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Workshop 9: Diffusion with surface reaction

Attempt these problems before opening the worked solutions.

A cylindrical graphite (pure carbon) rod (length = 25 cm, initial diameter = 2 cm) is placed in a combustion chamber with flowing air stream at 1100 K and 2 atm total pressure. A stagnant gas boundary layer 5 mm thick is formed around the surface of the rod. At 1100 K, solid carbon oxidises to carbon dioxide gas,

C (s)+O2 (g)→CO2 (g)\mathrm{C\ (s) + O_2\ (g) \rightarrow CO_2\ (g)}

Assuming that the oxidation is limited by molecular diffusion of O2\mathrm{O_2} through the stagnant gas film, and outside of the gas film, the bulk composition of air stream prevails,

a) Estimate the initial rate of CO2\mathrm{CO_2} production from the rod;

b) Write an equation for the rate of change in the radius of the rod as a function of time.

Data: Density of solid graphite = 2.25 g/cm3\mathrm{g/cm^3}; DABD_{AB} (CO2\mathrm{CO_2}-air) @ 273 K and 1 atm = 0.136 cm2/s\mathrm{cm^2/s}

Worked solution
Radial diffusion through a gas film around the graphite rod. The radius a decreases during oxidation, while the film thickness remains fixed. The drawing is a cylindrical cross-section; oxygen diffuses inward and carbon dioxide outward.
Figure 1: Radial diffusion through a gas film around the graphite rod. The radius a decreases during oxidation, while the film thickness remains fixed. The drawing is a cylindrical cross-section; oxygen diffuses inward and carbon dioxide outward.

Data

QuantitySymbolValue
Initial radius and rod lengtha0,ℓa_0,\ell0.010,0.25 m0.010,0.25\ \mathrm m
Gas-film thicknessδ\delta0.0050 m0.0050\ \mathrm m
Gas temperature and pressureT,PT,P1100 K,2 atm1100\ \mathrm K,2\ \mathrm{atm}
PropertyValue
Graphite density ρC\rho_C2250 kg m−32250\,\mathrm{kg\,m^{-3}}
Carbon molar mass MCM_C0.012 kg mol−10.012\,\mathrm{kg\,mol^{-1}}
Carbon-dioxide molar mass MCO2M_{CO_2}0.044 kg mol−10.044\,\mathrm{kg\,mol^{-1}}
Bulk oxygen mole fraction yby_b0.21
Reference effective gas diffusivity D0D_00.136 cm2 s−10.136\,\mathrm{cm^2\,s^{-1}} at 273 K and 1 atm

Assumptions

Treat the source’s CO2-air diffusivity as a common effective diffusivity for the oxygen and carbon-dioxide counterdiffusion. This is an approximation to multicomponent air. Nitrogen has zero net flux, and the reaction exchanges one gas mole for one gas mole, so total gas molar flux is zero. Estimate the diffusivity by

D=D01 atmP(T273 K)3/2.D=D_0\frac{1\,\mathrm{atm}}{P}\left(\frac{T}{273\,\mathrm K}\right)^{3/2}.

Assume isothermal quasi-steady radial diffusion, no gas-phase reaction, constant density and length, and no transport through the ends. The maintained bulk gas has yO2(a+δ)=yby_{O_2}(a+\delta)=y_b, while the fast reaction gives yO2(a)=0y_{O_2}(a)=0. Keep δ\delta fixed as aa decreases. Derive the constant rNO2rN_{O_2} from a cylindrical shell balance, integrate Eq. 1, and relate oxygen consumption to the changing carbon mass. Do not use the initial area as a constant area for the shrinking rod.

Calculations

Use molar flux NAN_A in mol m−2 s−1\mathrm{mol\,m^{-2}\,s^{-1}} and ideal-gas concentration c=P/(RT)c=P/(RT), with R=8.314 Pa m3 mol−1 K−1R=8.314\,\mathrm{Pa\,m^3\,mol^{-1}\,K^{-1}}. With negligible total molar flux, diffusion obeys

NA=−cDdyAds.N_A=-cD\frac{dy_A}{ds}.(1)

The coordinate ss increases away from the reacting surface. Reactant flux is therefore negative. Report removal and production rates as positive magnitudes.

The oxygen consumption balances carbon-dioxide production mole for mole at the rod surface.

A steady cylindrical shell balance gives

d(rNO2)dr=0.\frac{d(rN_{O_2})}{dr}=0.

The positive oxygen consumption rate qq satisfies q=−2πrℓNO2q=-2\pi r\ell N_{O_2}.

Integrating Eq. 1 between aa and a+δa+\delta gives

q(a)=2πℓcDybln⁡(a+δa).q(a)=\frac{2\pi\ell cD y_b}{\ln\left(\frac{a+\delta}{a}\right)}.(2)

Convert D0=1.36×10−5 m2 s−1D_0=1.36\times10^{-5}\,\mathrm{m^2\,s^{-1}}.

The scaled D=5.49989×10−5 m2 s−1D=5.49989\times10^{-5}\,\mathrm{m^2\,s^{-1}} and c=22.1587 mol m−3c=22.1587\,\mathrm{mol\,m^{-3}}.

At a0a_0,

ln⁡(a0+δa0)=ln⁡(1.5)=0.405465.\ln\left(\frac{a_0+\delta}{a_0}\right)=\ln(1.5)=0.405465.

Using Eq. 2, substitute the length and cylindrical logarithmic factor:

q(a0)=2π(0.25)(22.1587)(5.49989×10−5)(0.21)0.405465q(a_0)=\frac{2\pi(0.25)(22.1587)(5.49989\times10^{-5})(0.21)}{0.405465}

Evaluating this expression gives

q(a0)=9.91479×10−4 mol s−1,q(a_0)=9.91479\times10^{-4}\,\mathrm{mol\,s^{-1}},m˙CO2(0)=MCO2q(a0)=4.36251×10−5 kg s−1.\dot m_{CO_2}(0)=M_{CO_2}q(a_0) =4.36251\times10^{-5}\,\mathrm{kg\,s^{-1}}.

The carbon mass is mC=ρCπa2ℓm_C=\rho_C\pi a^2\ell.

Its balance is

2πρCaℓdadt=−MCq(a).2\pi\rho_C a\ell\frac{da}{dt}=-M_Cq(a).

Combining this balance with Eq. 2 yields

dadt=−MCcDybρCaln⁡(a+δa),a(0)=a0.\frac{da}{dt}=-\frac{M_C cD y_b}{\rho_C a\ln\left(\frac{a+\delta}{a}\right)}, \qquad a(0)=a_0.(3)

Initially

dadt=−3.36637×10−7 m s−1.\frac{da}{dt}=-3.36637\times10^{-7}\,\mathrm{m\,s^{-1}}.

The negative sign represents loss of radius.

Carbon consumption uses MCM_C; carbon-dioxide mass production uses MCO2M_{CO_2}.

The gas-film diffusion time δ2/D=0.455 s\delta^2/D=0.455\,\mathrm s is much shorter than the initial shrinkage scale

a0∣dadt∣=2.97×104 s,\frac{a_0}{\left|\frac{da}{dt}\right|}=2.97\times10^4\,\mathrm s,

supporting quasi-steady transport initially.

The model excludes combustion heating, carbon-monoxide formation, end effects and changes in the flow as the rod shrinks.

Answer

The initial carbon-dioxide production rate is 9.91×10−4 mol s−19.91\times10^{-4}\ \mathrm{mol\,s^{-1}}, or 4.36×10−5 kg s−14.36\times10^{-5}\ \mathrm{kg\,s^{-1}}. Radius evolves according to Eq. 3, starting from a0=0.010 ma_0=0.010\ \mathrm m; initially

dadt=−3.37×10−7 m s−1.\frac{da}{dt}=-3.37\times10^{-7}\ \mathrm{m\,s^{-1}}.

Film resistance and finite surface reaction

Section titled “Film resistance and finite surface reaction”

Nitric oxide (NO) emission from automobile exhaust can be reduced by using a catalytic converter. The following reaction occurs at the catalytic surface:

NO+CO→0.5 N2+CO2\mathrm{NO + CO \rightarrow 0.5\ N_2 + CO_2}

The concentration of NO is reduced by passing the exhaust gases over the surface of the catalyst, and the rate of reduction at the catalyst surface is as follows:

NNO=−k′′CNO(0),N_{NO}=-k'' C_{NO(0)},

where CNO(0)C_{NO(0)} is the concentration of NO at the catalyst surface.

As a first approximation, it may be assumed that NO reaches the surface by one-dimensional diffusion through a thin gas film of thickness L that adjoins the surface, and that the effects of bulk motion is negligible. Determine the mole fraction of NO at the catalytic surface and the NO removal rate for a catalytic surface area of 200 cm2\mathrm{cm^2}.

Data: The exhaust gas is at 500 ∘C500\,{}^\circ\mathrm{C} and 1.2 bar, the mole fraction of NO at L is 0.15, DABD_{AB} = 10−410^{-4} m2/s\mathrm{m^2/s}, k′′k'' = 0.05 m/s and the film thickness is L = 1 mm.

Worked solution
Nitric oxide diffuses through a nonreacting gas film to the catalyst. Its surface concentration is not zero when surface reaction is finite. The solution measures x from the catalyst toward the bulk.
Figure 2: Nitric oxide diffuses through a nonreacting gas film to the catalyst. Its surface concentration is not zero when surface reaction is finite. The solution measures x from the catalyst toward the bulk.

Data

PropertyValue
Bulk NO mole fraction yby_b0.15
Film thickness LL0.0010 m0.0010\,\mathrm m
Effective NO diffusivity DD1.0×10−4 m2 s−11.0\times10^{-4}\,\mathrm{m^2\,s^{-1}}
Surface rate constant ksk_s0.050 m s−10.050\,\mathrm{m\,s^{-1}}
Catalytic area AsA_s200 cm2200\,\mathrm{cm^2}
NO molar mass MNOM_{NO}0.030 kg mol−10.030\,\mathrm{kg\,mol^{-1}}

Assumptions

Assume steady isothermal one-dimensional diffusion with constant pressure and DD, no gas-phase reaction, sufficient CO, and the source’s first approximation of negligible bulk-motion contribution to NO transport. The reaction changes total gas mole number, so this approximation is not exact equimolar diffusion. Do not interpret the 0.15 mole fraction as realistic dilute exhaust data. It is the supplied idealised problem value. At the surface,

NNO(0)=−kscys,ys=yNO(0),N_{NO}(0)=-k_s c y_s, \qquad y_s=y_{NO}(0),

and yNO(L)=yby_{NO}(L)=y_b. Integrate Eq. 1 in xx and equate the film flux to the surface reaction flux.

Calculations

The finite catalytic reaction leaves a nonzero nitric-oxide concentration at the surface.

The steady flux is constant and the profile is linear:

yNO(x)=ys+(yb−ys)xL,y_{NO}(x)=y_s+(y_b-y_s)\frac{x}{L},NNO=−cDL(yb−ys).N_{NO}=-\frac{cD}{L}(y_b-y_s).

Matching the reaction flux gives

DL(yb−ys)=ksys,ys=yb1+ksLD=0.151+0.50=0.100.\begin{aligned} \frac{D}{L}(y_b-y_s)&=k_s y_s,\\ y_s&=\frac{y_b}{1+\frac{k_sL}{D}}\\ &=\frac{0.15}{1+0.50}=0.100. \end{aligned}(4)

Convert T=773.15 KT=773.15\,\mathrm K, P=120000 PaP=120000\,\mathrm{Pa} and As=0.0200 m2A_s=0.0200\,\mathrm{m^2}.

Then c=18.6684 mol m−3c=18.6684\,\mathrm{mol\,m^{-3}} and NNO=−0.0933421 mol m−2 s−1N_{NO}=-0.0933421\,\mathrm{mol\,m^{-2}\,s^{-1}}.

The positive removal rate is

n˙NO=−AsNNO=1.86684×10−3 mol s−1,\dot n_{NO}=-A_sN_{NO} =1.86684\times10^{-3}\,\mathrm{mol\,s^{-1}},m˙NO=MNOn˙NO=5.60052×10−5 kg s−1.\dot m_{NO}=M_{NO}\dot n_{NO} =5.60052\times10^{-5}\,\mathrm{kg\,s^{-1}}.

The equivalent concentration-based coefficient is

koverall=(LD+1ks)−1.k_{overall}=\left(\frac{L}{D}+\frac{1}{k_s}\right)^{-1}.

Its value is 0.0333333 m s−10.0333333\,\mathrm{m\,s^{-1}}.

The film resistance L/D=10 s m−1L/D=10\,\mathrm{s\,m^{-1}} and reaction resistance 1/ks=20 s m−11/k_s=20\,\mathrm{s\,m^{-1}} add.

Reaction supplies twice the film resistance, but neither can be ignored.

The calculated surface fraction in Eq. 4 confirms finite reaction, rather than a perfectly absorbing surface.

These results apply only to the stated film approximation.

Answer

The surface NO mole fraction is 0.1000.100. The positive removal rate is 1.87×10−3 mol s−11.87\times10^{-3}\ \mathrm{mol\,s^{-1}}, equivalent to 5.60×10−5 kg s−15.60\times10^{-5}\ \mathrm{kg\,s^{-1}}, within the stipulated film approximation.