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23-Chem-B1 Transport Phenomena · May 2015

Question 5 of 6: C1 — Lead dissolution along a pipe section

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format: National Exams, May 2015 — 04-CHEM-B1 Transport Phenomena; 3 hours, open book. Six problems in three sections (A Fluid Mechanics, B Heat Transfer, C Mass Transfer), each worth 25 marks; candidates attempt one problem from each section plus a fourth from any section (four of six marked). The worked solutions below cover all six problems. A summary of the conservation equations (continuity, Navier–Stokes, energy, species) is supplied as Appendix A in the paper and is used throughout.

Reference texts: R. B. Bird, W. E. Stewart & E. N. Lightfoot, Transport Phenomena (2nd ed., Wiley) — the equations of change and the differential momentum / energy / species balances used across every problem; J. R. Welty, C. E. Wicks, R. E. Wilson & G. L. Rorrer, Fundamentals of Momentum, Heat and Mass Transfer (Wiley) — pipe-friction and boundary-layer mass-transfer correlations; F. P. Incropera & D. P. DeWitt, Fundamentals of Heat and Mass Transfer (Wiley) — conduction with variable conductivity, exchanger analysis; D. Q. Kern, Process Heat Transfer (McGraw-Hill) — the Kern casing-side method and the LMTD–correction-factor chart for multiple casing passes; R. H. Perry & D. W. Green, Perry’s Chemical Engineers’ Handbook (9th ed.) — physical properties and the Moody chart.

Question 5: C1 — Lead dissolution along a pipe section (25 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given. Laminar internal flow, thin concentration boundary layer ($\delta_c\ll R$) so the curved lead wall is treated locally as a flat plate with $x$ measured from the start of the lead section; wall (saturation) concentration $C_{As}=S$; background $C_{A0}\approx0$ (lead-free inlet, dissolved lead stays dilute in the core); supplied correlation $Sh=0.332\,Re_x^{1/2}Sc^{1/3}$ with $Re_x=v_{max}x/\nu$. For fully developed laminar (Poiseuille) pipe flow the maximum (centre-line) velocity is twice the mean: $v_{max}=2Q/\pi R^2$.

Find. (a) $N_A(x)$; (b) total dissolution rate $W$; (c) mean outlet concentration $C_{out}$; (d) the factor by which $C_{out}$ changes from 25 °C to 100 °C.

lead section (length L, C=S at wall) δc(x) Q, inlet C=0 x=0 x=L
Fig. C1: A lead-lined section dissolves into laminar water flow. The concentration boundary layer grows from the leading edge of the section, so the local flux is highest at $x=0$ and decays as $x^{-1/2}$.

Approach. Convert the flat-plate Sherwood correlation into a local $k_c(x)$, multiply by the driving force $S$ for the local flux, integrate over the wetted lead area for the total rate, divide by $Q$ for the mean outlet concentration, and finally collect the temperature-dependent properties for part (d).

  1. (a) Local flux. From $Sh=k_c x/D_{AB}=0.332\,Re_x^{1/2}Sc^{1/3}$, $$k_c(x)=0.332\,\frac{D_{AB}}{x}\left(\frac{v_{max}x}{\nu}\right)^{1/2}\!\left(\frac{\nu}{D_{AB}}\right)^{1/3}=0.332\,D_{AB}^{2/3}\,v_{max}^{1/2}\,\nu^{-1/6}\,x^{-1/2}.$$ With $C_{As}=S$, $C_{A0}=0$ and $v_{max}=2Q/\pi R^2$, $$\boxed{\;N_A(x)=0.332\,S\,D_{AB}^{2/3}\,\nu^{-1/6}\left(\frac{2Q}{\pi R^2}\right)^{1/2}x^{-1/2}\;}\qquad(\propto x^{-1/2}).$$
  2. (b) Total dissolution rate. Integrate the flux over the wetted lead surface $dA=2\pi R\,dx$, using $\int_0^L x^{-1/2}dx=2\sqrt L$: $$W=\int_0^L N_A(x)\,2\pi R\,dx=2\pi R(0.332)S\,D_{AB}^{2/3}v_{max}^{1/2}\nu^{-1/6}\,(2\sqrt L)=1.328\,\pi R\sqrt L\,S\,D_{AB}^{2/3}\,v_{max}^{1/2}\,\nu^{-1/6}.$$ Since $\pi R\,v_{max}^{1/2}=\pi R\sqrt{2Q/\pi R^2}=\sqrt{2\pi Q}$, the radius drops out: $$\boxed{\;W=1.328\,\sqrt{2\pi QL}\;S\,D_{AB}^{2/3}\,\nu^{-1/6}\;}$$
  3. (c) Mean outlet concentration. All dissolved lead leaves in the volumetric flow $Q$ (inlet lead-free), so the mixing-cup outlet concentration is $$\boxed{\;C_{out}=\frac{W}{Q}=1.328\,\sqrt{\frac{2\pi L}{Q}}\;S\,D_{AB}^{2/3}\,\nu^{-1/6}\;}$$ Had the mean velocity $Q/\pi R^2$ been used in $Re_x$ instead of $v_{max}$, the results of (a)–(c) would each be smaller by a factor $\sqrt2$; the temperature ratio in (d) is unaffected either way.
  4. (d) Effect of temperature. Only $S$, $D_{AB}$ and $\nu$ change; the geometry and flow $Q$ are fixed, so $C_{out}\propto S\,D_{AB}^{2/3}\,\nu^{-1/6}$. Using Stokes–Einstein $D_{AB}\propto T/\mu$ (absolute $T$) and $\nu=\mu/\rho\propto\mu$ (water density nearly constant), $$\frac{C_{out,100}}{C_{out,25}}=\frac{S_{100}}{S_{25}}\left(\frac{T_{100}}{T_{25}}\frac{\mu_{25}}{\mu_{100}}\right)^{2/3}\!\left(\frac{\mu_{25}}{\mu_{100}}\right)^{1/6}.$$ With $S_{100}/S_{25}=2$, $T_{100}/T_{25}=373/298=1.25$, $\mu_{25}/\mu_{100}=9/2.7=3.33$: $$\frac{C_{out,100}}{C_{out,25}}=2\,(4.17)^{2/3}(3.33)^{1/6}=\boxed{6.3}$$ The outlet lead concentration rises about six-fold (≈ +530 %) on going from 25 °C to 100 °C.
PartResult
(a) Local flux$N_A(x)=0.332\,S\,D_{AB}^{2/3}\nu^{-1/6}(2Q/\pi R^2)^{1/2}x^{-1/2}$
(b) Total rate$W=1.328\sqrt{2\pi QL}\,S\,D_{AB}^{2/3}\nu^{-1/6}$
(c) Outlet conc.$C_{out}=1.328\sqrt{2\pi L/Q}\,S\,D_{AB}^{2/3}\nu^{-1/6}$
(d) 25→100 °C factor$\approx 6.3\times$ (about +530 %)