Engine oil \(\left(c_{p}=2100 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) is to be heated from \(20^{\circ} \mathrm{C}\) to \(60^{\circ} \mathrm{C}\) at a rate of \(0.3 \mathrm{~kg} / \mathrm{s}\) in a \(2-\mathrm{cm}\)-diameter thinwalled copper tube by condensing steam outside at a temperature of \(130^{\circ} \mathrm{C}\left(h_{f g}=2174 \mathrm{~kJ} / \mathrm{kg}\right)\). For an overall heat transfer coefficient of \(650 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the rate of heat transfer and the length of the tube required to achieve it.

Short Answer

Expert verified
Answer: The required length of the copper tube is approximately 7.045 meters.

Step by step solution

01

Calculate the mass flow rate of engine oil.

Given, the flow rate of engine oil is \(0.3\ kg/s\).
02

Determine the heat transfer required by the engine oil to raise its temperature.

To find the heat transfer required to raise the temperature of engine oil from \(20^\circ C\) to \(60^\circ C\), we can use the formula: \(Q=mc_p\Delta T\) Where \(Q\) is the heat transfer, \(m\) is the mass flow rate of engine oil, \(c_p\) is the specific heat capacity and \(\Delta T\) is the change in temperature. Given \(m=0.3\ kg/s\), \(c_p=2100\ J/kg\cdot K\), and \(\Delta T = 60-20 = 40^\circ C\). Therefore, \(Q = (0.3)(2100)(40)= 25200\ W\).
03

Calculate the rate of heat transfer between the steam and engine oil.

We are given the overall heat transfer coefficient U as \(650\ W/m^2\cdot K\). Also, we know \(Q=U\cdot A\cdot\Delta T_{lm}\) where the area A is given by \(A = \pi d L\) and \(\Delta T_{lm}\) is the log mean temperature difference. First, we need to calculate the log mean temperature difference. The outlet temperature of the engine oil is given as \(60^\circ C\). Since the steam is at a constant temperature, the inlet temperature difference can be calculated as \(\Delta T_1 = 130 - 60 = 70^\circ C\). Similarly, the outlet temperature difference is \(\Delta T_2 = 130 - 20 = 110^\circ C\). Now, we can find the log mean temperature difference: \(\Delta T_{lm} = \frac{\Delta T_2 - \Delta T_1}{\ln(\Delta T_2/\Delta T_1)}=\frac{110-70}{\ln(110/70)} = 87.25^\circ C\)
04

Find the length of the copper tube required for the desired heat transfer.

We have the rate of heat transfer \(Q=25200\ W\) and \(\Delta T_{lm}=87.25^\circ C\). We can now solve for the area, \(A\) \(A = \frac{Q}{U\cdot \Delta T_{lm}}=\frac{25200}{650\cdot 87.25}=0.443\ m^2\) Now, we can find the length of the copper tube. We know the diameter of the tube is \(2\ \mathrm{cm} = 0.02\ \mathrm{m}\) and the area \(A=0.443\ \mathrm{m}^2\). \(L = \frac{A}{\pi d}=\frac{0.443}{\pi\cdot 0.02}=7.045\ m\) So, the length of the copper tube required to achieve the desired rate of heat transfer is approximately \(7.045\ \mathrm{m}\).

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Most popular questions from this chapter

In a 1-shell and 2-tube heat exchanger, cold water with inlet temperature of \(20^{\circ} \mathrm{C}\) is heated by hot water supplied at the inlet at \(80^{\circ} \mathrm{C}\). The cold and hot water flow rates are \(5000 \mathrm{~kg} / \mathrm{h}\) and \(10,000 \mathrm{~kg} / \mathrm{h}\), respectively. If the shelland-tube heat exchanger has a \(U A_{s}\) value of \(11,600 \mathrm{~W} / \mathrm{K}\), determine the cold water and hot water outlet temperatures. Assume \(c_{p c}=4178 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\) and \(c_{p h}=4188 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\).

Saturated water vapor at \(100^{\circ} \mathrm{C}\) condenses in the shell side of a 1 -shell and 2-tube heat exchanger with a surface area of \(0.5 \mathrm{~m}^{2}\) and an overall heat transfer coefficient of \(2000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). 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.

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) \(50.0^{\circ} \mathrm{C}\)

Consider a shell-and-tube water-to-water heat exchanger with identical mass flow rates for both the hotand cold-water streams. Now the mass flow rate of the cold water is reduced by half. Will the effectiveness of this heat exchanger increase, decrease, or remain the same as a result of this modification? Explain. Assume the overall heat transfer coefficient and the inlet temperatures remain the same.

Steam is to be condensed on the shell side of a 2-shell-passes and 8-tube- passes condenser, with 20 tubes in each pass. Cooling water enters the tubes 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) \(1.0\)

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