25-Nav-A1 Fundamentals of Naval Architecture · May-98-Mar-A1 2016
Question 8 of 8: Cross-Flow Water/Air Tube-Bank Heat Exchanger
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Examinations, May 2016 — 98-Mar-A1 Applied Thermodynamics and Heat Transfer, 3 hours, open book (Part A: Thermodynamics, Part B: Heat Transfer; 5 of 8 questions required, all 8 answered below for full study coverage).
Reference texts: Cengel & Boles, Thermodynamics: An Engineering Approach; Sonntag, Borgnakke & Van Wylen, Fundamentals of Thermodynamics; Incropera & DeWitt, Fundamentals of Heat and Mass Transfer.
It is solved as the thermodynamics/heat-transfer exam it actually is.
Given. 40 tubes of 1 cm diameter, each spanning the 1 m width of a 1 m × 1 m duct (so each tube's length is 1 m), water inside and hot air in cross-flow outside.
Given data
Quantity
Symbol
Value
Tube count, diameter, length
$N,\,D,\,L$
40, 1 cm, 1 m
Water: $c_p$, inlet $T$, velocity
$c_{p,w},\,T_{w,i},\,V_w$
4180 J/kg·K, 18°C, 3 m/s
Air: $c_p$, inlet $T$, $P$, velocity
$c_{p,a},\,T_{a,i},\,P,\,V_a$
1010 J/kg·K, 130°C, 105 kPa, 12 m/s
Overall coefficient
$U$
80 W/m²·K
Find. Water and air outlet temperatures, and the total rate of heat transfer.
Approach. Get both mass flow rates from the given velocities and flow areas, form $C_{min},C_{max}$, compute $NTU=UA_s/C_{min}$ with $A_s=N\pi DL$, apply the crossflow (both fluids unmixed) effectiveness correlation, then back out $Q$ and both outlet temperatures.
Mass flow rates. Water fills the 40 tube bores: $\dot m_w=\rho_wV_w\!\left(N\dfrac{\pi}{4}D^2\right)=998(3)(40)(7.854\times10^{-5})\approx9.41\text{ kg/s}$. Air density at 130°C, 105 kPa (ideal gas): $\rho_a=P/(RT)=105{,}000/(287\times403.15)\approx0.908\text{ kg/m}^3$; the 40 tubes block a frontal area $N\,D\,L=0.40\text{ m}^2$ of the 1 m² duct, leaving a flow area of $0.60\text{ m}^2$:
$$\dot m_a=\rho_aV_a(1-ND L)=0.908(12)(0.60)\approx6.53\text{ kg/s}$$
Heat capacity rates and NTU. $C_w=\dot m_wc_{p,w}=39{,}320\text{ W/K}$, $C_a=\dot m_ac_{p,a}=6600\text{ W/K}$ (air is the minimum-capacity fluid), $C_r=C_{min}/C_{max}=0.168$. Surface area $A_s=N\pi DL=1.257\text{ m}^2$, so
$$NTU=\frac{UA_s}{C_{min}}=\frac{80(1.257)}{6600}\approx0.01523$$
Effectiveness and heat rate. For crossflow with both fluids unmixed at this very small NTU, $\varepsilon\approx NTU\approx0.01507$ (the exchanger is lightly loaded — only 40 small tubes across a 1 m² duct):
$$Q=\varepsilon C_{min}(T_{a,i}-T_{w,i})=0.01507(6600)(130-18)$$
$$\boxed{Q\approx11.14\text{ kW}}$$