22-Mec-A1 Applied Thermodynamics and Heat Transfer · December 2016
Question 6 of 8: Exit Gas Temperature in a Ceramic-Lined Duct
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 6: Exit Gas Temperature in a Ceramic-Lined Duct (equal value)
Figure 6 — Duct-wall build-up (inner film → 2 mm steel → 38 mm ceramic → outer film). The ceramic and the outer film dominate the resistance; the gas cools along the 30 m run following a single-stream exponential decay.
Approach. Add the four series resistances (inside film, steel, ceramic, outside film) to get the overall $U$, then march the single gas stream along the duct with the exponential temperature-decay relation.
Overall coefficient. On a per-unit-area (thin-wall) basis,
$$\frac1U=\frac1{h_i}+\frac{t_s}{k_s}+\frac{t_c}{k_c}+\frac1{h_o}=0.01+0.00008+0.19+0.10=0.300\ \text{m}^2\text{}\cdot\text{°C/W}$$
==**$U\approx3.33$ W/m²·°C** (the ceramic, 0.19, and outer film, 0.10, dominate).==
Conductance of the duct. Inner surface area $A_s=4(0.3)(30)=36$ m², so $UA_s=3.33\times36=120$ W/°C.
Single-stream temperature decay. With $\dot m c_p=1.5\times1100=1650$ W/°C,
$$T_\text{out}=T_\infty+(T_\text{in}-T_\infty)\,e^{-UA_s/\dot m c_p}=20+(800-20)\,e^{-120/1650}$$
$$=20+780\,e^{-0.0727}=20+725.3$$
==**$T_\text{out}\approx745$ °C.**==
Check
Thin-wall plane resistances on the inner area are used; carrying the true logarithmic/area corrections for the square section (outer perimeter 1.52 m vs inner 1.2 m) lowers the exit temperature by only ~1 °C (to ≈ 744 °C). The gas cools just 55 °C over 30 m because the ceramic makes the wall a good insulator — the duct loses little of its thermal energy.