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An air duct heater consists of an aligned array of electrical heating elements in which the longitudinal and transverse pitches are \(S_{L}=S_{T}=24 \mathrm{~mm}\). There are 3 rows of elements in the flow direction \(\left(N_{L}=3\right)\) and 4 elements per row \(\left(N_{T}=4\right)\). Atmospheric air with an upstream velocity of \(12 \mathrm{~m} / \mathrm{s}\) and a temperature of \(25^{\circ} \mathrm{C}\) moves in cross flow over the elements, which have a diameter of \(12 \mathrm{~mm}\), a length of \(250 \mathrm{~mm}\), and are maintained at a surface temperature of \(350^{\circ} \mathrm{C}\). (a) Determine the total heat transfer to the air and the temperature of the air leaving the duct heater. (b) Determine the pressure drop across the element bank and the fan power requirement. (c) Compare the average convection coefficient obtained in your analysis with the value for an isolated (single) element. Explain the difference between the results. (d) What effect would increasing the longitudinal and transverse pitches to \(30 \mathrm{~mm}\) have on the exit temperature of the air, the total heat rate, and the pressure drop?

Short Answer

Expert verified
In summary, to analyze the given air duct heater, we first calculated the total heat transfer and exit air temperature by determining the Reynolds number, Nusselt number, convection heat transfer coefficient, and using heat transfer relations. Next, we calculated the pressure drop across the element bank and the fan power requirement using resistance factors and Bernoulli's equation. We compared average convection coefficients for an isolated element and the array, discussing the effects of neighboring elements and flow patterns. Lastly, we analyzed the effects of increasing longitudinal and transverse pitches on exit temperature, heat rate, and pressure drop by repeating the calculations with updated pitches and comparing the results, discussing the changes in heat transfer and pressure drop based on increased spacing and flow characteristics.

Step by step solution

01

a) Total Heat Transfer and Exit Air Temperature

We'll use the following steps to determine the total heat transfer and the temperature of the air leaving the duct heater. 1. Calculate the Reynolds number for the flow over the elements, using the given air velocity and diameter. Use the air properties at the film temperature, which is the average of the air and surface temperatures: \[ Re = \frac{Ud}{\nu} \] 2. Calculate the Nusselt number using an appropriate correlation, such as the Zukauskas correlation for crossflow over tubes: \[ Nu = CRe^mPr^n \left(\frac{Pr}{Pr_s}\right)^{0.25} \] 3. Calculate the convection heat transfer coefficient, h, using the Nusselt number and thermal conductivity of the air: \[ h = \frac{kNu}{d} \] 4. Calculate the total heat transfer from the element array, Q, by multiplying the convection heat transfer coefficient by the total heat transfer area and the temperature difference between the surface and the air: \[ Q = hA_s(T_s - T_a) \] 5. Determine the exit air temperature using the heat transfer calculated and an appropriate heat transfer relation: \[ T_{a,exit} = T_{a} + \frac{Q}{\dot{m}c_p} \]
02

b) Pressure Drop and Fan Power Requirement

We'll use the following steps to determine the pressure drop across the element bank and the fan power requirement. 1. Calculate the resistance factor, K, for the flow through the element bank. For a regular element array, use a suitable correlation like the Idelchick correlation: \[ K = K_1 + K_2\frac{1}{N_L}\] 2. Calculate the pressure drop across the element bank using Bernoulli's equation and the resistance factor calculated in step 1: \[ \Delta P = \frac{1}{2}\rho U^2 K \] 3. Compute the fan power requirement, P_fan, by multiplying the pressure drop by the volumetric flow rate and dividing it by the fan efficiency: \[ P_{fan} = \frac{\Delta P \dot{V}}{\eta_{fan}} \]
03

c) Comparing Convection Coefficients

To compare the average convection coefficients, calculate the coefficient for an isolated (single) element using the same process as in part a) but considering only one element. Explain the difference in the results based on the influence of neighboring elements in the array and possible changes in flow patterns.
04

d) Effect of Increasing Pitches on Exit Temperature, Heat Rate, and Pressure Drop

To determine the effect of increasing pitches on exit temperature, heat rate, and pressure drop, repeat parts a) and b) using the new longitudinal and transverse pitches of 30 mm. Compare the results with the original configuration and discuss the changes in heat transfer and pressure drop based on the increased spacing and flow characteristics.

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Reynolds Number Calculation
The Reynolds number is a crucial element in understanding how fluid flows over objects. It helps us determine the nature of the flow, whether it's laminar or turbulent. In the case of ducts and tubes, the Reynolds number, which is dimensionless, is calculated using the formula:\[ Re = \frac{Ud}{u} \]Here, \(U\) is the velocity of the fluid, \(d\) is the characteristic length (or diameter of the tubes), and \(u\) is the kinematic viscosity of the fluid. Kinematic viscosity is different for each fluid and varies with temperature, so it's important to use the average (or film) temperature when calculating this number. This temperature is the average of the air and the surface temperature, which gives a more accurate depiction of the fluid behavior.
  • Reynolds number below 2300 indicates laminar flow.
  • Reynolds number above 4000 indicates turbulent flow.
Understanding whether the flow is laminar or turbulent helps us predict how effectively the heat will be transferred to or from the flowing fluid.
Nusselt Number Correlations
The Nusselt number is a dimensionless number that relates to convective heat transfer. It allows us to find the convective heat transfer coefficient, which is essential for calculating the amount of heat transferred from the surface to the fluid. Calculating the Nusselt number accurately is fundamental to effective heat exchanger design. Zukauskas, among other correlations, is commonly used for calculating the Nusselt number in crossflow over tubes:\[ Nu = CRe^mPr^n \left(\frac{Pr}{Pr_s}\right)^{0.25} \]In this equation, \(Re\) is the Reynolds number, \(Pr\) is the Prandtl number of the fluid, and \(Pr_s\) is the Prandtl number at surface temperature. The constants \(C\), \(m\), and \(n\) are determined from empirical correlations based on the configuration of the array.
  • The Prandtl number, \(Pr\), is a measure of the fluid's thermal diffusivity, impacting heat transfer rate.
  • Choosing the correct correlation is vital. It depends on the geometry and alignment of the heat exchanger elements.
Pressure Drop in Heat Exchange Systems
Pressure drops within heat exchangers can significantly affect their efficiency and the power required to maintain flow through them. Calculating the pressure drop is crucial for ensuring the system operates efficiently. Let's break it down:The resistance factor \(K\) for an element array is determined using correlations like Idelchick's:\[ K = K_1 + K_2\frac{1}{N_L} \]The pressure drop \(\Delta P\) across the element bank is then calculated with:\[ \Delta P = \frac{1}{2}\rho U^2 K \]This formula incorporates the density \(\rho\) and velocity \(U\) of the fluid. The pressure drop influences the fan power requirements since overcoming this resistance is crucial for sustaining the fluid flow.
  • High pressure drop means more energy is needed to move the air through the duct.
  • Design considerations should aim to minimize pressure drop for cost-effectiveness.
Convection Heat Transfer
Convection is the heat transfer method that occurs through the movement of fluids. In the context of heat exchangers, convection transfers heat from a hot surface to cooler air moving past it. The effectiveness of this process depends on the convection heat transfer coefficient \(h\), which is found from the Nusselt number:\[ h = \frac{kNu}{d} \]Where \(k\) is the thermal conductivity of the fluid and \(d\) is the characteristic length, such as the diameter of the tubes.
Key factors influencing convection in ducts include:
  • Surface area: More surface exposure leads to better heat transfer.
  • Temperature difference: Greater differences enhance heat transfer.
  • Fluid velocity: Higher speeds generally improve convection efficiency.
Changes in surface roughness, temperature gradients, and flow velocity all impact the rate of heat transfer by convection. The design of the duct system needs to consider these factors to optimize the heat transfer process.

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Most popular questions from this chapter

Copper spheres of \(20-\mathrm{mm}\) diameter are quenched by being dropped into a tank of water that is maintained at \(280 \mathrm{~K}\). The spheres may be assumed to reach the terminal velocity on impact and to drop freely through the water. Estimate the terminal velocity by equating the drag and gravitational forces acting on the sphere. What is the approximate height of the water tank needed to cool the spheres from an initial temperature of \(360 \mathrm{~K}\) to a center temperature of \(320 \mathrm{~K}\) ?

A long, cylindrical, electrical heating element of diameter \(D=10 \mathrm{~mm}\), thermal conductivity \(k=240 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), density \(\rho=2700 \mathrm{~kg} / \mathrm{m}^{3}\), and specific heat \(c_{p}=900 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\) is installed in a duct for which air moves in cross flow over the heater at a temperature and velocity of \(27^{\circ} \mathrm{C}\) and \(10 \mathrm{~m} / \mathrm{s}\), respectively. (a) Neglecting radiation, estimate the steady-state surface temperature when, per unit length of the heater, electrical energy is being dissipated at a rate of \(1000 \mathrm{~W} / \mathrm{m}\). (b) If the heater is activated from an initial temperature of \(27^{\circ} \mathrm{C}\), estimate the time required for the surface temperature to come within \(10^{\circ} \mathrm{C}\) of its steady-state value.

An array of electronic chips is mounted within a sealed rectangular enclosure, and cooling is implemented by attaching an aluminum heat \(\operatorname{sink}(k=180 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\). The base of the heat sink has dimensions of \(w_{1}=w_{2}=\) \(100 \mathrm{~mm}\), while the 6 fins are of thickness \(t=10 \mathrm{~mm}\) and pitch \(S=18 \mathrm{~mm}\). The fin length is \(L_{f}=50 \mathrm{~mm}\), and the base of the heat sink has a thickness of \(L_{b}=10 \mathrm{~mm}\). If cooling is implemented by water flow through the heat sink, with \(u_{\infty}=3 \mathrm{~m} / \mathrm{s}\) and \(T_{\infty}=17^{\circ} \mathrm{C}\), what is the base temperature \(T_{b}\) of the heat sink when power dissipation by the chips is \(P_{\text {elec }}=1800 \mathrm{~W}\) ? The average convection coefficient for surfaces of the fins and the exposed base may be estimated by assuming parallel flow over a flat plate. Properties of the water may be approximated as \(k=0.62 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \rho=995 \mathrm{~kg} / \mathrm{m}^{3}\), \(c_{p}=4178 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, \nu=7.73 \times 10^{-7} \mathrm{~m}^{2} / \mathrm{s}\), and \(\operatorname{Pr}=5.2\).

The roof of a refrigerated truck compartment is of composite construction, consisting of a layer of foamed urethane insulation \(\left(t_{2}=50 \mathrm{~mm}, k_{i}=0.026 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)\) sandwiched between aluminum alloy panels \(\left(t_{1}=5 \mathrm{~mm}\right.\), \(\left.k_{p}=180 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)\). The length and width of the roof are \(L=10 \mathrm{~m}\) and W \(=3.5 \mathrm{~m}\), respectively, and the temperature of the inner surface is \(T_{s, i}=-10^{\circ} \mathrm{C}\). Consider conditions for which the truck is moving at a speed of \(V=105 \mathrm{~km} / \mathrm{h}\), the air temperature is \(T_{\infty}=32^{\circ} \mathrm{C}\), and the solar irradiation is \(G_{S}=750 \mathrm{~W} / \mathrm{m}^{2}\). Turbulent flow may be assumed over the entire length of the roof. (a) For equivalent values of the solar absorptivity and the emissivity of the outer surface \(\left(\alpha_{S}=\varepsilon=0.5\right)\), estimate the average temperature \(T_{s, o}\) of the outer surface. What is the corresponding heat load imposed on the refrigeration system? (b) A special finish \(\left(\alpha_{S}=0.15, \varepsilon=0.8\right)\) may be applied to the outer surface. What effect would such an application have on the surface temperature and the heat load? (c) If, with \(\alpha_{S}=\varepsilon=0.5\), the roof is not insulated \(\left(t_{2}=0\right)\), what are the corresponding values of the surface temperature and the heat load?

The use of rock pile thermal energy storage systems has been considered for solar energy and industrial process heat applications. A particular system involves a cylindrical container, \(2 \mathrm{~m}\) long by \(1 \mathrm{~m}\) in diameter, in which nearly spherical rocks of \(0.03-\mathrm{m}\) diameter are packed. The bed has a void space of \(0.42\), and the density and specific heat of the rock are \(\rho=2300 \mathrm{~kg} / \mathrm{m}^{3}\) and \(c_{p}=879 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), respectively. Consider conditions for which atmospheric air is supplied to the rock pile at a steady flow rate of \(1 \mathrm{~kg} / \mathrm{s}\) and a temperature of \(90^{\circ} \mathrm{C}\). The air flows in the axial direction through the container. If the rock is at a temperature of \(25^{\circ} \mathrm{C}\), what is the total rate of heat transfer from the air to the rock pile?

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