NivaarExam PrepOfficial exam papers ↗

17-Phys-B6 Applied Thermodynamics and Heat Transfer · May 2016

Question 8 of 8: Cross-Flow Tube-Bank Heat Exchanger — Effectiveness–NTU

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

Notes on this paper

Paper format. 98-Phys-B6 Applied Thermodynamics and Heat Transfer, National Examination May 2016 — a three-hour open-book examination; candidates are expected to bring both a thermodynamics text and a heat-transfer text to make use of the property tables and charts. A complete examination is five questions — either three from Part A (Thermodynamics, Q1–Q4) and two from Part B (Heat Transfer, Q5–Q8), or two from Part A and three from Part B — every question carrying equal value; all eight are solved below as a complete study set. Where the exam's own "state your assumptions" licence applies (Part A cold-air-standard properties in Question 3; the rectangular-case geometry read from the printed illustration in Question 7), the assumption is flagged explicitly in a check callout rather than hedged inside the answer.

Reference texts. Y. A. Çengel and M. A. Boles, Thermodynamics: An Engineering Approach, 8th ed. (ideal-gas processes, vapour power cycles, gas-turbine/Brayton cycles, vapour-compression refrigeration); F. P. Incropera and D. P. DeWitt, Fundamentals of Heat and Mass Transfer, 7th ed. (conduction with convective boundaries, internal/external convection correlations, natural convection, radiation exchange, cross-flow heat-exchanger effectiveness–NTU analysis).

Question 8: Cross-Flow Tube-Bank Heat Exchanger — Effectiveness–NTU

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. 40 tubes, $D=1$ cm, in a 1 m × 1 m duct. Water (tube-side, hence UNMIXED — each tube's stream never contacts another): $c_p=4180$ J/kg°C, $T_{c,in}=18\,{}^{\circ}\text{C}$, $V=3$ m/s. Air (duct-side, open cross-section, hence MIXED): $c_p=1010$ J/kg°C, $T_{h,in}=130\,{}^{\circ}\text{C}$, 105 kPa, $V=12$ m/s. $U=80$ W/m2°C.

Check: the tube LENGTH is not printed explicitly. The only geometrically consistent reading of "40 tubes, 1 cm diameter, in a 1 m × 1 m duct" with air crossing the tube bank is that each tube spans the duct, i.e. $L=1$ m per tube — used below.
Given data
QuantitySymbolValue
Number of tubes / diameter$N,\,D$40 / 1 cm
Duct cross-section—1 m × 1 m
Water specific heat / inlet temp / velocity$c_{p,w},\,T_{c,in},\,V_w$4180 J/kg°C / $18\,{}^{\circ}\text{C}$ / 3 m/s
Air specific heat / inlet temp / velocity$c_{p,a},\,T_{h,in},\,V_a$1010 J/kg°C / $130\,{}^{\circ}\text{C}$ / 12 m/s
Air inlet pressure$P_a$105 kPa
Overall heat transfer coefficient$U$80 W/m2°C

Find. The water and air outlet temperatures and the total heat-transfer rate.

Approach. Compute both capacity rates $C=\dot{m}c_p$ from the given velocities and cross-sections, identify $C_{\min}/C_{\max}$, form $\text{NTU}=UA/C_{\min}$ with $A=N\pi DL$, apply the effectiveness–NTU relation for the one-fluid-mixed/one-unmixed cross-flow configuration (air mixed, water unmixed), then back out both outlet temperatures.

  1. Water-side capacity rate (40 parallel tubes). $$\dot{m}_w=\rho_w V_w N\left(\frac{\pi}{4}D^2\right)=(998.6)(3)(40)\left(\frac{\pi}{4}(0.01)^2\right)=9.41\text{ kg/s}$$ $$C_w=\dot{m}_w c_{p,w}=9.41(4180)=39{,}340\text{ W/K}$$
  2. Air-side capacity rate (duct approach flow). $$\rho_a=\frac{P_a}{RT_{h,in}}=\frac{105{,}000}{(287)(403.15)}=0.908\text{ kg/m}^3$$ $$\dot{m}_a=\rho_a V_a(1\text{ m}\times1\text{ m})=0.908(12)=10.89\text{ kg/s}$$ $$C_a=\dot{m}_a c_{p,a}=10.89(1010)=11{,}000\text{ W/K}$$
  3. $C_{\min}$, $C_{\max}$, and NTU. $C_a
  4. Effectiveness ($C_{\min}$ fluid mixed, $C_{\max}$ fluid unmixed): $$\varepsilon=\frac{1}{C_r}\left(1-\exp\!\big[-C_r\big(1-e^{-\text{NTU}}\big)\big]\right)=\boxed{0.00909}$$ (essentially $\varepsilon\approx\text{NTU}$, as expected in the small-NTU limit for any flow arrangement — a useful self-check.)
  5. Heat-transfer rate and outlet temperatures. $$q_{\max}=C_{\min}(T_{h,in}-T_{c,in})=11{,}000(130-18)=1{,}232{,}000\text{ W}$$ $$q=\varepsilon\, q_{\max}=0.00909(1{,}232{,}000)=\boxed{11.19\text{ kW}}$$ $$T_{c,out}=T_{c,in}+\frac{q}{C_w}=18+\frac{11{,}190}{39{,}340}=\boxed{18.29\,{}^{\circ}\text{C}}$$ $$T_{h,out}=T_{h,in}-\frac{q}{C_a}=130-\frac{11{,}190}{11{,}000}=\boxed{128.98\,{}^{\circ}\text{C}}$$

The temperature changes are small because the given $U$ (80 W/m2°C) and area (1.26 m2) together give a very small NTU relative to the large capacity rates on both sides — this is a genuinely undersized/lightly-loaded exchanger for the flow rates specified, not a computational error (confirmed by the $\varepsilon\approx\text{NTU}$ self-check above).

Question 8 — results
QuantityValue
Water capacity rate, $C_w$39,340 W/K
Air capacity rate, $C_a$11,000 W/K
NTU / effectiveness0.00914 / 0.00909
Heat-transfer rate, $q$11.19 kW
Water outlet temperature, $T_{c,out}$$18.29\,{}^{\circ}\text{C}$
Air outlet temperature, $T_{h,out}$$128.98\,{}^{\circ}\text{C}$
Back to the paper →