated by a distance L = 0.20m. The
lower disks (A 1) is solid with a diameter Do = 0.80m and a temp. T1 = 300K. The upper disk (A 2) at temp. T2 = 1000K has the same outerdiameter but is ring shaped withan inner diameter Di = 0.40m.
Assuming the disks to be blackbody, calculate the net radiative heatexchange between them.