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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)

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.

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.

QuantityValue
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 inlet300 °C / 1000 °C
Case 1 cold outlet700 °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.

position along exchanger →$T$ (°C)hot 1000→600cold 700 (out) ← 300 (in)Case 1: ΔT = 300 °C everywhere (Cr=1) → LMTD = 300Case 2 target: cold out 800 °C, ΔT = 200 → larger area
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.

  1. Case 1 duty and hot outlet. $$\dot Q_1=C_c(700-300)=1920(400)=768\ \text{kW},\qquad T_{h,o}=1000-\frac{\dot Q_1}{C_h}=1000-400=600\ ^\circ\text{C}$$
  2. Case 1 LMTD and $UA$. Terminal differences: hot-in/cold-out $=1000-700=300$; hot-out/cold-in $=600-300=300$. Equal, so $\text{LMTD}_1=300\ ^\circ\text{C}$: $$UA_1=\frac{\dot Q_1}{\text{LMTD}_1}=\frac{768\,000}{300}=2560\ \text{W/}^\circ\text{C}$$
  3. Case 2 duty and hot outlet. $$\dot Q_2=C_c(800-300)=1920(500)=960\ \text{kW},\qquad T_{h,o}=1000-\frac{960\,000}{1920}=500\ ^\circ\text{C}$$
  4. Case 2 LMTD and $UA$. Terminal differences: $1000-800=200$ and $500-300=200$, so $\text{LMTD}_2=200\ ^\circ\text{C}$: $$UA_2=\frac{960\,000}{200}=4800\ \text{W/}^\circ\text{C}$$
  5. 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).
QuantityCase 1 (700 °C)Case 2 (800 °C)
Duty $\dot Q$768 kW960 kW
Hot outlet600 °C500 °C
LMTD300 °C200 °C
$UA$2560 W/°C4800 W/°C
Required area increase ≈ 87.5 % (A₂ = 1.875 A₁)
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