Question 3 of 6: Copper Tube — Free Convection and Fins
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exams — May 2017 — 16-Chem-A3 Heat and Mass Transfer. Three-hour, open-book exam; one textbook and any non-communicating calculator permitted. Format: two parts of three problems each (Part A — Heat Transfer, Part B — Mass Transfer), all problems worth 25 points; candidates attempt at least two per part and only the first two per part are marked. The six problems are renumbered 1–6 and all are solved below for completeness. Property data are taken from the problem statements and standard open-book tables (the paper supplies the air-property table A-9); values used are stated in each Given block.
Reference texts: Incropera, DeWitt, Bergman & Lavine, Fundamentals of Heat and Mass Transfer (Wiley) — conduction resistances, critical radius, fins, convection correlations; Coulson & Richardson, Chemical Engineering Vol. 1 (Butterworth-Heinemann) — the packed-bed, distillation and sublimation problems of this style; Treybal, Mass-Transfer Operations (3rd ed., McGraw-Hill) — differential distillation and gas adsorption; Geankoplis, Transport Processes and Separation Process Principles (4th ed., Prentice Hall) — packed-bed and convective mass-transfer coefficients; supporting data from Perry's Chemical Engineers' Handbook (9th ed.) and the paper's Table A-9 (properties of air).
Part A — Heat Transfer
Question 3: Copper Tube — Free Convection and Fins (25 points)
Given. Water at $40\ \text{°C}$, $v = 0.10$ m/s inside a thin copper tube $D = 0.025$ m, $L = 1$ m, $k_{Cu} = 380\ \text{W/m}\cdot\text{K}$; air at $20\ \text{°C}$ outside with $h_a = 1.32\{(T_s-T_a)/D\}^{0.25}$. Water: $\rho = 965.3$, $k = 0.675$, $\mu = 3.15\times10^{-4}$ (SI); $c_p \approx 4180\ \text{J/kg}\cdot\text{K}$ assumed (not printed — see note).
Quantity
Value
Water T / velocity
40 °C / 0.10 m/s
Tube ID / length
0.025 m / 1 m
Air T
20 °C
Fins
8 × (2 mm thick, 20 mm high), copper
Find. (a) $U$, (b) wall temperature $T_s$, (c) heat loss $Q$ for the bare tube; then (d) $U$ and (e) $Q$ with the 8 fins.
Figure 3 — End view of the finned copper tube: warm water inside, eight longitudinal copper fins radiating into still air. The outside free-convection film is the controlling resistance, so extending the outer area is what raises the overall coefficient.
Check
The water $c_p$ is not printed; 4180 J/kg·K is assumed. It is not load-bearing: the inside coefficient comes out ~1000 W/m²·K against an outside free-convection coefficient of ~7 W/m²·K, so the air film controls $U$ and any reasonable $c_p$ leaves the answers unchanged to three figures. The "8 rectangular radial fins" are taken as straight fins running the full 1 m length of the tube and projecting radially outward (a star-shaped cross-section), which is the arrangement the fin count and the adiabatic-tip wording describe.
Approach. Get the inside coefficient from Dittus–Boelter, then close the wall energy balance $h_i(T_w-T_s)=h_a(T_s)(T_s-T_a)$ (with the temperature-dependent $h_a$) for $T_s$; $U$ and $Q$ follow. For the fins, compute the fin efficiency, build the effective outside area, and re-close the balance.
Inside (water) coefficient. $Re = \rho v D/\mu = (965.3)(0.10)(0.025)/(3.15\times10^{-4}) = 7660$ (turbulent), $Pr = \mu c_p/k = 1.95$. The water is being cooled, so Dittus–Boelter takes $n = 0.3$ (at $Re \approx 7700$ the flow is only just turbulent, but $h_i$ barely matters here):
$$Nu = 0.023\,Re^{0.8}Pr^{0.3} = 36.0,\qquad h_i = \frac{Nu\,k}{D} = \boxed{972\ \text{W/m}^2\text{K}}.$$
Wall temperature from the coupled balance (part b). Through the thin, high-conductivity wall $T_s$ is essentially uniform, so at steady state the inside and outside fluxes match:
$$h_i(T_w - T_s) = 1.32\left(\frac{T_s-T_a}{D}\right)^{0.25}(T_s-T_a).$$
Solving (the outside coefficient is tiny) gives $\boxed{T_s = 39.9\ \text{°C}}$ — the wall sits within $0.1\ \text{°C}$ of the water, because the air film chokes the heat flow.
Outside coefficient and overall $U$ (part a). At $T_s = 39.9\ \text{°C}$,
$$h_a = 1.32\left(\frac{39.9-20}{0.025}\right)^{0.25} = 7.01\ \text{W/m}^2\text{K}.$$
With the thin wall ($A_i \approx A_o$) the series resistance gives
$$U = \left(\frac1{h_i} + \frac1{h_a}\right)^{-1} = \left(\frac1{972}+\frac1{7.01}\right)^{-1} = \boxed{6.96\ \text{W/m}^2\text{K}}.$$
Bare-tube heat loss (part c). Outer area $A_o = \pi D L = \pi(0.025)(1) = 0.0785\ \text{m}^2$:
$$Q = U A_o (T_w - T_a) = 6.96(0.0785)(20) = \boxed{10.9\ \text{W}}.$$
Fin efficiency (parts d–e). Each rectangular fin ($t = 2$ mm, height $L_f = 20$ mm, adiabatic tip) has $m = \sqrt{2h_a/(k_{Cu}t)} = \sqrt{2(7.01)/(380\times0.002)} = 4.30\ \text{m}^{-1}$, so $mL_f = 0.086$ and
$$\eta_f = \frac{\tanh(mL_f)}{mL_f} = 0.998.$$
The copper fins are essentially isothermal — as expected against so weak an air film.
Effective outside area and new $U$. Eight fins add $A_{fin} = 8(2 L_f)L = 8(0.040)(1) = 0.320\ \text{m}^2$ (two faces each); the exposed base is $A_{base} = \pi D L - 8tL = 0.0785 - 0.016 = 0.0625\ \text{m}^2$, so
$$A_{eff} = A_{base} + \eta_f A_{fin} = 0.0625 + 0.998(0.320) = 0.382\ \text{m}^2.$$
Combining resistances on a UA basis and referring $U$ to the bare outer area $A_o$:
$$UA = \left(\frac1{h_i A_i} + \frac1{h_a A_{eff}}\right)^{-1} = 2.57\ \text{W/K}, \qquad U = \frac{UA}{A_o} = \boxed{32.7\ \text{W/m}^2\text{K}}.$$
Finned heat-transfer rate (part e).
$$Q = UA\,(T_w - T_a) = 2.57(20) = \boxed{51.4\ \text{W}},$$
a 4.7-fold increase over the bare tube — the fins pay off precisely because the outside film is the bottleneck.