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RADIATIVE PROPERTIES OF
REAL MATERIALS• Electromagnetic Theory:
▪ ideal, optically smooth surface
▪ valid for spectral range larger than visible
• Real Materials: surface condition
▪ contaminants or oxides ▪ surface roughness ▪ thin coating on substrate
• Material Dependence
▪ opaque nonmetals ▪ opaque metals ▪ selective and directional opaque surfaces ▪ selectively transparent materials
• Parameter Dependence
▪ spectral and directional variations ▪ variation with temperature ▪ effect of surface roughness ▪ effect of surface impurities
Radiative Properties of Opaque Nonmetals
Effect of Coating Thickness
Emissivity of zinc oxide coatings on oxidized stainless steel substrate. Surface temperature, 880 ± 8 K
Effect of Substrates
Effect of substrate reflection characteristics on the hemispherical characteristics of a TiO2 paint film for normal incidence: Film thickness, 14.4 m; volume concentration of pigment 0.017,
Effect of Surface Roughness
Bidirectional total reflectivity of typewriter paper in plane of incidence. Source temperature, 1178 K
Bidirectional total reflectivity for visible light in plane of incidence for mountainous regions of lunar surface
Reflected energy at full moon
varies from 0° to 90° as the position of the incident energy varies from the center to the edge of the lunar diskuniform brightness: constant intensity reflected to earthcos consta
nt
Semiconductor
Normal spectral emissivity of a highly doped silicon semiconductor at room temperature
Radiative Properties of Metals
Effect of wavelength on directional spectral emissivity of pure titanium. Surface ground to 0.4 m rms
Directional Dependence
follow theoretical trend
EM theory doesn’t hold at shorter wavelengths.
Spectral Dependence
Variation with wavelength of normal spectral emissivity for polished metals
gray body assumption
Peak near the visible region
infrared region
1.27 m
X point: iron, 1.0 m; nickel, 1.5 m; copper, 1.7 m; platinum, 0.7 m
Effect of wavelength and surface temperature on hemispherical spectral emissivity of tungsten
H-R relation holds
Peak appears near the visible region
Variation with Temperature
Effect of temperature on hemispherical total emissivity of several metals and one dielectric
er T
Hagen – Rubens
Effect of Surface Roughness
Roughness effects for small optical roughness, 0/ < 1; effect of surface finish on directional spectral emissivity of pure titanium. Wavelength, 2 m
follow theoretical trend
approach to optically smooth surface
Precise definition of surface characteristics geometric shape, method of preparation, distribution of size around rms
0/ > 1: multiple reflection
Effects of roughness on bidirectional reflectivity in specular direction for ground nickel specimens. Mechanical roughness for polished specimen, 0.015 m
behave more like a polished surface
smoother relative to the incident radiation for large
Bidirectional reflectivity in plane of incidence for various incidence angles; material, aluminum (2024-T4), aluminum coated; rms roughness 0 = 1.3 m; wavelength of incident radiation, = 0.5 m
For large , peak r shifted to larger anglesOff-specular reflection at larger rough-ness and incident angle
/= 2.6
Effect of Surface Impurities
Effect of oxide layer on directional spectral emissivity of titanium. Emission angle, = 25°; surface lapped to 0.05 m rms; temperature, 294 K.
0.690.45
Approximate directional total absorptivity of anodized aluminum at room temperature relative to value for normal incidence
At low source temperature, incident radiation in long wavelength region
→ Barely influenced by the thin oxide layer on the anodized surface
→ Acts like a bare metal
Hemispherical spectral reflectivity for normal incident beam on aluminum coated with lead sulfide. Coating mass per unit surface area, 0.68 mg/cm2
Selective and Directional Opaque SurfacesModification of Surface Spectral
Characteristics
Characteristics of some spectrally selective surfaces
c: cutoff wavelength
c
Ex 5-1
An ideal selective surface with a cutoff wavelength c = 1 m
21353 W/miq
eq ?T
Energy balance
in out g stE E E E in outE E
inE : absorbed energy
outE : emitted energy
arriving from the sun at Ts = 5780 K
1 0 , 0 c c
4 2 162
2 22
5.67 57.8 6.95 10= 1358 W/m
1.5 10
sunearth
TS = 5780 K
ib,s d
L = 1.50 × 1011 m
R = 6.95 × 108 m
, cosc b sS i d 4 2
2 (cos 1)ST R
L
An ideal selective surface with a cutoff wavelength c = 1 m
21353 W/miqarriving from the sun at Ts = 5780 K
eq ?T
0( )cosi b sq Ci T d d
4
sC T 21353 W/m
4 4 25.67 (57.8) 63,284,000 W/msT
0( ) ( )cosb s eqCi T T d d
inE 0
( ) ( )coseq b sT Ci T d d
For diffuse irradiation
in 0( ) ( )cosb s eqE Ci T T d d
,
,
cos
cos
i i i
i i i
i d
i d
eq( )cosT d
in 0( ) ( )eq b sE C T i T d
0( ) ( )eq b sC T e T d
0
( )c
b sC e T d
4
40
( )c b ss
s
e TC T d
T
0 c si Tq F
eq eq0( ) ( )cosbi T T d d
eq eq0
1( ) ( )cosbi T T d d
eq eq0( ) ( )bT e T d
For diffuse irradiation
eq eq( ) ( )T T
out eq0( )
c
bE e T d
eq
40eq cTFT
eqe4
0q 0 c c siT TF q FT oreq
040eq
c s
c
i TTT
q FF
outE eq eq0
( ) ( )cosbT i T d d
By trial and erroreq 1334 KT
Cutoff wavelengt
h c, m
0.6
0.8
1.0
1.2
1.5
∞
Equilibrium temperatur
e Teq, K
1811
1523
1334
1210
1041
393
Ex 5-3,n
Wavelength
approximation
SiO-Al selective surface
21353 W/miq
Solar energy absorberat TA = 393 K1. extracted energy for use in a
power- generating cycle
?pq
2. for the black surface at the same
temperature
pq
0.95
0.051.5
in out g stE E E E
Energy balance
in , aE qout peE q q
p a eqq q
aq 0 00.95 0.05 1c s c si T Tq F F
21139 W/m
eq 40 00.95 0.05 1
c A c AA T TT F F
267.63 W/m
21139 68 1071 W/mpq
For black surface
(79% of )iq
4 21353 W/me A iq T q
No energy available
,n
Wavelength
approximation
SiO-Al selective surface
0.95
0.051.5
Reflectivity of white paint coating on aluminum
reflect well at short wavelengths
radiate well at long wavelengths
Selective Transmission
Normal overall spectral transmittance of glass plate (includes surface reflection) at 298 K
c c
ordinary glasses: typically two strong cutoff wavelengths
A transmitting Layer with Thickness L >
Reflectance
2 22 2
2 2 2 2
111 1 1
1 1
Transmittance
22 2 2 4 4
2 2
11 1
1T
1-
(1-)
(1-)2
(1-)
(1-)2
(1-)22
2(1-)2
(1-)3
2 (1-)23
3 (1-)3
3 (1-)4
3 (1-)24
(1-)(1-) (1-)(1-)
(1-)2(1-)
3 (1-)3(1-)
4 (1-)4
2 2 2 2 4 41 1 1R
2 2 3 3 1 11 1 1
1A
spectral transmittance 2
2 2
1
1T
2
2 20
1
1G d
G
,trG T G
total transmittance
Absorptance
1-
(1-)(1-)
(1-)
(1-)2
(1-)
(1-)(1-)
(1-)2
(1-)22
2(1-)2
(1-)2(1-)
(1-)3
2 (1-)23
3 (1-)3
3 (1-)3(1-)
3 (1-)4
3 (1-)24
4 (1-)4
,tr ,G
G
0T G d
G
,tr0
0
G dT
G d
R + T + A =1
Effect of plate thickness on normal overall spectral transmittance of soda-lime glass (includes surface reflection) at 298 K
Transmittance depends on thickness.95% of solar energy can be trapped.
Transmittance and reflectance of 0.35-m-thick film of Sn-doped In2O3 film on Corning 7059 glass. Also shown is the effect on T of an antireflection coating of MgF2
Selectively transparent coating may also be useful in the collection of solar energy.