Question 3 of 6: B1 — Conduction with temperature-dependent conductivity
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 3: B1 — Conduction with temperature-dependent conductivity
Given. One-dimensional steady conduction, no generation. Conductivity $k=k_0(1+\beta T)$. Surfaces held at $T_0$ (hot) and $T_L$ (cold). Compare against the constant-$k$ (reference) profile, which is linear in $x$ for the wall and logarithmic in $r$ for the cylinder.
Find. The location of maximum deviation between the actual and constant-$k$ temperature profiles, (a) in the plane wall, (b) in the hollow cylinder.
Fig. B1: The actual variable-$k$ profile (blue) departs most from the constant-$k$ reference (red dashed) at the location where the local temperature equals the mean $T_m=(T_0+T_L)/2$ — a result independent of geometry. The dashed circle marks the cylinder’s $r^\ast$.
Approach. The deviation is greatest where its $x$- (or $r$-) derivative vanishes, i.e. where the actual profile’s slope equals the reference slope; because the constant flux equals the mean conductivity times the reference slope, that condition pins the local temperature to the mean $T_m$.
Constant flux integral (plane wall). With $q=-k\,dT/dx$ constant, $-k_0(1+\beta T)\,dT=q\,dx$; integrating, $$k_0\!\left(T+\tfrac{\beta}{2}T^2\right)=D-qx .$$ The reference (constant-$k$) profile is the straight line $T_{ref}(x)=T_0+(T_L-T_0)\,x/L$ with constant slope $(T_L-T_0)/L$.
Mean-conductivity form of the flux. Integrating $q$ across the wall gives $q=\dfrac{k_0\left[1+\tfrac{\beta}{2}(T_0+T_L)\right](T_0-T_L)}{L}=\bar k\,\dfrac{T_0-T_L}{L}$, where $\bar k=k_0\!\left[1+\tfrac{\beta}{2}(T_0+T_L)\right]$ is $k$ evaluated at the mean temperature.
Locate maximum deviation. The gap $\Delta(x)=T(x)-T_{ref}(x)$ is stationary where $dT/dx=(T_L-T_0)/L$. Substituting this slope into $-k_0(1+\beta T)\,dT/dx=q=\bar k(T_0-T_L)/L$ forces $1+\beta T=1+\tfrac{\beta}{2}(T_0+T_L)$, i.e. $$\boxed{\,T^\ast=\frac{T_0+T_L}{2}\equiv T_m\,}\qquad(\text{independent of geometry}).$$
Position in the wall (part a). Setting $T(x^\ast)=T_m$ in the integral of Step 1 and simplifying gives $$\frac{x^\ast}{L}=\frac{1+\tfrac{\beta}{4}(3T_0+T_L)}{2\left[1+\tfrac{\beta}{2}(T_0+T_L)\right]}\ \xrightarrow{\ \beta\to0\ }\ \tfrac12 .$$ Since $T_0>T_L$ gives $3T_0+T_L>2(T_0+T_L)$, the ratio exceeds $\tfrac12$ for $\beta>0$: the higher conductivity near the hot face flattens the gradient there, so the actual profile bows above the straight line and does not fall to $T_m$ until past the mid-plane — the peak-deviation plane sits toward the cold face (toward the hot face if $\beta<0$).
Hollow cylinder (part b). The same argument with $q'=-k\,2\pi r\,dT/dr$ constant gives $k_0(T+\tfrac{\beta}{2}T^2)=D-\dfrac{q'}{2\pi}\ln r$; the reference profile is logarithmic. The maximum deviation is again at $T=T_m$ (the slope-matching argument is unchanged, since $k\,r\,dT/dr$ is constant and the reference has $r\,dT_{ref}/dr$ constant). Because $k_0(T+\tfrac{\beta}{2}T^2)$ is now linear in $\ln r$ exactly as it was linear in $x$ for the wall, the same fraction applies to $\ln r$: $$\boxed{\,\frac{\ln(r^\ast/R_0)}{\ln[(R_0+L)/R_0]}=\frac{1+\tfrac{\beta}{4}(3T_0+T_L)}{2\left[1+\tfrac{\beta}{2}(T_0+T_L)\right]},\qquad r^\ast=R_0\left(\frac{R_0+L}{R_0}\right)^{x^\ast/L}\,}$$ As $\beta\to0$ this tends to the geometric-mean radius $\sqrt{R_0(R_0+L)}$; for $\beta>0$ it lies outside it, toward the cold outer surface.
Quantity
Result
Temperature of max deviation
$T^\ast=(T_0+T_L)/2$ (both geometries)
Plane-wall position
$x^\ast/L=\dfrac{1+\tfrac{\beta}{4}(3T_0+T_L)}{2[1+\tfrac{\beta}{2}(T_0+T_L)]}$ ($>\tfrac12$, toward the cold face, for $\beta>0$)
Cylinder radius
$r^\ast=R_0\left[(R_0+L)/R_0\right]^{x^\ast/L}\to\sqrt{R_0(R_0+L)}$ as $\beta\to0$