ANALYSIS: Consider first the furnace wall (A). Since the wall material is diffuse and gray, it follows that
εA=εf=αA=0.85.
The emissive power is
EA=εAEb(Tf)=εAσTf=0.85×5.67×10−8 W/m2⋅K4(3000 K)4=3.904×106 W/m2.
Since the furnace is an isothermal enclosure, blackbody conditions exist such that
GA=JA=Eb(Tf)=σTf4=5.67×10−8 W/m2⋅K4(3000 K)4=4.593×106 W/m2.
Considering now the semitransparent, diffuse, spectrally selective object at To = 300 K. From the radiation balance requirement, find
αλ=1−ρλ−τλ or α1=1−0.6−0.3=0.1 and α2=1−0.7−0.0=0.3
αB=∫0∞αλGλdλ/G=F0−λT⋅α1+(1−F0−λT)⋅α2=0.970×0.1+(1−0.970)×0.3=0.106
where F0–λT = 0.970 at λT = 5 μm × 3000 K = 15,000 μm·K since G=Eb(Tf). Since the object is diffuse, ελ=αλ, hence
εB=∫0∞ελEλ,b(To)dλ/Eb,o=F0−λTα1+(1−F0−λT)⋅α2=0.0138×0.1+(1−0.0138)×0.3=0.297
where F0–λT = 0.0138 at λT = 5 μm × 300 K = 1500 μmK. The emissive power is
EB=εBEb,B(To)=0.297×5.67×10−8 W/m2⋅K4(300 K)4=136.5 W/m2.
The irradiation is that due to the large furnace for which blackbody conditions exist,
GB=GA=σTf4=4.593×106 W/m2.
The radiosity leaving point B is due to emission and reflected irradiation,
JB=EB+ρBGB=136.5 W/m2+0.3×4.593×106 W/m2=1.378×106 W/m2.
If we include transmitted irradiation, JB=EB+(ρB+τB)GB=EB+(1 – αB)GB=4.106×106 W/m².
In the first calculation, note how we set ρB≈ρλ(λ<5 μm).