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

Question 8 of 8: Cross-Flow Tube-Bank Heat Exchanger

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, boundary work, reciprocating-compressor and vapour/gas power cycles, and gas-turbine refrigeration; Çengel & Ghajar, Heat and Mass Transfer (6th ed.) and Incropera, DeWitt, Bergman & Lavine, Fundamentals of Heat and Mass Transfer (8th ed., Wiley) — radial composite-wall conduction, internal-flow decay, natural convection with radiation from a horizontal cylinder, and the ε–NTU cross-flow heat-exchanger method. Air and steam properties are evaluated from IAPWS-IF97 / ideal-air data; the gas-turbine cycle uses cold-air-standard constant specific heats.

Paper format: National Examination 07-Mec-A1, December 2016, 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 and two from the other). All eight questions are solved in full below.

Question 8: Cross-Flow Tube-Bank Heat Exchanger (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
Tubes40 × 1 cm diameter, thin-walled, 1 m long
Water side18 °C in, $V=3$ m/s, $c_p=4180$
Air side130 °C, 105 kPa in, $V=12$ m/s, $c_p=1010$
Overall coefficient$U=80$ W/m²·°C
hot air 130°C, 12 m/swater in tubes: 18°C, 3 m/s (⊗ into page)both fluidsunmixed
Figure 8 — Cross-flow arrangement: cold water flows through the 40 tubes (into the page) while hot air sweeps across them along the duct. Both streams are unmixed.

Approach. Compute both heat-capacity rates from the flow areas and inlet densities, identify $C_\text{min}$, evaluate NTU from $UA_s/C_\text{min}$, and apply the both-fluids-unmixed cross-flow effectiveness to get the duty and outlet temperatures.

  1. Capacity rates. Water: $\dot m_w=\rho_w A_\text{tubes}V=998.6\,(40\cdot\tfrac{\pi}{4}0.01^2)(3)=9.41$ kg/s, $C_w=39{,}340$ W/°C. Air: $\rho_a=105000/(287\cdot403)=0.908$ kg/m³, $\dot m_a=0.908(1)(12)=10.89$ kg/s, $C_a=11{,}000$ W/°C. Thus $C_\text{min}=C_a$, $C_r=0.280$.
  2. NTU. Heat-transfer area $A_s=40\,\pi(0.01)(1)=1.257$ m², so $$\text{NTU}=\frac{UA_s}{C_\text{min}}=\frac{80(1.257)}{11000}=0.00914$$
  3. Effectiveness (both unmixed). $$\varepsilon=1-\exp\!\left\{\tfrac{1}{C_r}\text{NTU}^{0.22}\big[e^{-C_r\,\text{NTU}^{0.78}}-1\big]\right\}=0.0091$$
  4. Duty and outlet temperatures. $$\dot Q=\varepsilon\,C_\text{min}(T_{a,i}-T_{w,i})=0.0091(11000)(130-18)$$ ==**$\dot Q\approx11.2$ kW.**== $$T_{a,o}=130-\frac{\dot Q}{C_a}=129.0\ \text{°C},\qquad T_{w,o}=18+\frac{\dot Q}{C_w}=18.3\ \text{°C}$$
Check — the exchanger is drastically undersized.
With only 40 one-metre tubes the surface is $A_s=1.26$ m² and $UA_s=100$ W/°C — barely 1 % of $C_\text{min}$, so $\varepsilon<1\%$ and both streams leave essentially at their inlet temperatures ($\Delta T_\text{air}\approx1$ °C, $\Delta T_\text{water}\approx0.3$ °C). The numbers are solved exactly as printed; a real unit would need vastly more area. (This question is identical to the 2016-May sitting's Q8.)
QuantityResult
Water / air capacity rate39.3 / 11.0 kW/°C ($C_\text{min}=$ air)
NTU / effectiveness0.0091 / 0.91 %
Heat-transfer rate≈ 11.2 kW
Air outlet temperature≈ 129 °C
Water outlet temperature≈ 18.3 °C
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