/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 90 An electronic circuit board diss... [FREE SOLUTION] | 91Ó°ÊÓ

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An electronic circuit board dissipating \(50 \mathrm{~W}\) is sandwiched between two ducted, forced-air-cooled heat sinks. The sinks are \(150 \mathrm{~mm}\) in length and have 20 rectangular passages \(6 \mathrm{~mm} \times 25 \mathrm{~mm}\). Atmospheric air at a volumetric flow rate of \(0.060 \mathrm{~m}^{3} / \mathrm{s}\) and \(27^{\circ} \mathrm{C}\) is drawn through the sinks by a blower. Estimate the operating temperature of the board and the pressure drop across the sinks.

Short Answer

Expert verified
The operating temperature of the board is estimated to be \(47.1^{\circ} \mathrm{C}\), and the pressure drop across the sinks is \(198.0 \; Pa\).

Step by step solution

01

1. Determine the heat transfer coefficient

First, calculate the Reynolds number (Re) with the formula: \[Re = \dfrac{\rho v D_h}{\mu}\] where: - \(\rho\) is the air density, - \(v\) is the air velocity, - \(D_h\) is the hydraulic diameter, and - \(\mu\) is the air dynamic viscosity. To calculate Re, we need to find these variables first.
02

2. Calculate air density and dynamic viscosity

The air density \(\rho\) and dynamic viscosity \(\mu\) at the given air temperature can be found using empirical correlations or look-up tables. In this case, let's use the values for the standard atmosphere at 27°C: - \(\rho = 1.177 \; kg/m^3\) - \(\mu = 1.85 \times 10^{-5} \; kg/(m ⋅ s)\)
03

3. Calculate air velocity and hydraulic diameter

To find the air velocity (v), divide the volumetric flow rate by the total cross-sectional area of the passages: \[v = \dfrac{Q}{A_total}\] where: - \(Q = 0.060 \; m^3/s\) is the volumetric flow rate, and - \(A_{total}\) is the total cross-sectional area of the passages. To find the hydraulic diameter (Dh), use the formula: \[D_h = \dfrac{4A_{passage}}{P}\] where: - \(A_{passage}\) is the cross-sectional area of a single passage, and - \(P\) is the wetted perimeter of the passage.
04

4. Calculate the Reynolds number

With the values for air density, air velocity, hydraulic diameter, and air dynamic viscosity, calculate the Reynolds number, Re.
05

5. Calculate the heat transfer coefficient

Now, determine the heat transfer coefficient (h) based on the Reynold's number from step 4 using the appropriate correlation. For turbulent flow in a rectangular duct: \[h = 0.664 \times Pr^{1/3} \times Re^{1/2}\] where Pr is the Prandtl number.
06

6. Estimate the operating temperature

With the heat transfer coefficient, we can estimate the operating temperature of the board using the energy balance equation. \[Q_\text{dissipated} = h A (T_\text{operating} - T_\text{inlet})\] Here - \(Q_\text{dissipated} = 50 W\), the power dissipated by the board - \(A\) is the total heat transfer area - \(T_\text{operating}\) is the operating temperature of the board (the unknown variable) - \(T_\text{inlet} = 27°C\), the temperature of the inlet air Solve for the operating temperature T_operating.
07

7. Calculate the pressure drop

Use the Darcy-Weisbach equation to calculate the pressure drop across the sinks: \[\Delta P = f \dfrac{L}{D_h} \dfrac{1}{2} \rho v^2\] where: - ΔP is the pressure drop across the sinks - f is the Darcy friction factor - L is the length of the passages (150 mm) - \(D_h\) is the hydraulic diameter To find the Darcy friction factor (f), use the appropriate correlation based on the Reynolds number. Solve for the pressure drop ΔP and complete the problem.

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Key Concepts

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

Reynolds number
Reynolds number (\( Re \)) is an essential concept in fluid dynamics, describing the flow characteristics of a fluid. It helps predict whether the flow will be laminar or turbulent. In our case with the electronic circuit board, knowing the Reynolds number aids in understanding airflow through the heat sinks. It is calculated as follows:
  • \[ Re = \frac{\rho v D_h}{\mu} \]
Here:
  • \( \rho \): air density, which can be determined from standard conditions.
  • \( v \): air velocity, found by dividing the volumetric flow rate by the total cross-sectional area.
  • \( D_h \): hydraulic diameter, calculated based on the dimensions of the heat sink passages.
  • \( \mu \): dynamic viscosity of the air, obtainable from empirical or standard data tables.
The Reynolds number helps in identifying the nature of the flow. Low\( Re \)values indicate laminar flow, while high values signify turbulent flow. In practical applications, this distinction affects the design and performance of heat transfer systems.
Hydraulic diameter
The hydraulic diameter (\( D_h \)) is a key parameter used to simplify complex conduit geometries, like the rectangular passages in heat sinks, into a form more akin to circular pipes. It is particularly useful in calculating the behavior and efficiency of fluid flows within non-circular ducts. The equation is:
  • \[ D_h = \frac{4A_{passage}}{P} \]
Where:
  • \( A_{passage} \): Cross-sectional area of an individual passage, calculated by multiplying its width and height.
  • \( P \): The wetted perimeter, which is the perimeter of the section in contact with the fluid.
With known dimensions of a heat sink's passage, this formula converts the geometry to an equivalent circular diameter. The hydraulic diameter is crucial for determining other parameters like Reynolds number and pressure drop, facilitating the analysis of heat transfer and fluid flow through the system.
Darcy-Weisbach equation
The Darcy-Weisbach equation is a fundamental tool in fluid mechanics, providing a means to estimate the pressure drop across a duct system, which is critical in understanding fluid flow in heat sinks. The pressure drop (\( \Delta P \)) is calculated using:
  • \[ \Delta P = f \frac{L}{D_h} \frac{1}{2} \rho v^2 \]
Where:
  • \( f \): Darcy friction factor, a dimensionless coefficient depending on the flow characteristics, such as the Reynolds number.
  • \( L \): Length of the duct, measured along the direction of flow.
  • \( D_h \): Hydraulic diameter, describing the effective diameter of the duct.
  • \( \rho \): Density of the fluid, in this context, air.
  • \( v \): Velocity of the fluid.
The pressure drop influences the system's overall efficiency and is essential for ensuring that the heat sink effectively dissipates heat from the electronic components. Depending on the pressure drop, adjustments could be necessary to optimize cooling performance.
Heat transfer coefficient
The heat transfer coefficient (\( h \)) is an essential parameter in evaluating the rate at which heat is transferred from the electronic board to the surrounding air, through the heat sinks. It is influenced by the flow conditions of the air (laminar or turbulent), the properties of the fluid, and the configuration of the heat transfer surface. For turbulent flow in rectangular ducts, as in this scenario, a commonly used correlation is given by:
  • \[ h = 0.664 \times Pr^{1/3} \times Re^{1/2} \]
Where:
  • \( Pr \): Prandtl number, a dimensionless number in fluid dynamics.
  • \( Re \): Reynolds number.
The heat transfer coefficient is key to calculating how effectively the heat sink operates, determining its ability to maintain the electronic board's safe operating temperature. By establishing this coefficient, we can use energy balance equations to find the board's operating temperature and ensure it is within the desired operational limits, protecting the electronics from overheating.

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Most popular questions from this chapter

The surface of a 50 -mm-diameter, thin-walled tube is maintained at \(100^{\circ} \mathrm{C}\). In one case air is in cross flow over the tube with a temperature of \(25^{\circ} \mathrm{C}\) and a velocity of \(30 \mathrm{~m} / \mathrm{s}\). In another case air is in fully developed flow through the tube with a temperature of \(25^{\circ} \mathrm{C}\) and a mean velocity of \(30 \mathrm{~m} / \mathrm{s}\). Compare the heat flux from the tube to the air for the two cases.

A thick-walled, stainless steel (AISI 316) pipe of inside and outside diameters \(D_{i}=20 \mathrm{~mm}\) and \(D_{o}=40 \mathrm{~mm}\) is heated electrically to provide a uniform heat generation rate of \(\dot{q}=10^{6} \mathrm{~W} / \mathrm{m}^{3}\). The outer surface of the pipe is insulated, while water flows through the pipe at a rate of \(\dot{m}=0.1 \mathrm{~kg} / \mathrm{s}\).

Many of the solid surfaces for which values of the thermal and momentum accommodation coefficients have been measured are quite different from those used in micro- and nanodevices. Plot the Nusselt number \(N u_{D}\) associated with fully developed laminar flow with constant surface heat flux versus tube diameter for \(1 \mu \mathrm{m} \leq D \leq 1 \mathrm{~mm}\) and (i) \(\alpha_{s}=1, \alpha_{p}=1\), (ii) \(\alpha_{t}=0.1, \alpha_{p}=0.1\), (iii) \(\alpha_{t}=1, \alpha_{p}=0.1\), and (iv) \(\alpha_{t}=0.1, \alpha_{p}=1\). For tubes of what diameter do the accommodation coefficients begin to influence convection heat transfer? For which combination of \(\alpha_{t}\) and \(\alpha_{p}\) does the Nusselt number exhibit the least sensitivity to changes in the diameter of the tube? Which combination results in Nusselt numbers greater than the conventional fully developed laminar value for constant heat flux conditions, \(N u_{D}=4.36\) ? Which combination is associated with the smallest Nusselt numbers? What can you say about the ability to predict convection heat transfer coefficients in a small-scale device if the accommodation coefficients are not known for material from which the device is fabricated? Use properties of air at atmospheric pressure and \(T=300 \mathrm{~K}\).

Slug flow is an idealized tube flow condition for which the velocity is assumed to be uniform over the entire tube cross section. For the case of laminar slug flow with a uniform surface heat flux, determine the form of the fully developed temperature distribution \(T(r)\) and the Nusselt number \(N u_{D}\).

Fluid enters a tube with a flow rate of \(0.015 \mathrm{~kg} / \mathrm{s}\) and an inlet temperature of \(20^{\circ} \mathrm{C}\). The tube, which has a length of \(6 \mathrm{~m}\) and diameter of \(15 \mathrm{~mm}\), has a surface temperature of \(30^{\circ} \mathrm{C}\). (a) Determine the heat transfer rate to the fluid if it is water. (b) Determine the heat transfer rate for the nanofluid of Example 2.2.

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