22-Mec-A1 Applied Thermodynamics and Heat Transfer · May 2018
Question 8 of 8: Counterflow heat-exchanger area for a higher outlet temperature
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format: National Examination 16-Mec-A1, 3 hours, open book. Eight questions of equal value: Part A — Thermodynamics (Q1–Q4) and Part B — Heat Transfer (Q5–Q8). A complete paper is any five questions (three from one part and two from the other).
Reference texts: Çengel & Boles, Thermodynamics: An Engineering Approach (9th ed., McGraw-Hill) — first-law cycle analysis, wet-region steam properties, the ideal regenerative Rankine cycle with a closed feedwater heater, the air-standard Diesel cycle, and isentropic-efficiency compressor analysis; Çengel & Ghajar, Heat and Mass Transfer (6th ed.) and Incropera, DeWitt, Bergman & Lavine, Fundamentals of Heat and Mass Transfer (8th ed., Wiley) — steady conduction with internal generation in a composite cylinder, internal-flow convection at constant wall temperature, combined convection–radiation surface balances, and the LMTD method for counterflow heat exchangers. Water/steam properties are IAPWS-consistent; air is treated as an ideal gas with constant specific heats.
Question 8 — Counterflow heat-exchanger area for a higher outlet temperature (Part B, equal value)
Given. Counterflow exchanger. Cold fluid: $c_{p,c}=800\ \text{J/kg}\cdot\text{°C}$, $\dot m_c=2.4$ kg/s, in at 300 °C. Hot fluid: $c_{p,h}=960\ \text{J/kg}\cdot\text{°C}$, $\dot m_h=2.0$ kg/s, in at 1000 °C.
Quantity
Value
Cold capacity rate, $C_c=\dot m_c c_{p,c}$
2.4×800 = 1920 W/°C
Hot capacity rate, $C_h=\dot m_h c_{p,h}$
2.0×960 = 1920 W/°C
Cold inlet / hot inlet
300 °C / 1000 °C
Case 1 cold outlet
700 °C
Case 2 cold outlet (target)
800 °C
Find. the fractional increase in surface area (with $U$, flows and inlet temperatures unchanged) to raise the cold-fluid outlet from 700 °C to 800 °C.
Figure 8 — Counterflow temperature profiles. With equal capacity rates ($C_r=1$) the temperature difference is uniform along the exchanger, so the LMTD equals that constant gap: 300 °C in the base case, 200 °C for the more demanding 800 °C target.
Approach. The capacity rates are equal ($C_r=1$), so for counterflow the terminal temperature differences are equal and the LMTD is just that constant gap. Compute $UA=\dot Q/\text{LMTD}$ for each case; with $U$ fixed the area ratio equals the $UA$ ratio.
Case 1 duty and hot outlet.
$$\dot Q_1=C_c(700-300)=1920(400)=768\ \text{kW},\qquad T_{h,o}=1000-\frac{\dot Q_1}{C_h}=1000-400=600\ ^\circ\text{C}$$
Case 1 LMTD and $UA$. Terminal differences: hot-in/cold-out $=1000-700=300$; hot-out/cold-in $=600-300=300$. Equal, so $\text{LMTD}_1=300\ ^\circ\text{C}$:
$$UA_1=\frac{\dot Q_1}{\text{LMTD}_1}=\frac{768\,000}{300}=2560\ \text{W/}^\circ\text{C}$$
Case 2 duty and hot outlet.
$$\dot Q_2=C_c(800-300)=1920(500)=960\ \text{kW},\qquad T_{h,o}=1000-\frac{960\,000}{1920}=500\ ^\circ\text{C}$$
Case 2 LMTD and $UA$. Terminal differences: $1000-800=200$ and $500-300=200$, so $\text{LMTD}_2=200\ ^\circ\text{C}$:
$$UA_2=\frac{960\,000}{200}=4800\ \text{W/}^\circ\text{C}$$
Area increase (U constant).
$$\frac{A_2}{A_1}=\frac{UA_2}{UA_1}=\frac{4800}{2560}=1.875\;\Rightarrow\;\frac{\Delta A}{A_1}=0.875$$
The surface area must increase by about 87.5 % (to 1.875× the original).