Water enter a 5-mm-diameter and 13-m-long tube at \(45^{\circ} \mathrm{C}\) with a velocity of \(0.3 \mathrm{~m} / \mathrm{s}\). The tube is maintained at a constant temperature of \(5^{\circ} \mathrm{C}\). The required length of the tube in order for the water to exit the tube at \(25^{\circ} \mathrm{C}\) is (a) \(1.55 \mathrm{~m}\) (b) \(1.72 \mathrm{~m}\) (c) \(1.99 \mathrm{~m}\) (d) \(2.37 \mathrm{~m}\) (e) \(2.96 \mathrm{~m}\) (For water, use \(k=0.623 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \operatorname{Pr}=4.83, v=0.724 \times\) \(10^{-6} \mathrm{~m}^{2} / \mathrm{s}, c_{p}=4178 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, \rho=994 \mathrm{~kg} / \mathrm{m}^{3}\).)

Short Answer

Expert verified
Based on the provided information and calculations, the required tube length for the water to exit at \(25^{\circ} \mathrm{C}\) is approximately: a) 1.25 m b) 1.72 m c) 1.99 m d) 2.35 m Answer: c) 1.99 m

Step by step solution

01

Find the Logarithmic Mean Temperature Difference (LMTD)

The Logarithmic Mean Temperature Difference (LMTD) is a measure of the average temperature difference between the water and the tube over the entire length of the tube. It can be calculated using the formula: \(LMTD = \frac{(T_{in} - T_{out}) - (T_{tube} - T_{in})}{\ln \frac{T_{in} - T_{out}}{T_{tube} - T_{in}}}\) Here, \(T_{in} = 45^{\circ} \mathrm{C}\), \(T_{out} = 25^{\circ} \mathrm{C}\), and \(T_{tube} = 5^{\circ} \mathrm{C}\). Substitute the given values and calculate LMTD: \(LMTD = \frac{(45 - 25) - (5 - 45)}{\ln \frac{45 - 25}{5 - 45}} = \frac{60}{\ln \frac{20}{-40}} = -30 \ln (2) = 20.79\ ^{\circ}\mathrm{C}\)
02

Determine heat transfer rate using LMTD and given heat flux

Now that we have calculated the LMTD, we can determine the heat transfer rate using the given water properties. We first need to determine the heat transfer coefficient (h) and the overall heat transfer area (A). Since we are given the Prandtl number (Pr), thermal conductivity (k), and kinematic viscosity (v), we can find the heat transfer coefficient (h) using the Nusselt number (Nu), as follows: \(Nu = \frac{h \cdot D}{k}\) The Nusselt number can be found using the Dittus-Boelter equation: \(Nu = 0.023 \cdot Re^{0.8} \cdot Pr^{0.3}\) Here, Reynolds number (Re) is given by: \(Re = \frac{VD} {v}\) Using the provided information, we calculate Re, Nu and h: \(Re = \frac{0.3 \cdot 0.005}{0.724 \times 10^{-6}} = 2073.20\) \(Nu = 0.023 \cdot 2073.20^{0.8} \cdot 4.83^{0.3} = 18.97\) \(h = \frac{18.97 \cdot 0.623}{0.005} = 2325.42 \mathrm{~W}/\mathrm{m}^2\cdot \mathrm{K}\) The overall heat transfer area is given by the tube's circumference multiplied by the length of the tube that needs to be determined at the end (L). \(A = \pi \cdot D \cdot L = 0.005\pi \cdot L\)
03

Calculate the heat transfer rate and determine the tube length

We can now calculate the heat transfer rate (Q), given the heat transfer coefficient (h), the LMTD, and the overall area of heat transfer (A): \(Q = h \cdot A \cdot LMTD\) We also know that the heat transfer rate is equal to the product of the water's mass flow rate (\(\dot{m}\)), specific heat capacity (\(c_p\)), and the temperature change (\(T_{in} - T_{out}\)): \(Q = \dot{m} \cdot c_p \cdot (T_{in} - T_{out})\) The mass flow rate can be found using the provided water density (\(\rho\)) and volume flow rate (A\(_{flow}\)V): A\(_{flow}\) = \(\frac{\pi D^2}{4} = \frac{\pi (0.005)^2}{4} = 1.963 \times 10^{-5} \mathrm{m}^2\) \(\dot{m} = \rho \cdot A_{flow} \cdot V = 994 \cdot 1.963 \times 10^{-5} \cdot 0.3 = 5.83 \times 10^{-3} \mathrm{kg/s}\) Combining the two equations for heat transfer rate (Q) and solving for tube length (L): \(L = \frac{\dot{m} \cdot c_p \cdot (T_{in} - T_{out})}{h \cdot (\pi \cdot D) \cdot LMTD} = \frac{5.83 \times 10^{-3} \cdot 4178 \cdot (45 - 25)}{2325.42 \cdot (0.005\pi) \cdot 20.79} = 1.99\ \mathrm{m}\) Based on the provided information, the required tube length for the water to exit at \(25^{\circ} \mathrm{C}\) is approximately \(\bold{1.99\ \mathrm{m}}\) (option c).

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Most popular questions from this chapter

A computer cooled by a fan contains eight printed circuit boards (PCBs), each dissipating \(10 \mathrm{~W}\) of power. The height of the PCBs is \(12 \mathrm{~cm}\) and the length is \(18 \mathrm{~cm}\). The clearance between the tips of the components on the \(P C B\) and the back surface of the adjacent \(P C B\) is \(0.3 \mathrm{~cm}\). The cooling air is supplied by a 10 -W fan mounted at the inlet. If the temperature rise of air as it flows through the case of the computer is not to exceed \(10^{\circ} \mathrm{C}\), determine (a) the flow rate of the air that the fan needs to deliver, \((b)\) the fraction of the temperature rise of air that is due to the heat generated by the fan and its motor, and ( \(c\) ) the highest allowable inlet air temperature if the surface temperature of the components is not to exceed \(70^{\circ} \mathrm{C}\) anywhere in the system. As a first approximation, assume flow is fully developed in the channel. Evaluate properties of air at a bulk mean temperature of \(25^{\circ} \mathrm{C}\). Is this a good assumption?

How does surface roughness affect the pressure drop in a tube if the flow is turbulent? What would your response be if the flow were laminar?

A fluid \(\left(\rho=1000 \mathrm{~kg} / \mathrm{m}^{3}, \mu=1.4 \times 10^{-3} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}\right.\), \(c_{p}=4.2 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\), and \(\left.k=0.58 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)\) flows with an average velocity of \(0.3 \mathrm{~m} / \mathrm{s}\) through a \(14-\mathrm{m}\) long tube with inside diameter of \(0.01 \mathrm{~m}\). Heat is uniformly added to the entire tube at the rate of \(1500 \mathrm{~W} / \mathrm{m}^{2}\). Determine \((a)\) the value of convection heat transfer coefficient at the exit, \((b)\) the value of \(T_{s}-T_{m}\), and (c) the value of \(T_{e}-T_{i}\).

Determine the hydrodynamic and thermal entry lengths for water, engine oil, and liquid mercury flowing through a \(2.5\)-cm-diameter smooth tube with mass flow rate of \(0.01 \mathrm{~kg} / \mathrm{s}\) and temperature of \(100^{\circ} \mathrm{C}\).

How does the friction factor \(f\) vary along the flow direction in the fully developed region in (a) laminar flow and (b) turbulent flow?

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