Hot exhaust gases of a stationary diesel engine are to be used to generate steam in an evaporator. Exhaust gases \(\left(c_{p}=1051 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) enter the heat exchanger at \(550^{\circ} \mathrm{C}\) at a rate of \(0.25 \mathrm{~kg} / \mathrm{s}\) while water enters as saturated liquid and evaporates at \(200^{\circ} \mathrm{C}\left(h_{f g}=1941 \mathrm{~kJ} / \mathrm{kg}\right)\). The heat transfer surface area of the heat exchanger based on water side is \(0.5 \mathrm{~m}^{2}\) and overall heat transfer coefficient is \(1780 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Determine the rate of heat transfer, the exit temperature of exhaust gases, and the rate of evaporation of water.

Short Answer

Expert verified
Question: Calculate the rate of heat transfer, the exit temperature of the exhaust gases, and the rate of evaporation of water in an evaporator heat exchanger given the following information: overall heat transfer coefficient (U), heat transfer surface area (A), initial temperature of the exhaust gas (T_in), mass flow rate of the exhaust gas (m), and specific heat capacity of the exhaust gas (c_p).

Step by step solution

01

Use the heat transfer formula to find the rate of heat transfer

The heat transfer equation is given by: \(q = UA(T_{in} - T_{out})\), where \(q\) is the rate of heat transfer, \(U\) is the overall heat transfer coefficient, \(A\) is the heat transfer surface area, \(T_{in}\) is the initial temperature and \(T_{out}\) is the final temperature. We have the values for \(U\), \(A\), and \(T_{in}\). We need to find \(q\) and \(T_{out}\). First, let's find \(q\). We can rewrite the heat transfer equation as: \(q = mA(T_{in} - T_{out})=m_water \times h_{fg}\), where \(m\) is the mass flow rate of the exhaust gas, \(A\) is the specific heat capacity of exhaust gas, \(T_{in}\) is the initial temperature of exhaust gas, \(T_{out}\) is the final temperature of exhaust gas, and \(m_water\) and \(h_{fg}\) are (respectively) the mass flow rate of water and the specific enthalpy of water. Rearrange the equation to solve for \(q\): \(q = \frac{m_water \times h_{fg}}{A}\).
02

Find the change in temperature of exhaust gases

Solve the equation we found in step 1 for \(m_water\): \(m_water = \frac{q}{h_{fg}}\). Now we can use the heat transfer equation to find the change in temperature of the exhaust gases: \(\Delta T = T_{in} - T_{out} = \frac{q}{mc_p}\).
03

Calculate the exit temperature of exhaust gases

To find the final temperature of the exhaust gases (\(T_{out}\)), we can subtract the change in temperature (\(\Delta T\)) found in step 2 from the initial temperature (\(T_{in}\)): \(T_{out} = T_{in} - \Delta T\).
04

Calculate the rate of evaporation of water

Now, we can calculate the rate of evaporation of water by using the equation from step 1 and the heat transfer equation we used in step 2: \(Rate\ of\ evaporation = \frac{m_water}{\Delta T} = \frac{q}{h_{fg}\Delta T}\).

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Most popular questions from this chapter

A 1 -shell and 2-tube type heat exchanger has an overall heat transfer coefficient of \(300 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2} \cdot{ }^{\circ} \mathrm{F}\). The shell side fluid has a heat capacity rate of \(20,000 \mathrm{Btu} / \mathrm{h} \cdot{ }^{\circ} \mathrm{F}\), while the tube side fluid has a heat capacity rate of \(40,000 \mathrm{Btu} / \mathrm{h} \cdot{ }^{\circ} \mathrm{F}\). The inlet temperatures on the shell side and tube side are \(200^{\circ} \mathrm{F}\) and \(90^{\circ} \mathrm{F}\), respectively. If the total heat transfer area is \(100 \mathrm{ft}^{2}\), determine \((a)\) the heat transfer effectiveness and \((b)\) the actual heat transfer rate in the heat exchanger.

Reconsider Prob. 11-131. Using EES (or other) software, plot the number of tube passes as a function of water velocity as it varies from \(1 \mathrm{~m} / \mathrm{s}\) to \(8 \mathrm{~m} / \mathrm{s}\), and discuss the results.

Can the temperature of the cold fluid rise above the inlet temperature of the hot fluid at any location in a heat exchanger? Explain.

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 \(c_{p h}=4188 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\).

Consider a heat exchanger that has an NTU of 4 . Someone proposes to double the size of the heat exchanger and thus double the NTU to 8 in order to increase the effectiveness of the heat exchanger and thus save energy. Would you support this proposal?

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