23-Chem-B1 Transport Phenomena · May 2018
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Paper format. EGBC 16-CHEM-B1 Transport Phenomena, May 2018, 3 hours, open-book (one textbook permitted, no loose notes). 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, and only the first four in the answer book are marked. All six problems are solved below as a complete study resource. Appendix A of the paper supplies the equations of change (continuity, Navier–Stokes, energy and species-continuity tables) in rectangular, cylindrical and spherical coordinates; these are quoted rather than re-derived.
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; J. R. Welty, C. E. Wicks, R. E. Wilson & G. L. Rorrer, Fundamentals of Momentum, Heat and Mass Transfer (Wiley) — pipe friction, tank draining, the internal-flow and wetted-wall correlations; F. P. Incropera & D. P. DeWitt, Fundamentals of Heat and Mass Transfer (Wiley) — the Sieder–Tate laminar-tube correlation and cylindrical conduction; C. J. Geankoplis, Transport Processes and Separation Process Principles (Prentice Hall) — the Gilliland–Sherwood wetted-wall correlation and diffusion with heterogeneous reaction; R. H. Perry & D. W. Green, Perry’s Chemical Engineers’ Handbook — transport properties.
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. A long hollow cylinder (a pipe wall), length $L$, inner radius $r_i$ at $T_i$, outer radius $r_o$ at $T_o$, both ends insulated (no axial conduction) with rotational symmetry (no $\theta$-dependence); constant $k$, $\rho$, $c_p$; no heat generation.
Find. (a) the governing unsteady conduction equation; (b) the steady radial temperature profile $T(r)$; (c) the steady radial heat flow $q$.
Approach. This is a derivation: reduce the cylindrical energy equation to the radial direction for part (a); set the time derivative to zero and integrate twice with the two surface temperatures for part (b); then apply Fourier’s law over the cylindrical area for part (c).
Starting from the energy equation in cylindrical coordinates (Appendix Table A.3) with no bulk motion ($\vec u=0$), no generation, and $T=T(r,t)$ only (insulated ends kill $\partial/\partial z$; symmetry kills $\partial/\partial\theta$), every $\theta$- and $z$-term drops and $$\boxed{\rho c_p\frac{\partial T}{\partial t}=\frac{1}{r}\frac{\partial}{\partial r}\!\left(k\,r\frac{\partial T}{\partial r}\right)\quad\Longleftrightarrow\quad \frac{\partial T}{\partial t}=\frac{\alpha}{r}\frac{\partial}{\partial r}\!\left(r\frac{\partial T}{\partial r}\right),}$$ with thermal diffusivity $\alpha=k/\rho c_p$. This is the transient radial-conduction (Fourier) equation for the cylinder.
At steady state $\partial T/\partial t=0$, so the right-hand side must vanish: $\dfrac{d}{dr}\!\left(r\dfrac{dT}{dr}\right)=0$. Integrating once, $r\dfrac{dT}{dr}=C_1$, i.e. $\dfrac{dT}{dr}=\dfrac{C_1}{r}$; integrating again, $$T(r)=C_1\ln r+C_2.$$ Applying the surface temperatures $T(r_i)=T_i$ and $T(r_o)=T_o$ gives $C_1=\dfrac{T_o-T_i}{\ln(r_o/r_i)}$ and $C_2=T_i-C_1\ln r_i$. Substituting, the profile is logarithmic: $$\boxed{\frac{T(r)-T_i}{T_o-T_i}=\frac{\ln(r/r_i)}{\ln(r_o/r_i)}.}$$
Fourier’s law over the cylindrical conduction area $A(r)=2\pi rL$, using $dT/dr=C_1/r$: $$q=-k\,A\,\frac{dT}{dr}=-k(2\pi rL)\frac{C_1}{r}=-2\pi kL\,C_1.$$ The $r$ cancels — $q$ is the same through every radius, as steady conservation demands. With $C_1=(T_o-T_i)/\ln(r_o/r_i)$, $$\boxed{q=\frac{2\pi kL\,(T_i-T_o)}{\ln(r_o/r_i)}.}$$
| Part | Result |
|---|---|
| (a) Unsteady equation | $\rho c_p\,\partial_t T=\dfrac{1}{r}\partial_r(k\,r\,\partial_r T)$ |
| (b) Steady profile | $\dfrac{T-T_i}{T_o-T_i}=\dfrac{\ln(r/r_i)}{\ln(r_o/r_i)}$ |
| (c) Steady heat flow | $q=\dfrac{2\pi kL(T_i-T_o)}{\ln(r_o/r_i)}$ |