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.
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.
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.)