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A single-pass crossflow heat exchanger with both fluids unmixed has water entering at \(16^{\circ} \mathrm{C}\) and exiting at \(33^{\circ} \mathrm{C}\), while oil $\left(c_{p}=1.93 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right.\( and \)\left.\rho=870 \mathrm{~kg} / \mathrm{m}^{3}\right)$ flowing at \(0.19 \mathrm{~m}^{3} / \mathrm{min}\) enters at $38^{\circ} \mathrm{C}\( and exits at \)29^{\circ} \mathrm{C}$. If the surface area of the heat exchanger is \(20 \mathrm{~m}^{2}\), determine \((a)\) the NTU value and \((b)\) the value of the overall heat transfer coefficient.

Short Answer

Expert verified
Question: Calculate the NTU value and the overall heat transfer coefficient for a single-pass crossflow heat exchanger with both fluids unmixed, given the inlet and outlet temperatures of water and oil, the flow rate of oil, and the surface area of the heat exchanger. Inlet temperatures: Water: \(T_{wi} = 20 ^{\circ}C\) Oil: \(T_{oi} = 70 ^{\circ}C\) Outlet temperatures: Water: \(T_{wo} = 45 ^{\circ}C\) Oil: \(T_{oo} = 42 ^{\circ}C\) Flow rate of oil: \(\text{0.19 m}^3\text{/min}\) Density of oil: \(870\,\text{kg/m}^3\) Specific heat capacity of oil: \(c_{p_{o}} = 2.1\,\text{kJ/kg}\cdot^{\circ}C\) Heat exchanger surface area: \(A = 20\,\text{m}^2\) Calculate (a) NTU value, and (b) the value of the overall heat transfer coefficient.

Step by step solution

01

Find the capacity rates of water and oil

To find the capacity rates (C), we first need to find the mass flow rate of oil and the specific heat capacities of water and oil. We are given the specific heat capacity of oil, but we need to find the specific heat capacity of water. The specific heat capacity of water is approximately \(c_{p_{w}} = 4.18 \mathrm{kJ/kg \cdot K}\). Next, we need to find the mass flow rate of oil (m_o) using the given volumetric flow rate and density: $$m_o = \rho \cdot \text{flow rate} = 870 \mathrm{kg/m^3} \cdot 0.19 \mathrm{m^3/min} \cdot \frac{1 \mathrm{min}}{60 \mathrm{s}} = 2.744 \mathrm{kg/s}$$ Now, we can calculate the capacity rates of water and oil (C_w and C_o, respectively): $$C_w = m_{w}c_{p_{w}} \hspace{1cm} \text{and} \hspace{1cm} C_o = m_{o}c_{p_{o}}$$
02

Calculate the heat transfer effectiveness

Next, we need to find the heat transfer effectiveness (ε) using the given temperature values: $$ε = \frac{q_{actual}}{q_{max}}$$ Here, the actual heat transfer (\(q_{actual}\)) is the product of the capacity rates and the change in temperature for either the water or the oil: $$q_{actual} = m_{w}c_{p_{w}}(T_{wo} - T_{wi}) = m_{o}c_{p_{o}}(T_{oi} - T_{oo})$$ The maximum possible heat transfer (\(q_{max}\)) is given as the product of the minimum capacity rate and the change in inlet temperatures: $$q_{max} = C_{min}(T_{oi}-T_{wi})$$
03

Calculate the NTU value

Now, we can use the effectiveness-NTU method to find the NTU value: $$NTU = \frac{-\log{(1-ε)}}{1-\frac{C_{min}}{C_{max}}}$$
04

Calculate the rate of heat transfer (Q)

We will now calculate the rate of heat transfer: $$Q = C_{min} (T_{oi} - T_{wi}) \cdot ε$$
05

Calculate the log mean temperature difference (LMTD)

Next, we need to find the LMTD by using the inlet and outlet temperatures: $$LMTD = \frac{(ΔT_1 - ΔT_2)}{\log{\frac{ΔT_1}{ΔT_2}}}$$ where $$ΔT_1 = T_{wi} - T_{oo} \hspace{1cm} \text{and} \hspace{1cm} ΔT_2 = T_{wo} - T_{oi}$$
06

Determine the overall heat transfer coefficient (U)

Finally, we can now calculate the overall heat transfer coefficient (U) using the surface area (A), rate of heat transfer (Q), and LMTD: $$U = \frac{Q}{A \cdot LMTD}$$

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Most popular questions from this chapter

Oil in an engine is being cooled by air in a crossflow heat exchanger, where both fluids are unmixed. Oil $\left(c_{p k}=2047 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( flowing with a flow rate of \)0.026 \mathrm{~kg} / \mathrm{s}\( enters the heat exchanger at \)75^{\circ} \mathrm{C}$, while air \(\left(c_{p c}=1007 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) enters at \(30^{\circ} \mathrm{C}\) with a flow rate of $0.21 \mathrm{~kg} / \mathrm{s}$. The overall heat transfer coefficient of the heat exchanger is \(53 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}\) and the total surface area is \(1 \mathrm{~m}^{2}\). Determine \((a)\) the heat transfer effectiveness and \((b)\) the outlet temperature of the oil.

A counterflow heat exchanger is used to cool oil $\left(c_{p}=2.20 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\( from \)110^{\circ} \mathrm{C}\( to \)85^{\circ} \mathrm{C}\( at a rate of \)0.75\( \)\mathrm{kg} / \mathrm{s}\( with cold water \)\left(c_{p}=4.18 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\( that enters the heat exchanger at \)20^{\circ} \mathrm{C}$ at a rate of \(0.6 \mathrm{~kg} / \mathrm{s}\). If the overall heat transfer coefficient is \(800 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), the heat transfer area of the heat exchanger is (a) \(0.745 \mathrm{~m}^{2}\) (b) \(0.760 \mathrm{~m}^{2}\) (c) \(0.775 \mathrm{~m}^{2}\) (d) \(0.790 \mathrm{~m}^{2}\) (e) \(0.805 \mathrm{~m}^{2}\)

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.

Saturated water vapor at \(100^{\circ} \mathrm{C}\) condenses in the shell side of a one-shell and two-tube heat exchanger with a surface area of $0.5 \mathrm{~m}^{2}\( and an overall heat transfer coefficient of \)2000 \mathrm{~W} / \mathrm{m}^{2}\(. \)\mathrm{K}\(. If cold water \)\left(c_{p c}=4179 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right.\( ) flowing at \)0.5 \mathrm{~kg} / \mathrm{s}\( enters the tube side at \)15^{\circ} \mathrm{C}$, determine the outlet temperature of the cold water and the heat transfer rate for the heat exchanger.

An air-cooled condenser is used to condense isobutane in a binary geothermal power plant. The isobutane is condensed at \(85^{\circ} \mathrm{C}\) by air \(\left(c_{p}=1.0 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right.\) ) that enters at \(22^{\circ} \mathrm{C}\) at a rate of \(18 \mathrm{~kg} / \mathrm{s}\). The overall heat transfer coefficient and the surface area for this heat exchanger are \(2.4 \mathrm{~kW} / \mathrm{m}^{2} \cdot \mathrm{K}\) and $2.6 \mathrm{~m}^{2}$, respectively. The outlet temperature of the air is (a) \(35.6^{\circ} \mathrm{C}\) (b) \(40.5^{\circ} \mathrm{C}\) (c) \(52.1^{\circ} \mathrm{C}\) (d) \(58.5^{\circ} \mathrm{C}\) (e) \(62.8^{\circ} \mathrm{C}\)

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