Question 1 of 6: A1 — Combined pressure–drag flow in an annulus
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format: National Exams, December 2014 — 04-CHEM-B1 Transport Phenomena; 3 hours, open book. Six problems in three sections (A Fluid Mechanics, B Heat Transfer, C Mass Transfer); candidates attempt one from each section plus a fourth from any section (four of six marked, 25 marks each). The worked solutions below cover all six problems. A summary of the conservation equations (continuity, Navier–Stokes, energy, species) is provided as Appendix A in the paper and is quoted throughout rather than re-derived.
Reference texts: R. S. Brodkey & H. C. Hershey, Transport Phenomena — A Unified Approach (McGraw-Hill) — the paper’s own reference and source of the appended conservation-equation tables; R. B. Bird, W. E. Stewart & E. N. Lightfoot, Transport Phenomena (2nd ed., Wiley) — 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) — annular flow, variable-conductivity conduction and diffusion; F. P. Incropera & D. P. DeWitt, Fundamentals of Heat and Mass Transfer (Wiley) — internal-flow convection ($Nu=3.66$) and transient conduction/diffusion; C. J. Geankoplis, Transport Processes and Separation Process Principles (Prentice Hall) — Stefan-tube / evaporating-drop mass transfer.
Question 1: A1 — Combined pressure–drag flow in an annulus
Given. A Newtonian fluid (constant $\rho$, $\mu$) fills the annular gap between an inner rod of radius $R_1$ moving axially at velocity $V$ and a stationary outer tube of inner radius $R_2$. Flow is horizontal, fully developed, steady and laminar, driven by both the moving rod (drag) and a constant axial pressure gradient $dP/dz$.
Find. (a) the axial velocity profile $u(r)$ for the moving rod; (b) the profile when $V=0$ (rod stationary).
Fig. A1: Longitudinal section of the extruder annulus. The stationary outer tube ($R_2$) and the axially moving rod ($R_1$, velocity $V$) bound a Newtonian film that is simultaneously dragged by the rod and pushed by the pressure gradient $dP/dz$.
Approach. With unidirectional fully developed flow $u=u_z(r)$ only, the cylindrical $z$-momentum equation collapses to an ordinary differential equation; integrate twice and fix the two constants with no-slip on the moving rod and the stationary tube.
Reduce the equation of motion. For steady, fully developed axial flow $u_z=u(r)$, $u_r=u_\theta=0$, the Navier–Stokes $z$-component (Appendix A, Table A.2f) loses every inertial and $\theta,z$ term, leaving a balance of pressure and viscous stress: $$\mu\,\frac{1}{r}\frac{d}{dr}\!\left(r\frac{du}{dr}\right)=\frac{dP}{dz}.$$
Integrate twice. Writing $\beta=\dfrac{1}{\mu}\dfrac{dP}{dz}$ (a constant), $\dfrac{d}{dr}\!\left(r\dfrac{du}{dr}\right)=\beta r$, so $r\dfrac{du}{dr}=\dfrac{\beta r^2}{2}+C_1$ and hence $$u(r)=\frac{\beta r^2}{4}+C_1\ln r+C_2 .$$
Recast about the outer wall. Absorbing $C_2$ so that the constant vanishes at $r=R_2$: $$u(r)=\frac{\beta}{4}\left(r^2-R_2^2\right)+C_1\ln\!\frac{r}{R_2},$$ which already satisfies $u(R_2)=0$.
Apply no-slip on the rod. Setting $u(R_1)=V$ gives $\dfrac{\beta}{4}(R_1^2-R_2^2)+C_1\ln\dfrac{R_1}{R_2}=V$, so $$C_1=\frac{V+\dfrac{\beta}{4}\left(R_2^2-R_1^2\right)}{\ln\!\dfrac{R_1}{R_2}} .$$
Assemble the profile (part a). With $\beta=(1/\mu)\,dP/dz$, $$\boxed{\,u(r)=\frac{1}{4\mu}\frac{dP}{dz}\left(r^2-R_2^2\right)+C_1\ln\!\frac{r}{R_2}\,},\qquad C_1=\frac{V+\dfrac{1}{4\mu}\dfrac{dP}{dz}\left(R_2^2-R_1^2\right)}{\ln\!\dfrac{R_1}{R_2}}.$$ The first term is the pressure-driven (Poiseuille) contribution; the logarithmic term carries the drag of the moving rod plus the annular curvature.
Stationary rod (part b). Put $V=0$: the drag term disappears and only pressure flow remains, $$u(r)=\frac{1}{4\mu}\frac{dP}{dz}\left(r^2-R_2^2\right)+C_1'\ln\!\frac{r}{R_2},\qquad C_1'=\frac{\dfrac{1}{4\mu}\dfrac{dP}{dz}\left(R_2^2-R_1^2\right)}{\ln\!\dfrac{R_1}{R_2}}.$$ The maximum occurs where $du/dr=0$, i.e. at $$\boxed{\,r_{max}=\sqrt{\dfrac{R_2^2-R_1^2}{2\,\ln(R_2/R_1)}}\,},$$ which lies nearer the inner wall than the arithmetic mean radius.