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Transcript of RADIATION HEAT TRANSFER - Vysoké učení technické v...
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RADIATION HEAT TRANSFER
Heat conduction and convection - always a fluid which transfers the heat (gas, liquid, solid) – motion of atoms or moleculesHeat conduction and convection is not possible in a vacuumIn most practical applications all three modes occur concurrently at varying degrees
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A hot object in a vacuumchamber looses heat byradiation only
Unlike conduction and convection, heattransfer by radiation can occur between two bodies, even when they are separated by a medium colder than both of them
convection
radiation
What will be a final equilibrium temperature of the body surface? Can you write an energy balance equation between the body and surrounding air and the hot source (fire)?
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Theoretical foundation of radiation was establishedby MaxwellElectromagnetic wave motion or electromagnetic radiationElectromagnetic waves travel at the speed of light c in a vacuumElectromagnetic waves are characterized by their frequency for wavelength λ: λ=c/fc=co/n co light speed in a vacuum
n refraction index of a medium (n=1 for air and most gases, n=1,5 for glass, 1,33 for water)
In all material medium, there is attenuation of the energyIn a vacuum there is no attenuation of the energy
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Electromagnetic radiation covers a wide range of wavelengths
Radiation that is related toheat transfer –Thermal radiationλ from 0,1μm to 100 μmAs a result of energy transition in molecules, atoms and electrons.
Thermal radiation is emitted by all matter whose temperature is above absolute zero.
Everything around us emits (and absorbs) radiation.
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• Thermal radiation includes entire visible (0,4 to 0,76 μm)and infrared light and a portion of ultraviolet radiation.
• Bodies start emit visible radiation at 800K (red hot) and tungsten wire in the lightbulb at 2000K (white hot) to emit a significant amount of radiation in the visible range.
• Bodies at room temperature emit radiation in infrared range 0,7 to 100 μm.
• Sun (primary light source) emits solar radiation –0,3 to 3 μm – almost half is visible, remaining is ultraviolet and infrared.
• Body that emits radiation in the visible range is called light source.
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Spectral and Directional Distribution
Radiation characteristics varywith wavelength and direction
• Monochromatic or spectral: Characteristics at a given λ• Total: Integrated values over all wavelengths• Directional: At a given direction
• Diffuse radiation: Uniform in all directions • Hemispherical: Integrated values over all directions
The assumption of diffuse radiation will be made throughout
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Emissive Power E, Irradiation G and Radiosity J
• Emissive Power (zářivost):Radiation emitted from a surface
• Spectral emissive power λE :
λEper unit area per unit wavelength,
= rate of emitted radiationmW/m2μ
• Total emissive power E:,E = Integration of λE over all values of λ 2W/m :
( ) ( )∫∞
=
0, λλλ dTETE
∫∞
=0
λλdEE
λ
λE
10.1 Fig.
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• Irradiation: Radiation energy incident on a surface• Spectral irradiation λG :
λGper unit area per unit wavelength,
= rate of radiation energy incident upon a surfacemμW/m2−
• Total irradiationG:G = integration of λG over all values of λ :
( ) ( )∫∞
=
0 , λλλ dTGTG
• Radiosity: The sum of emitted and reflected radiation • Spectral radiosity λJ :
λJ = rate of radiation leaving a surface per unit area perunit wavelength, mμW/m2−
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In the above definitions, summation in all directions isimplied although the term hemispherical is not used
• Total radiosity J:
( ) ( )∫∞
=
0 , λλλ dTJTJ
J = integration of λJ over all values of λ :
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Characteristics of blackbody:(1) It absorbs all radiation incident upon it(2) It emits the maximum energy at a given temperature
and wavelength(3) Its emission is diffuse
Planck's Law λbE = spectral emissive power of a blackbody:
( )1)/exp(
,2
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−=
−
TCCTEb λλλλ C1 and C2 are constants
Blackbody Radiation
Blackbody: An ideal radiation surface used as standard for describing radiation of real surfaces
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Planck's Law
Blackbody Radiation
2879,6Tλmax =
Maximum emitted energy atspecific temperatures given byWien law:
Note - by qualitative judgment -energy emitted in visible range for 2000 K – tungsten wire ina light bulb.
Thermal radiation 0,1 to 100 μm
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Stefan-Boltzmann LawBased on: • Experimental data by Stefan (1879)• Theoretical derivation by Boltzmann (1884)
4TEb σ=
bE = total blackbody emissive power (all wavelengths and all directions), [W/m2]
428- KW/m105.67 −×=σ is the Stefan-Boltzmannconstant
It can also be arrived at using Planck's law
Stefan-Boltzmann law
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( ) ( )
4
0 2
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0 bλb
Tσ
dλ1)T/λC(exp
λC
dxλ,TETE
=
∫ =−
=
=∫=
∞ −
∞
• Stefan-Boltzmann law gives the total radiation emitted froma black body at all wavelengths from λ=0 to λ=∞.
• Often an interest in radiation over some wavelength band –light bulb – how much is emitted in the visible range?
• We use a procedure to determine Eb,0-λ
∫=−
λ
0bλλb,0 T)dλ(E(T)E ,λ
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Define a dimensionless quantity fλ(T):
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λ0 b,λ
λ σT(T)dλE
(T)f ∫=
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Want to know how energy is emitted in the visible range 0,40 to 0,76 μm.
λ1T=0,40.2500=1000 ⇒ fλ1 = 0,000321
λ2T=0, 76.2500=1900 ⇒ fλ2 = 0,053035
fλ2 - fλ1 = 0,0527
Only about 5% of radiation is emittedin the visible range. The remaining95% is in the infrared region in theform of heat.
Light bulb.
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Radiation of Real Surfaces
Objective: Develop a methodology for determining radiation heat exchange between real surfaces.
• Surface radiation properties
• The graybody
• Kirchhoff's law
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Absorptivity a, Reflectivity r, Transmissivity t
Gα
Gτ
GρG E
J
10.2 Fig.
rG
tG
Irradiation incident on a real surface can be absorbed, reflected and transmitted.
Remind: radiosity J (total radiation leavingthe surface) is a sum of emitted E and reflected rG radiation.
a = total absorptivity = fraction absorbedr = total reflectivity = fraction reflected t = total transmissivity = fraction transmitted
GGtrGaG =++
1=++ tra
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Similarly
1=++ λλλ tra
aλ = spectral absorptivityrλ = spectral reflectivitytλ = spectral transmissivity
Opaque material: 0== λtt
Simplification: 1=+ ra
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Emissivity (emisivita, poměrná zářivost)
Total emissivity ε(T):Ratio of emissive power of a surface to that of a blackbody at the same temperature:
( ) ( )TETET
b
)(=ε
Spectral emissivity λε :Ratio of the spectral emissive power of a surface to that of a blackbody at the same temperature:
( ) ( )( )TE
TETb ,
,,λλλε
λ
λλ =
λ
λE
10.3 Fig.
blackbodysurface real
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Kirchhoff's Law
It is much easier to determine emissivity ε than absorptivity a.By experiments. But how we can determine absorptivity?
Kirchhoff’s law says that under certain conditions:
( ) ( )TT αε =Total ( ) ( )TT ,, λαλε λλ =Spectral
Kirchhoff’s law is used to determine aλ(λ,T) from experimentaldata on ελ(λ,T)
Equality of emissivity and absorptivityQuite different physical quantitiesJust numerical equality
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Graybody ApproximationThe graybody concept is introduced to simplify the analysis of radiation exchange between bodies
Graybody: An ideal surface for which thespectral emissivity ελ is independent of λ
λ
λE
10.3 Fig.
blackbodysurface realgray body
λ
λE
10.3 Fig.
blackbody
body gray
approx. 0,75 Eb
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Thus: == )(),( TT ελελ constant independent of λ
It follows from Kirchhoff's Law that
( ) ( ) graybodya forTT αε =
NOTE:(1) Radiation properties ε, a and r are assigned single
values instead of a spectrum of values(2) Data on ε give r and a for opaque surface.
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Radiation Exchange Between Black Surfaces
Two black surfaces withareas 1S and 2S attemperatures 1T and 2T
Objective: Determine the netheat transfer 21Q −& between the two surfaces
21 TT >
1T2T
1S
2S
1E2E
12Q&
1
2
Important factors:• Configuration• Surface area• Surface temperature • Radiation properties (for gray body) • Surrounding surfaces • Space medium
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The View Factor(1) Definition and use:
• It is a geometric factor
• Also known as shape factor and configuration factor
The view factor is the fraction of radiation energyleaving surface S1 which is intercepted by S2
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1Q& = rate of radiation energy leaving surface 1, = S1E1
2Q& = rate of radiation energy leaving surface 2, = S2E2
21Q −& = net radiation energy exchanged between 1 and 221−F = fraction of radiation energy leaving 1 and
reaching 2
12−F = fraction of radiation energy leaving 2 and reaching 1
1T2T
1S
2S
1E2E
21Q −&
1
2
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For black surfaces:
The net energy exchanged between the surfaces 1 and 2:
21-2212-112-1 bb EFSEFSQ −=& (a)
Radiation that leaves the surface 1: 111 bESQ =&
1121 bESF −and is intercepted by the surface 2:
222 bESQ =&Radiation that leaves the surface 2:
2212 bESF −and is intercepted by the surface 1:
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If 21 TT = then 21 bb EE = and 12Q& = 0.
( ) ( )44212-11212-112-1 TTFSEEFSQ bb −=−= σ&
122211 −− = FSFS (b)
Combine (a) and (b) and use Stefan-Boltzmann law :4TEb σ=
Reciprocal rule (vztah recoprocity)
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(2) Rules: • Reciprocal rule can be generalized
ijjjii FSFS −− =
• Additive rule: Conservation of energy - see the figure.
( ) 3-12-132-1 FFF +=+
Multiply by 1S
3-112-113)21 FSFSFS +=+−(1
Use the reciprocal rule
1-331-221-3)+(232 )( FSFSFSS +=+
10.5 Fig.
1
23
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• Enclosure or summation rule: All energy leaving one surface must be received by some or all other surfaces
1 1131211 =++++ nFFFF K
niFn
jji ,,3,2,1 1=
1=K=∑
• Conclusion: iiF = 0 for a plane or convex surface and
iiF ≠ 0 for a concave surface
(3) Determination of view factors:
• Simple configurations: By physical reasoning:
n
4
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1
6.10 Fig.
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21A 2A
1
112 =F
Apply the reciprocal rule
211122 −− = FSFS
21212112 /)/( SSFSSF == −−
• Other methods:• Surface integration method: Can involve tedious
double integrals• View factor algebra method: Known factors are used
in a superposition scheme together with the three view factor rules to construct factors for other configurations
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View factor for parallel rectangles
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View factor for perpendicular rectangleswith a common side