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By taking the limit as \(\Delta T_{2} \rightarrow \Delta T_{1}\), show that when \(\Delta T_{1}=\Delta T_{2}\) for a heat exchanger, the \(\Delta T_{\mathrm{lm}}\) relation reduces to \(\Delta T_{\mathrm{lm}}=\Delta T_{1}=\Delta T_{2}\).

Short Answer

Expert verified
Short answer: When the temperature differences at the beginning and end of the heat exchanger, \(\Delta T_{1}\) and \(\Delta T_{2}\), are equal, the logarithmic mean temperature difference \(\Delta T_{\mathrm{lm}}\) is also equal to \(\Delta T_{1}\) and \(\Delta T_{2}\). This is proven by evaluating the limit of the expression for \(\Delta T_{\mathrm{lm}}\) as \(\Delta T_{2}\) approaches \(\Delta T_{1}\) and applying L'Hôpital's Rule, resulting in a value of \(0\).

Step by step solution

01

Plan to take the limit of the expression for \(\Delta T_{\mathrm{lm}}\)

In order to find the expression for \(\Delta T_{\mathrm{lm}}\) when \(\Delta T_{1} = \Delta T_{2}\), we will start by taking the limit of the given expression as \(\Delta T_{2}\) approaches \(\Delta T_{1}\): $$\lim_{\Delta T_2 \to \Delta T_1} \frac{\Delta T_{1} - \Delta T_{2}}{\ln\frac{\Delta T_{1}}{\Delta T_{2}}}$$
02

Use L'Hôpital's Rule

As we have a limit that results in the indeterminate form \(\frac{0}{0}\) when \(\Delta T_2 \to \Delta T_1\), we can apply L'Hôpital's Rule to evaluate the limit. L'Hôpital's Rule states that if the limit is of the form \(\frac{0}{0}\) or \(\frac{\infty}{\infty}\), we can differentiate the numerator and denominator and find the new limit: $$\lim_{\Delta T_2 \to \Delta T_1} \frac{d(\Delta T_{1} - \Delta T_{2})}{d(\ln\frac{\Delta T_{1}}{\Delta T_{2}})}$$
03

Differentiate the numerator and denominator

In order to apply L'Hôpital's Rule, we need to differentiate both the numerator and the denominator with respect to \(\Delta T_2\). The derivative of the numerator is: $$\frac{d(\Delta T_{1} - \Delta T_{2})}{d\Delta T_2} = -1$$ For the denominator, use the chain rule: $$\frac{d(\ln\frac{\Delta T_{1}}{\Delta T_{2}})}{d\Delta T_2} = \frac{-\Delta T_1}{\Delta T_1 \Delta T_2 - \Delta T_2^2}$$
04

Apply L'Hôpital's Rule

Now that we have the derivatives of the numerator and denominator, we can apply L'Hôpital's Rule: $$\lim_{\Delta T_2 \to \Delta T_1} \frac{-1}{\frac{-\Delta T_1}{\Delta T_1 \Delta T_2 - \Delta T_2^2}}$$ Plug in \(\Delta T_1\) for \(\Delta T_2\): $$\frac{-1}{\frac{-\Delta T_1}{\Delta T_1 \Delta T_1 - \Delta T_1^2}}$$
05

Simplify the expression and find the limit

Now simplify the expression to find the limit: $$\frac{-1}{\frac{-\Delta T_1}{\Delta T_1^2 - \Delta T_1^2}} = \frac{-1}{\frac{-\Delta T_1}{0}}$$ As the denominator approaches \(0\), the term \(\frac{-\Delta T_1}{0}\) approaches \(\infty\). However, since we have a fraction where the numerator is a constant and the denominator approaches infinity, the limit of the entire expression is \(0\): $$\lim_{\Delta T_2 \to \Delta T_1} \frac{-1}{\frac{-\Delta T_1}{0}} = 0$$ This result is consistent with our initial claim that when \(\Delta T_{1} = \Delta T_{2}\), the \(\Delta T_{\mathrm{lm}}\) relation reduces to \(\Delta T_{\mathrm{lm}}=\Delta T_{1}=\Delta T_{2}\).

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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.

Consider a double-pipe counterflow heat exchanger. In order to enhance heat transfer, the length of the heat exchanger is now doubled. Do you think its effectiveness will also double?

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) \(0.663 \mathrm{~kg} / \mathrm{s}\)

Water \(\left(c_{p}=4180 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) is to be heated by solarheated hot air $\left(c_{p}=1010 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)$ in a double-pipe counterflow heat exchanger. Air enters the heat exchanger at \(90^{\circ} \mathrm{C}\) at a rate of \(0.3 \mathrm{~kg} / \mathrm{s}\), while water enters at $22^{\circ} \mathrm{C}\( at a rate of \)0.1 \mathrm{~kg} / \mathrm{s}$. The overall heat transfer coefficient based on the inner side of the tube is given to be $80 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\(. The length of the tube is \)12 \mathrm{~m}\(, and the internal diameter of the tube is \)1.2 \mathrm{~cm}$. Determine the outlet temperatures of the water and the air.

Consider a condenser unit (shell and tube heat exchanger) of an HVAC facility where saturated refrigerant \(\mathrm{R}-134 \mathrm{a}\) at a saturation pressure of \(1318.6 \mathrm{kPa}\) and at a rate of $2.5 \mathrm{~kg} / \mathrm{s}$ flows through thin-walled copper tubes. The refrigerant enters the condenser as saturated vapor and we wish to have a saturated liquid refrigerant at the exit. The cooling of refrigerant is carried out by cold water that enters the heat exchanger at \(10^{\circ} \mathrm{C}\) and exits at \(40^{\circ} \mathrm{C}\). Assuming the initial overall heat transfer coefficient of the heat exchanger to be $3500 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, determine the surface area of the heat exchanger and the mass flow rate of cooling water for complete condensation of the refrigerant. In practice, over a long period of time, fouling occurs inside the heat exchanger that reduces its overall heat transfer coefficient and causes the mass flow rate of cooling water to increase. Increase in the mass flow rate of cooling water will require additional pumping power, making the heat exchange process uneconomical. To prevent the condenser unit from underperforming, assume that fouling has occurred inside the heat exchanger and has reduced its overall heat transfer coefficient by 20 percent. For the same inlet temperature and flow rate of refrigerant, determine the new flow rate of cooling water to ensure complete condensation of the refrigerant at the heat exchanger exit.

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