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Ethylene glycol is heated from \(25^{\circ} \mathrm{C}\) to $40^{\circ} \mathrm{C}\( at a rate of \)2.5 \mathrm{~kg} / \mathrm{s}$ in a horizontal copper tube \((k=386 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) with an inner diameter of \(2.0 \mathrm{~cm}\) and an outer diameter of \(2.5 \mathrm{~cm}\). A saturated vapor \(\left(T_{g}=110^{\circ} \mathrm{C}\right)\) condenses on the outside-tube surface with the heat transfer coefficient (in $\mathrm{kW} / \mathrm{m}^{2} \cdot \mathrm{K}\( ) given by \)9.2 /\left(T_{g}-T_{w}\right)^{0.25}\(, where \)T_{n}$ is the average outside-tube wall temperature. What tube length must be used? Take the properties of ethylene glycol to be $\rho=1109 \mathrm{~kg} / \mathrm{m}^{3}, c_{p}=2428 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\(, \)k=0.253 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \mu=0.01545 \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}$, and \(\operatorname{Pr}=148.5\).

Short Answer

Expert verified
Answer: The main challenge in calculating the length of the tube in this scenario is that we have one equation with two unknowns (l and T_w), making it impossible to find an explicit value for the tube length without additional assumptions or simplification methods.

Step by step solution

01

Calculate the heat required to raise the temperature of the ethylene glycol

We will use the formula \(Q=m\cdot c_{p}\cdot \Delta T\), where \(Q\) is the heat required, \(m\) is the mass of the ethylene glycol, \(c_{p}\) is the specific heat capacity, and \(\Delta T\) is the difference in temperature. First, calculate the mass flow rate for \(2.5~kg/s\) and the temperature difference between \(25^{\circ}C\) and \(40^{\circ}C\). \(m=2.5~kg/s\) \(\Delta T=(40-25)^{\circ}C=15^{\circ}C\) Now, substitute these values into the formula to find the heat required: \(Q = (2.5~kg/s) \times (2428~J/kg\cdot K) \times (15~K) = 90825~W\)
02

Calculate the heat transfer between the ethylene glycol and the surrounding vapor

We are given the heat transfer coefficient \(h_{g}=\frac{9.2}{(T_{g}-T_{w})^{0.25}}\), where \(T_{g}\) is \(110^{\circ}C\) and \(T_{w}\) is the average outside-tube wall temperature. Let's find the heat transfer between the ethylene glycol and the surrounding vapor using the formula \(Q=h_{g}\cdot A\cdot \Delta T_{w_g}\), where \(A\) is the heat transfer area and \(\Delta T_{w_g}\) is the difference in temperature between inside and outside the tube. As we know the total heat required \(Q\), we can rearrange the formula to find the heat transfer area: \(A=\frac{Q}{h_{g}\cdot \Delta T_{w_g}}\) We need to express \(\Delta T_{w_g}\) in terms of \(T_{w}\), so we have: \(\Delta T_{w_g}=(T_{g}-T_{w})\) Now, substitute the values and rearrange the equation: \(A = \frac{90825~W}{\frac{9.2}{(110-T_{w})^{0.25}}\cdot (110-T_{w})}\)
03

Express heat transfer area in terms of the length of the tube

We can express the heat transfer area in terms of the length of the tube and the outer diameter of the tube: \(A=ld\pi\) where \(l\) is the length of the tube and \(d\) is the outer diameter of the tube. Substitute this expression into the equation obtained in step 2: \(l = \frac{90825~W}{\frac{9.2}{(110-T_{w})^{0.25}}\cdot (110-T_{w})\cdot (2.5\times10^{-2}m)\pi}\)
04

Calculate the length of the tube

As we only have one equation with two unknowns (\(l\) and \(T_w\)), it is not possible to find an explicit value for the tube lengths without some additional assumptions or simplification methods. It is possible to determine the tube length when given an appropriate assumption on \(T_w\).

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Most popular questions from this chapter

Consider a crossflow engine oil heater that uses ethylene glycol flowing at a temperature of \(110^{\circ} \mathrm{C}\) to heat the oil initially at \(10^{\circ} \mathrm{C}\). The ethylene glycol enters a tube bank consisting of copper tubes \((k=250 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) with staggered arrangement in a \(0.5-\mathrm{m} \times 0.5-\mathrm{m}\) plenum. The outside diameter of the \(0.5\)-m-long copper tubes is \(25 \mathrm{~mm}\), and the wall thickness is \(2 \mathrm{~mm}\). The longitudinal and transverse pitch of the rod bundles is \(0.035 \mathrm{~m}\) each. The engine oil to be heated flows inside the tubes with a mass flow rate of $4.05 \mathrm{~kg} / \mathrm{s}\(. Take the heat transfer coefficient of the oil to be \)2500 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. If the minimum desired exit temperature of oil is \(70^{\circ} \mathrm{C}\) and the measured exit temperature of ethylene glycol is \(90^{\circ} \mathrm{C}\), determine (a) the mass flow rate of ethylene glycol and \((b)\) the number of tube rows. In your calculation, use the following properties for the ethylene glycol.

A shell-and-tube heat exchanger with two shell passes and 12 tube passes is used to heat water $\left(c_{p}=4180 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( with ethylene glycol \)\left(c_{p}=2680 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\(. Water enters the tubes at \)22^{\circ} \mathrm{C}\( at a rate of \)0.8 \mathrm{~kg} / \mathrm{s}$ and leaves at \(70^{\circ} \mathrm{C}\). Ethylene glycol enters the shell at $110^{\circ} \mathrm{C}\( and leaves at \)60^{\circ} \mathrm{C}$. If the overall heat transfer coefficient based on the tube side is $280 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, determine the rate of heat transfer and the heat transfer surface area on the tube side.

A shell-and-tube heat exchanger with two shell passes and eight tube passes is used to heat ethyl alcohol $\left(c_{p}=2670 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( in the tubes from \)25^{\circ} \mathrm{C}\( to \)70^{\circ} \mathrm{C}\( at a rate of \)2.1 \mathrm{~kg} / \mathrm{s}$. The heating is to be done by water $\left(c_{p}=4190 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( that enters the shell at \)95^{\circ} \mathrm{C}$ and leaves at \(60^{\circ} \mathrm{C}\). If the overall heat transfer coefficient is $800 \mathrm{~W} / \mathrm{m}^{2} . \mathrm{K}$, determine the heat transfer surface area of the heat exchanger using \((a)\) the LMTD method and \((b)\) the \(\varepsilon-\mathrm{NTU}\) method. Answer: \((a) 11.4 \mathrm{~m}^{2}\)

Cold water $\left(c_{p}=4.18 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\( enters a counterflow heat exchanger at \)18^{\circ} \mathrm{C}\( at a rate of \)0.7 \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 $1.6 \mathrm{~kg} / \mathrm{s}\( and leaves at \)25^{\circ} \mathrm{C}$. The maximum possible outlet temperature of the cold water is (a) \(25.0^{\circ} \mathrm{C}\) (b) \(32.0^{\circ} \mathrm{C}\) (c) \(35.5^{\circ} \mathrm{C}\) (d) \(39.7^{\circ} \mathrm{C}\) (e) \(50.0^{\circ} \mathrm{C}\)

A heat exchanger is used to condense steam coming off the turbine of a steam power plant by cold water from a nearby lake. The cold water $\left(c_{p}=4.18 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)$ enters the condenser at \(16^{\circ} \mathrm{C}\) at a rate of \(42 \mathrm{~kg} / \mathrm{s}\) and leaves at \(25^{\circ} \mathrm{C}\), while the steam condenses at $45^{\circ} \mathrm{C}$. The condenser is not insulated, and it is estimated that heat at a rate of \(8 \mathrm{~kW}\) is lost from the condenser to the surrounding air. The rate at which the steam condenses is (a) \(0.228 \mathrm{~kg} / \mathrm{s}\) (b) \(0.318 \mathrm{~kg} / \mathrm{s}\) (c) \(0.426 \mathrm{~kg} / \mathrm{s}\) (d) \(0.525 \mathrm{~kg} / \mathrm{s}\) (e) \(0.663 \mathrm{~kg} / \mathrm{s}\)

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