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Cold water $\left(c_{p}=4.18 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\( enters a heat exchanger at \)15^{\circ} \mathrm{C}$ at a rate of \(0.5 \mathrm{~kg} / \mathrm{s}\), where it is heated by hot air \(\left(c_{p}=1.0 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\) that enters the heat exchanger at \(50^{\circ} \mathrm{C}\) at a rate of $1.8 \mathrm{~kg} / \mathrm{s}$. The maximum possible heat transfer rate in this heat exchanger is (a) \(51.1 \mathrm{~kW}\) (b) \(63.0 \mathrm{~kW}\) (c) \(66.8 \mathrm{~kW}\) (d) \(73.2 \mathrm{~kW}\) (e) \(80.0 \mathrm{~kW}\)

Short Answer

Expert verified
Based on the solution provided, the maximum heat transfer rate in the heat exchanger is \(32.16 \mathrm{~kW}\).

Step by step solution

01

Identify known and unknown variables

We are given the following information: \(c_{p_{water}} = 4.18 \mathrm{~kJ/ (kg \cdot K)}\) - specific heat of water \(T_{water,initial} = 15^\circ \mathrm{C}\) - initial water temperature \(m_{water} = 0.5 \mathrm{~kg/s}\) - mass flow rate of water \(c_{p_{air}} = 1.0 \mathrm{~kJ/ (kg \cdot K)}\) - specific heat of air \(T_{air,initial} = 50^\circ \mathrm{C}\) - initial air temperature \(m_{air} = 1.8 \mathrm{~kg/s}\) - mass flow rate of air Unknown: \(Q\) - maximum heat transfer rate
02

Calculate the maximum temperature change

The maximum possible heat transfer occurs when the temperature of the air and water is equalized. Therefore, we need to calculate the maximum temperature change for both air and water: \(\Delta T_{max} = T_{mixed} - T_{initial}\) We also need to determine the mixed temperature \(T_{mixed}\). Since the heat exchange happens within a closed system, we have the relationship: \(m_{air} \cdot c_{p_{air}} \cdot (T_{air,initial} - T_{mixed}) = m_{water} \cdot c_{p_{water}} \cdot (T_{mixed} - T_{water,initial})\)
03

Solve for the mixed temperature

Let's solve the equation above to find \(T_{mixed}\): \(1.8 \cdot 1.0 \cdot (50 - T_{mixed}) = 0.5 \cdot 4.18 \cdot (T_{mixed} - 15)\) Simplify and solve for \(T_{mixed}\): \(T_{mixed} = \frac{1.8 \cdot 1.0 \cdot 50 + 0.5 \cdot 4.18 \cdot 15}{1.8 \cdot 1.0 + 0.5 \cdot 4.18} = 30.32^\circ \mathrm{C}\)
04

Calculate the heat transfer rate

Now, we can calculate the heat transfer rate for both air and water. For water: \(Q_{water} = m_{water} \cdot c_{p_{water}} \cdot (T_{mixed} - T_{water,initial})\) \(Q_{water} = 0.5 \cdot 4.18 \cdot (30.32 - 15) = 32.16 \mathrm{~kW}\) For air: \(Q_{air} = m_{air} \cdot c_{p_{air}} \cdot (T_{air,initial} - T_{mixed})\) \(Q_{air} = 1.8 \cdot 1.0 \cdot (50 - 30.32) = 35.41 \mathrm{~kW}\) Since in a heat exchanger, the heat transfer rate must be the same for air and water: \(Q = Q_{water} = Q_{air} = 32.16 \mathrm{~kW}\) The closest answer choice is: (a) \(51.1 \mathrm{~kW}\)

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Most popular questions from this chapter

Consider a recuperative crossflow heat exchanger (both fluids unmixed) used in a gas turbine system that carries the exhaust gases at a flow rate of $7.5 \mathrm{~kg} / \mathrm{s}\( and a temperature of \)500^{\circ} \mathrm{C}$. The air initially at \(30^{\circ} \mathrm{C}\) and flowing at a rate of $15 \mathrm{~kg} / \mathrm{s}$ is to be heated in the recuperator. The convective heat transfer coefficients on the exhaust gas and air sides are $750 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\( and \)300 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}$, respectively. Due to long-term use of the gas turbine, the recuperative heat exchanger is subject to fouling on both gas and air sides that offers a resistance of \(0.0004\) \(\mathrm{m}^{2}\). $/ \mathrm{W}$ each. Take the properties of exhaust gas to be the same as that of air \(\left(c_{p}=1069 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\). If the exit temperature of the exhaust gas is \(320^{\circ} \mathrm{C}\), determine \((a)\) if the air could be heated to a temperature of \(150^{\circ} \mathrm{C}\) and \((b)\) the area of the heat exchanger. (c) If the answer to part \((a)\) is no, then determine what should be the air mass flow rate in order to attain the desired exit temperature of \(150^{\circ} \mathrm{C}\) and \((d)\) plot the variation of the exit air temperature over a range of \(75^{\circ} \mathrm{C}\) to \(300^{\circ} \mathrm{C}\) with the air mass flow rate, assuming all the other conditions remain the same.

A shell-and-tube heat exchanger with two shell passes and four tube passes is used for cooling oil $\left(c_{p}=2.0 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\( from \)125^{\circ} \mathrm{C}\( to \)55^{\circ} \mathrm{C}$. The coolant is water, which enters the shell side at \(25^{\circ} \mathrm{C}\) and leaves at \(46^{\circ} \mathrm{C}\). The overall heat transfer coefficient is \(900 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). For an oil flow rate of \(10 \mathrm{~kg} / \mathrm{s}\), calculate the cooling water flow rate and the heat transfer area.

Steam is to be condensed on the shell side of a twoshell-passes and eight- tube-passes condenser, with 20 tubes in each pass. Cooling water enters the tubes at a rate of \(2 \mathrm{~kg} / \mathrm{s}\). If the heat transfer area is \(14 \mathrm{~m}^{2}\) and the overall heat transfer coefficient is $1800 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, the effectiveness of this condenser is (a) \(0.70\) (b) \(0.80\) (c) \(0.90\) (d) \(0.95\) (e) \(1.0\)

How would the answer to Prob. 11-150 be altered if we tried to approximate the heat transfer loss through the blood vessel with a fouling factor to describe physiological inhomogeneities? Assume that the fouling factor for the artery is \(0.0005\) \(\mathrm{m}^{2}\). K/W and the fouling factor for the vein is \(0.0003 \mathrm{~m}^{2} \cdot \mathrm{K} / \mathrm{W}\).

For a specified fluid pair, inlet temperatures, and mass flow rates, what kind of heat exchanger will have the highest effectiveness: double-pipe parallel- flow, double-pipe counterflow, crossflow, or multipass shell-and-tube heat exchanger?

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