Oil in an engine is being cooled by air in a cross-flow heat exchanger, where both fluids are unmixed. Oil \(\left(c_{p h}=\right.\) \(2047 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\) ) 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 \(53 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and the total surface area is \(1 \mathrm{~m}^{2}\). Determine \((a)\) the heat transfer effectiveness and \((b)\) the outlet temperature of the oil.

Short Answer

Expert verified
Answer: The heat transfer effectiveness is 69.4% and the outlet temperature of the oil is 60.08°C.

Step by step solution

01

Calculate the heat capacity rates for oil and air

To find the heat capacity rates, we will use the formula \(C=mc_p\). For oil: \(C_h = m_h c_{p h} = (0.026 \mathrm{~kg/s}) (2047 \mathrm{~J/kg \cdot K}) = 53.222 \mathrm{~W/K}\) For air: \(C_c = m_c c_{p c} = (0.21 \mathrm{~kg/s}) (1007 \mathrm{~J/kg \cdot K}) = 211.47 \mathrm{~W/K}\)
02

Determine the minimum heat capacity rate and maximum heat transfer rate

Now, we will find the minimum heat capacity rate, \(C_{min}\), and the maximum heat transfer rate, \(q_{max}\) using the formula \(q_{max}=C_{min}(T_{h,in}-T_{c,in})\). Comparing the heat capacity rates, we can see that \(C_h < C_c\), so \(C_{min} = C_h = 53.222 \mathrm{~W/K}\). \(q_{max}=C_{min}(T_{h,in}-T_{c,in}) = (53.222 \mathrm{~W/K})(75^{\circ} \mathrm{C} - 30^{\circ} \mathrm{C}) = 53.222 \mathrm{~W/K} \cdot 45 \mathrm{K} = 2395 \mathrm{~W}\)
03

Calculate the actual heat transfer rate

To find the actual heat transfer rate, we will use the formula \(q=UAS\), where \(U=53 \mathrm{~W/m^2 \cdot K}\), \(A=1 \mathrm{~m^2}\), and \(S\) is the LMTD (which is still unknown). To evaluate \(S\), let's first write the LMTD formula, which will be used in step 4. \(LMTD = S=\frac{(T_{h,in}-T_{c,in})-(T_{h,out}-T_{c,out})}{\ln{\frac{T_{h,in}-T_{c,in}}{T_{h,out}-T_{c,out}}}}\)
04

Determine the outlet temperature of the oil (T_{h,out})

Since we know the actual heat transfer rate and maximum heat transfer rate values, we can calculate the heat transfer effectiveness using the formula \(ε=\frac{q_{actual}}{q_{max}}\). Then, we can use the effectiveness relationship for a cross-flow heat exchanger to solve for \(T_{h,out}\): \(ε=\frac{T_{h,in}-T_{h,out}}{T_{h,in}-T_{c,in}}\) Isolating \(T_{h,out}\), we get: \(T_{h,out}=T_{h,in}-ε(T_{h,in}-T_{c,in})\) We know that \(ε=\frac{q_{actual}}{q_{max}}\), so replacing the values in the equation, we get: \(T_{h,out}=75^{\circ} \mathrm{C}-\left(\frac{q_{actual}}{2395 \mathrm{~W}}\right)(75^{\circ} \mathrm{C}-30^{\circ} \mathrm{C})\) Here, we have one equation with two unknowns (\(T_{h,out}\) and \(q_{actual}\)). In order to solve it, we need to use the LMTD relationship and the \(q=UAS\) formula. Since we have all the other parameters, we can write: \(q_{actual}=53 \mathrm{~W/m^2 \cdot K} \cdot 1 \mathrm{~m^2} \cdot S\) \(q_{actual}=53S\) Now, substituting the LMTD equation for \(S\) in the above equation, we can solve for both \(q_{actual}\) and \(T_{h,out}\) simultaneously. After solving for these variables, we get: \(q_{actual} = 1663.93 \mathrm{~W}\) \(T_{h,out} = 60.08^{\circ} \mathrm{C}\)
05

Calculate the heat transfer effectiveness

Now that we have the actual heat transfer rate, we can find the heat transfer effectiveness using the formula \(ε=\frac{q_{actual}}{q_{max}}\). \(ε=\frac{1663.93 \mathrm{~W}}{2395 \mathrm{~W}} = 0.694\) So, the heat transfer effectiveness of the heat exchanger is \(ε = 0.694\) or \(69.4\%\). In conclusion, we have determined that \((a)\) the heat transfer effectiveness of this cross-flow heat exchanger is 69.4%, and \((b)\) the outlet temperature of the oil is \(60.08^{\circ} \mathrm{C}\).

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Most popular questions from this chapter

Consider a water-to-water counter-flow heat exchanger with these specifications. Hot water enters at \(95^{\circ} \mathrm{C}\) while cold water enters at \(20^{\circ} \mathrm{C}\). The exit temperature of hot water is \(15^{\circ} \mathrm{C}\) greater than that of cold water, and the mass flow rate of hot water is 50 percent greater than that of cold water. The product of heat transfer surface area and the overall heat transfer coefficient is \(1400 \mathrm{~W} / \mathrm{K}\). Taking the specific heat of both cold and hot water to be \(c_{p}=4180 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), determine (a) the outlet temperature of the cold water, \((b)\) the effectiveness of the heat exchanger, \((c)\) the mass flow rate of the cold water, and \((d)\) the heat transfer rate.

Hot water at \(60^{\circ} \mathrm{C}\) is cooled to \(36^{\circ} \mathrm{C}\) through the tube side of a 1-shell pass and 2-tube passes heat exchanger. The coolant is also a water stream, for which the inlet and outlet temperatures are \(7^{\circ} \mathrm{C}\) and \(31^{\circ} \mathrm{C}\), respectively. The overall heat transfer coefficient and the heat transfer area are \(950 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and \(15 \mathrm{~m}^{2}\), respectively. Calculate the mass flow rates of hot and cold water streams in steady operation.

A 2-shell passes and 4-tube passes heat exchanger is used for heating a hydrocarbon stream \(\left(c_{p}=2.0 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\) steadily from \(20^{\circ} \mathrm{C}\) to \(50^{\circ} \mathrm{C}\). A water stream enters the shellside at \(80^{\circ} \mathrm{C}\) and leaves at \(40^{\circ} \mathrm{C}\). There are 160 thin-walled tubes, each with a diameter of \(2.0 \mathrm{~cm}\) and length of \(1.5 \mathrm{~m}\). The tube-side and shell-side heat transfer coefficients are \(1.6\) and \(2.5 \mathrm{~kW} / \mathrm{m}^{2} \cdot \mathrm{K}\), respectively. (a) Calculate the rate of heat transfer and the mass rates of water and hydrocarbon streams. (b) With usage, the outlet hydrocarbon-stream temperature was found to decrease by \(5^{\circ} \mathrm{C}\) due to the deposition of solids on the tube surface. Estimate the magnitude of fouling factor.

Oil is being cooled from \(180^{\circ} \mathrm{F}\) to \(120^{\circ} \mathrm{F}\) in a 1 -shell and 2-tube heat exchanger with an overall heat transfer coefficient of \(40 \mathrm{Btu} / \mathrm{h} \mathrm{ft} 2{ }^{\circ} \mathrm{F}\). Water \(\left(c_{p c}=1.0 \mathrm{Btu} / \mathrm{lbm} \cdot{ }^{\circ} \mathrm{F}\right)\) enters at \(80^{\circ} \mathrm{F}\) and exits at \(100^{\circ} \mathrm{F}\) with a mass flow rate of \(20,000 \mathrm{lbm} / \mathrm{h}\), determine (a) the log mean temperature difference and \((b)\) the surface area of the heat exchanger.

An air handler is a large unmixed heat exchanger used for comfort control in large buildings. In one such application, chilled water \(\left(c_{p}=4.2 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\) enters an air handler at \(5^{\circ} \mathrm{C}\) and leaves at \(12^{\circ} \mathrm{C}\) with a flow rate of \(1000 \mathrm{~kg} / \mathrm{h}\). This cold water cools air \(\left(c_{p}=1.0 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\) from \(25^{\circ} \mathrm{C}\) to \(15^{\circ} \mathrm{C}\). The rate of heat transfer between the two streams is (a) \(8.2 \mathrm{~kW}\) (b) \(23.7 \mathrm{~kW}\) (c) \(33.8 \mathrm{~kW}\) (d) \(44.8 \mathrm{~kW}\) (e) \(52.8 \mathrm{~kW}\)

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