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22-Mec-A1 Applied Thermodynamics and Heat Transfer · May 2016

Question 8 of 8: Cross-Flow Tube-Bank Heat Exchanger (ε–NTU)

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

Notes on this paper

Reference texts: Çengel & Boles, Thermodynamics: An Engineering Approach (9th ed., McGraw-Hill) — closed- and open-system energy balances, steam tables, vapour and gas power cycles, and vapour-compression refrigeration; Çengel & Ghajar, Heat and Mass Transfer (6th ed.) and Incropera, DeWitt, Bergman & Lavine, Fundamentals of Heat and Mass Transfer (8th ed., Wiley) — cylindrical composite-wall conduction, internal-flow and cross-flow convection correlations, natural convection with radiation, and the ε–NTU heat-exchanger method. Freon-12 property data are taken from the appendix supplied with the exam; steam, air and engine-oil data from standard tables.

Paper format: National Examination 07-Mec-A1, 3 hours, open book. Part A — Thermodynamics (Q1–4); Part B — Heat Transfer (Q5–8). Each answer carries equal value; a complete paper is any five (three from one part, two from the other). All eight questions are solved in full below.

Question 8: Cross-Flow Tube-Bank Heat Exchanger (ε–NTU) (equal value)

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.

QuantityValue
Tubes: number / diameter / length40 / 0.01 m / 1 m (span the duct)
Water inlet / velocity18 °C / 3 m/s
Air inlet / pressure / velocity130 °C / 105 kPa / 12 m/s
Overall coefficient $U$80 W/m²·°C
1 m × 1 m duct40 water tubes (into page)air 130°C≈129°C
Figure 8 — Cross-flow tube bank: cold water runs inside the 40 tubes (into the page); hot air sweeps across them along the duct. Both streams are unmixed. The exchanger area is small relative to the large capacity rates, so the temperature changes are slight.

Given. A cross-flow bank of 40 tubes (1 cm dia) in a 1 m × 1 m duct: water in at 18 °C/3 m/s inside, air in at 130 °C/105 kPa/12 m/s across, U = 80 W/m²·°C. Find. Both outlet temperatures and the heat-transfer rate.

Approach. Compute both capacity rates from the stated velocities, form NTU on the tube surface area, and use the cross-flow (both-unmixed) effectiveness relation to get the duty and the two outlet temperatures.

  1. Water capacity rate. $\dot m_w=\rho_w(n\tfrac{\pi}{4}D^2)V=998.7(40\cdot7.85\times10^{-5})(3)=9.41\ \text{kg/s}$; $C_w=\dot m_w c_{p,w}=3.93\times10^{4}$ W/K.
  2. Air capacity rate. $\rho_a=P/RT=105\,000/(287\cdot403)=0.908\ \text{kg/m}^3$; $\dot m_a=\rho_a(1\,\text{m}^2)V=0.908(12)=10.9\ \text{kg/s}$; $C_a=1.10\times10^{4}$ W/K. Thus $C_\text{min}=C_a$, $C_r=0.28$.
  3. Surface area and NTU. $A_s=n\pi DL=40\pi(0.01)(1)=1.257\ \text{m}^2$, so $$\text{NTU}=\frac{UA_s}{C_\text{min}}=\frac{80(1.257)}{1.10\times10^{4}}=0.0091.$$
  4. Effectiveness (cross-flow, both unmixed). $\varepsilon=1-\exp\!\big\{\tfrac{1}{C_r}\text{NTU}^{0.22}[e^{-C_r\text{NTU}^{0.78}}-1]\big\}=0.00907$ (essentially $\varepsilon\approx\text{NTU}$ at this tiny NTU).
  5. Duty and outlet temperatures. $$\dot Q=\varepsilon C_\text{min}(T_{a,i}-T_{w,i})=0.00907(1.10\times10^{4})(112)=\boxed{11.2\ \text{kW}}.$$ Then $T_{a,o}=130-\dot Q/C_a=\boxed{129.0\,{}^\circ\text{C}}$ and $T_{w,o}=18+\dot Q/C_w=\boxed{18.3\,{}^\circ\text{C}}.$
Check
Energy balances close: $\dot Q=C_a(130-129.0)=C_w(18.3-18)=11.2$ kW. The striking result — barely 1 °C off the air and 0.3 °C on the water — is correct: with only 1.26 m² of area against ~10⁴ W/K capacity rates, NTU ≈ 0.009, so this exchanger is grossly undersized for any meaningful temperature change. The tube length is taken as the 1 m duct span, since the tubes must cross the flow for a cross-flow arrangement.
QuantityResult
Water / air capacity rate3.93×10⁴ / 1.10×10⁴ W/K
$C_\text{min}$ / $C_r$air / 0.28
Surface area / NTU1.26 m² / 0.0091
Effectiveness≈ 0.0091
Heat-transfer rate≈ 11.2 kW
Air outlet temperature≈ 129.0 °C
Water outlet temperature≈ 18.3 °C
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