320 RADIATIVE HEAT TRANSFER
11.29 An optical device to determine NOxcontent in the combustion products powering a gas turbine measures the
transmissivity of NO for its 5.3 µm band. The device consists of a blackbody source (Tbb =2000 K), two ports,
a filter/detector combination (with flat response 1750 cm−1< η < 2000 cm−1, and zero response elsewhere),
and a chopper (such that the detector registers radiation from the blackbody source, but not the emission from
the combustion gases). Two measurements are taken: one with an inert gas in the turbine (signal S0), and
another with combustion gases present (assume T1=1600 K =const, p1=5 bar =const, light path through
gas L=1 m; signal S).
(a) Show that the measured transmissivity, τ, is
τ≡S
S0
=1−ω
∆ηA∗(T1,p1,L,xNO),∆η=250cm−1,
assuming that the Planck function is constant across ∆η.
(b) If the transmissivity is measured as τ=0.7, what is the NO volumetric concentration, xNO?
(Note: for NO at 1600 K β∗/β∗
0=0.827).
0=0.1805,
ω0=20.0cm−1,n=0.65,b=1.0
0(β∗/β∗
0)Pe=0.1805 ×0.827 ×2.847 =0.4249
Thus
A∗=250
80 (1 −0.7) =0.9375 <1/β =⇒probably square root–regime
τ0=α
ωρNOL=α
ω
p1MNO
RuTL xNO
ω
RuT1
8.314 ×1600J/mol