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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)

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
Duct side / length0.3 m / 30 m
Wall / ceramic thickness2 mm steel, 38 mm ceramic
Inside / outside coefficients$h_i=100$, $h_o=10$ W/m²·°C
Conductivities$k_\text{steel}=25$, $k_\text{ceramic}=0.2$ W/m·°C
Gas flow / $c_p$ / inlet1.5 kg/s / 1100 J/kg·°C / 800 °C
Surroundings20 °C
gas 800°C1.5 kg/sseries resistances (per m²-basis):1/U = 1/hᵢ + t_s/k_s + t_c/k_c + 1/hₒ= 0.01 + 0.00008 + 0.19 + 0.10U ≈ 3.33 W/m²·°CT_out = T∞ + (T_in−T∞)e^(−UAₛ/ṁc_p)ceramic (38 mm) over 2 mm steel
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.

  1. 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).==
  2. Conductance of the duct. Inner surface area $A_s=4(0.3)(30)=36$ m², so $UA_s=3.33\times36=120$ W/°C.
  3. 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.
QuantityResult
Overall coefficient $U$≈ 3.33 W/m²·°C
Duct conductance $UA_s$≈ 120 W/°C
Exit bulk gas temperature≈ 745 °C