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17-Phys-B6 Applied Thermodynamics and Heat Transfer · December 2018

Question 8 of 8: Water/Air Tubular Heat Exchanger — Effectiveness, Duty, Outlet Temperatures

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. 17-Phys-B6 Applied Thermodynamics and Heat Transfer, National Examination December 2018 — a three-hour open-book examination; candidates are expected to bring both a thermodynamics text and a heat-transfer text to make use of the property tables and graphs. A complete examination is five questions — either three from Part A (Thermodynamics, Q1–Q4) and two from Part B (Heat Transfer, Q5–Q8), or two from Part A and three from Part B — every question carrying equal value; all eight are solved below as a complete study set. Question 2 is solved as one connected narrative: the wet steam whose quality is measured by the throttling calorimeter in part (a) is the same steam entering the turbine in part (b), which is what makes part (c)'s "isentropic despite heat loss" observation checkable. Question 3 gives every cycle temperature directly from the printed diagram but no pressures, so it is solved purely from energy balances (constant specific heat, cold-air-standard) rather than isentropic pressure ratios — the intended reading, since no compressor/turbine pressure ratio is given anywhere on the page.

Reference texts. Y. A. Çengel and M. A. Boles, Thermodynamics: An Engineering Approach, 8th ed. (ideal-gas mixtures, air-standard Otto and Brayton cycles, throttling calorimeters, steam turbines, vapour-compression refrigeration); F. P. Incropera and D. P. DeWitt, Fundamentals of Heat and Mass Transfer, 7th ed. (composite cylindrical conduction with convection at both surfaces, heat generation in a solid cylinder, internal/external convection combined via an overall coefficient, effectiveness–NTU heat-exchanger analysis). Ammonia and steam saturation/superheat property values were computed (Bell et al., IAPWS-95 / REFPROP-quality equations of state) and cross-checked against the printed appendix tables on pages 5–6 of the source exam and standard steam tables, which they matched to 3–4 significant figures throughout.

Question 8: Water/Air Tubular Heat Exchanger — Effectiveness, Duty, Outlet Temperatures

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. Fifty parallel brass tubes ($d_i=2.3\text{ cm}$, $d_o=2.6\text{ cm}$, $L=6.7\text{ m}$ each) carry water ($\dot m_w=10\text{ kg/s}$, entering at 75°C) inside a tube-bundle exchanger; air ($\dot m_a=1.6\text{ kg/s}$, entering at 15°C) flows over the outside of the bundle. $\bar h_i=470$, $\bar h_o=210\text{ W/m}^2\cdot{}^{\circ}\text{C}$.

Given data
QuantitySymbolValue
Number / length of tubes$N,L$50 / 6.7 m
Tube ID / OD$d_i,d_o$2.3 cm / 2.6 cm
Inside / outside coefficients$\bar h_i,\bar h_o$470 / 210 W/m²·°C
Water flow / inlet temperature$\dot m_w,T_{w,in}$10 kg/s, 75°C
Air flow / inlet temperature$\dot m_a,T_{a,in}$1.6 kg/s, 15°C

Find. The exchanger effectiveness $\varepsilon$; the heat transfer rate $\dot Q$; the water and air outlet temperatures.

Casing(50 brass tubes, water inside,air across bundle)water in75°C, 10 kg/swater out(find)air in, 15°C, 1.6 kg/sair out (find)
Fifty parallel brass tubes carry hot water; air crosses the tube bundle inside the surrounding casing and is heated.
Check: no brass thermal conductivity is given, so the (thin, high-conductivity) tube-wall conduction resistance is neglected next to the two convective resistances — standard for a metal tube this thin.

Approach. Build the overall $UA$ from the inside and outside convective resistances (areas based on $d_i$ and $d_o$ respectively, $N$ tubes in parallel); find $C_{min},C_{max},C_r=C_{min}/C_{max}$ and $NTU=UA/C_{min}$; since $C_r$ turns out to be very small here, the effectiveness–NTU relation collapses to the single-stream limit regardless of the exact flow arrangement (crossflow/counterflow all agree to within about 1% at this $C_r$), so $\varepsilon=1-e^{-NTU}$ is used directly.

  1. Heat transfer areas and overall $UA$. $$A_i=\pi d_iLN=\pi\times0.023\times6.7\times50=24.21\text{ m}^2$$ $$A_o=\pi d_oLN=\pi\times0.026\times6.7\times50=27.36\text{ m}^2$$ $$\frac{1}{UA}=\frac{1}{\bar h_iA_i}+\frac{1}{\bar h_oA_o}=\frac{1}{470\times24.21}+\frac{1}{210\times27.36}$$ $$\boxed{UA=3818\text{ W/}{}^{\circ}\text{C}}$$
  2. Capacity rates and $NTU$. $$C_w=\dot m_wc_{p,w}=10\times4186=41{,}860\text{ W/K},\qquad C_a=\dot m_ac_{p,a}=1.6\times1005=1608\text{ W/K}$$ $$C_{min}=C_a=1608\text{ W/K},\qquad C_r=\frac{C_{min}}{C_{max}}=\frac{1608}{41{,}860}=0.0384$$ $$NTU=\frac{UA}{C_{min}}=\frac{3818}{1608}$$ $$\boxed{NTU=2.374}$$
  3. Effectiveness. With $C_r\approx0.038\ll1$, the water side is so much larger in capacity rate that it barely cools as it gives up heat — effectively a constant-temperature source, so every standard flow arrangement (counterflow, crossflow, either fluid mixed) converges to the same single-stream result to within about 1%: $$\varepsilon=1-e^{-NTU}=1-e^{-2.374}$$ $$\boxed{\varepsilon=0.907=90.7\%}$$ (An exact counterflow calculation at $C_r=0.0384$ gives $\varepsilon=0.902$ — a 0.5-point difference, confirming the arrangement is nearly irrelevant here.)
  4. Heat transfer rate and outlet temperatures. $$\dot Q_{max}=C_{min}(T_{w,in}-T_{a,in})=1608\times(75-15)=96{,}480\text{ W}$$ $$\dot Q=\varepsilon\,\dot Q_{max}=0.907\times96{,}480$$ $$\boxed{\dot Q=87.5\text{ kW}}$$ $$T_{a,out}=T_{a,in}+\frac{\dot Q}{C_a}=15+\frac{87{,}500}{1608}$$ $$\boxed{T_{a,out}=69.4\,{}^{\circ}\text{C}}$$ $$T_{w,out}=T_{w,in}-\frac{\dot Q}{C_w}=75-\frac{87{,}500}{41{,}860}$$ $$\boxed{T_{w,out}=72.9\,{}^{\circ}\text{C}}$$
Question 8 — results
QuantityValue
Overall $UA$3818 W/°C
$NTU$ (based on $C_{min}$ = air side)2.374
Effectiveness $\varepsilon$90.7%
Heat transfer rate $\dot Q$87.5 kW
Air outlet temperature69.4°C
Water outlet temperature72.9°C
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