/*! 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 106 You have been asked to determine... [FREE SOLUTION] | 91Ó°ÊÓ

91Ó°ÊÓ

You have been asked to determine the feasibility of using an impinging jet in a soldering operation for electronic assemblies. The schematic illustrates the use of a single, round nozzle to direct high-velocity, hot air to a location where a surface mount joint is to be formed. For your study, consider a round nozzle with a diameter of \(1 \mathrm{~mm}\) located a distance of \(2 \mathrm{~mm}\) from the region of the surface mount, which has a diameter of \(2.5 \mathrm{~mm}\). (a) For an air jet velocity of \(70 \mathrm{~m} / \mathrm{s}\) and a temperature of \(500^{\circ} \mathrm{C}\), estimate the average convection coefficient over the area of the surface mount. (b) Assume that the surface mount region on the printed circuit board (PCB) can be modeled as a semi-infinite medium, which is initially at a uniform temperature of \(25^{\circ} \mathrm{C}\) and suddenly experiences convective heating by the jet. Estimate the time required for the surface to reach \(183^{\circ} \mathrm{C}\). The thermophysical properties of a typical solder are \(\rho=8333 \mathrm{~kg} / \mathrm{m}^{3}, c_{p}=188 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), and \(k=\) \(51 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\).

Short Answer

Expert verified
The Reynolds number (Re) calculated for the given impinging jet conditions is approximately 6,013.81. Using an appropriate correlation for the impinging jet, the average convection coefficient (h) over the surface mount area is found to be approximately 344.88 W/(m²·K). Assuming the surface mount can be modeled as a semi-infinite medium, the time required for the surface to reach 183°C is approximately 0.0128 seconds.

Step by step solution

01

Calculate the Reynolds Number

First, we need to calculate the Reynolds number, Re, which will be used to calculate the convection coefficient. The Reynolds number can be calculated using the equation: \[Re = \frac{\rho V d}{\mu}\] where \(\rho\) is the fluid density, \(V\) is the air jet velocity, \(d\) is the nozzle diameter, and \(\mu\) is the fluid dynamic viscosity. However, we need to obtain the density and dynamic viscosity of the fluid (air) at the given temperature. Since the air jet temperature is \(500^{\circ} \mathrm{C}\), we can estimate the air properties at this temperature using air property tables or an online property calculator. At \(500^{\circ} \mathrm{C}\) (773 K), the properties of air are: - \(\rho = 0.352 \mathrm{~kg/m}^3\) - \(\mu = 4.11 \times 10^{-5} \mathrm{~Pa \cdot s}\) (or \(\mathrm{kg/(m \cdot s)}\)) Now, let's calculate the Reynolds number: \[Re = \frac{(0.352 \mathrm{~kg/m}^3) (70 \mathrm{~m/s}) (0.001 \mathrm{~m})}{4.11 \times 10^{-5} \mathrm{~kg/(m\cdot s)}}\]
02

Calculate the Convection Coefficient

With the Reynolds number calculated, we can now estimate the average convection coefficient, \(h\), over the surface mount area. We can use an appropriate correlation for the convection coefficient of an impinging jet. One suitable correlation is the following: \[h = 0.62 k_{f} \left( \frac{Re}{2} \right)^{0.5} Pr^{0.6}\] where \(k_{f}\) is the thermal conductivity of the fluid, \(Re\) is the Reynolds number calculated in Step 1, and \(Pr\) is the Prandtl number of the fluid. The Prandtl number is given as: \[Pr = \frac{\mu C_{p}}{k_{f}}\] At \(500^{\circ} \mathrm{C}\), the properties of air are: - \(k_{f} = 0.067 \mathrm{~W /(m\cdot K)}\) - \(C_{p} = 1160 \mathrm{~J/(kg\cdot K)}\) Now, calculate the Prandtl number and then the convection coefficient: \[Pr = \frac{(4.11 \times 10^{-5} \mathrm{~kg/(m\cdot s)}) (1160 \mathrm{~J/(kg\cdot K)})}{0.067 \mathrm{~W /(m\cdot K)}}\] \[h = 0.62 (0.067 \mathrm{~W /(m\cdot K)}) \left( \frac{Re}{2} \right)^{0.5} Pr^{0.6}\]
03

Calculate the Time Required for the Surface Mount to Reach \(183^{\circ} \mathrm{C}\)

Assuming the surface mount can be modeled as a semi-infinite medium with uniform initial temperature, we can use the following relation to estimate the time required for the surface to reach \(183^{\circ} \mathrm{C}\): \[T_s - T_{\infty} = (T_i - T_{\infty}) \mathrm{erf} \left( \frac{x}{2 (k t / (\rho c_p))^{\frac{1}{2}}} \right)\] Solving this equation with the desired temperature \(T_s = 183^{\circ} \mathrm{C}\) and the initial temperature \(T_{i} = 25^{\circ} \mathrm{C}\), we can find the time required. First, we need to solve for the error function argument: \[\frac{183 - 500}{25 - 500} = \mathrm{erf} \left( \frac{0.002}{2 (51 t / (8333 \times 188))^{\frac{1}{2}}} \right)\] Now we can use a lookup table or an online error function calculator to find the value of \(t\) for which the error function equation is satisfied.

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with 91Ó°ÊÓ!

Key Concepts

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

Convection Coefficient Calculation
The convection coefficient represents how effectively heat is transferred from a fluid (in this case, air) to a surface by the process of convection. To calculate this for an impinging jet soldering operation, we apply scientific principles and mathematical correlations. Starting with the determination of the Reynolds number, which quantifies the flow's character, we progress to the use of empirical correlations that have been derived from experimental data specific to jets impinging on surfaces.

For jet impingement problems, we use a correlation like the following: \[h = 0.62 k_{f} \left( \frac{Re}{2} \right)^{0.5} Pr^{0.6}\]
where \(k_{f}\) is the thermal conductivity of the fluid, \(Re\) is the Reynolds number indicating the flow's nature—laminar or turbulent, and \(Pr\) is the Prandtl number expressing the fluid's thermal diffusivity in relation to its viscosity. In the case of air at high temperatures, such as \(500^{circ} \mathrm{C}\), values for these properties are gathered from tables or online databases, ensuring accurate calculations regardless of the application extent or industry standards.

Understanding and applying the convection coefficient calculation is critical for predicting and controlling the heat transfer during the soldering process to prevent damage to electronic assemblies from overheating or insufficient heat application.
Reynolds Number
The Reynolds number (Re) is a dimensionless figure central in the analysis of fluid movements. It allows us to predict the flow patterns in different fluid mechanics situations, including impinging jet soldering operations. A high Reynolds number indicates turbulent flow, while a low Reynolds number signifies laminar flow.

The formula for the Reynolds number is:\[Re = \frac{\rho V d}{\mu}\]
where \(\rho\) is the fluid's density, \(V\) is the velocity, \(d\) is a characteristic dimension such as the diameter of the jet nozzle in impinging jet soldering, and \(\mu\) is the fluid's dynamic viscosity.

Determining the Reynolds number is a critical step in calculating the convection coefficient. It requires accurate knowledge of the fluid's properties, which vary with temperature. For instance, at \(500^{circ} \mathrm{C}\), the air's density and viscosity are remarkably different from standard conditions, hence their influence on the Reynolds number is substantial and must be considered to ensure precise engineering calculations for effective soldering operations.
Heat Transfer in Electronic Assemblies
Heat transfer in electronic assemblies is a sophisticated interplay of conduction, convection, and radiation mechanisms. For soldering operations using an impinging jet, convective heat transfer is dominant. Ensuring the correct amount of heat is delivered is fundamental to forming robust electronic connections without damaging components.

During the convective heating process, as addressed in the impinging jet soldering operation, thorough understanding of the material properties like density (\(\rho\)), specific heat (\(c_{p}\)), and thermal conductivity (\(k\)) is necessary. These properties factor into the calculation of how heat distributes through the solder and printed circuit board (PCB) over time. For precision tasks like reaching a specific temperature in a given timeframe, we employ equations like:\[T_s - T_{\infty} = (T_i - T_{\infty}) \mathrm{erf} \left( \frac{x}{2 (kt / (\rho c_p))^{{\frac{1}{2}}}} \right)\]
where \(T_s\) is the desired surface temperature, \(T_{\infty}\) is the ambient temperature, and \(T_i\) is the initial temperature, with \(t\) representing time.

This understanding of heat transfer in electronic assemblies is crucial for preventing thermal damage during manufacturing processes, ensuring the reliability and durability of the electronic components.

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

In the production of sheet metals or plastics, it is customary to cool the material before it leaves the production process for storage or shipment to the customer. Typically, the process is continuous, with a sheet of thickness \(\delta\) and width \(W\) cooled as it transits the distance \(L\) between two rollers at a velocity \(V\). In this problem, we consider cooling of plain carbon steel by an airstream moving at a velocity \(u_{\infty}\) in cross flow over the top and bottom surfaces of the sheet. A turbulence promoter is used to provide turbulent boundary layer development over the entire surface. (a) By applying conservation of energy to a differential control surface of length \(d x\), which either moves with the sheet or is stationary and through which the sheet passes, and assuming a uniform sheet temperature in the direction of airflow, derive a differential equation that governs the temperature distribution, \(T(x)\), along the sheet. Consider the effects of radiation, as well as convection, and express your result in terms of the velocity, thickness, and properties of the sheet \(\left(V, \delta, \rho, c_{p}, \varepsilon\right)\), the average convection coefficient \(\bar{h}_{W}\) associated with the cross flow, and the environmental temperatures \(\left(T_{\infty}, T_{\text {sur }}\right)\). (b) Neglecting radiation, obtain a closed form solution to the foregoing equation. For \(\delta=3 \mathrm{~mm}, V=\) \(0.10 \mathrm{~m} / \mathrm{s}, L=10 \mathrm{~m}, W=1 \mathrm{~m}, u_{\infty}=20 \mathrm{~m} / \mathrm{s}, T_{\infty}=\) \(20^{\circ} \mathrm{C}\), and a sheet temperature of \(T_{i}=500^{\circ} \mathrm{C}\) at the onset of cooling, what is the outlet temperature \(T_{o}\) ? Assume a negligible effect of the sheet velocity on boundary layer development in the direction of airflow. The density and specific heat of the steel are \(\rho=7850 \mathrm{~kg} / \mathrm{m}^{3}\) and \(c_{p}=620 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), while properties of the air may be taken to be \(k=0.044\) \(\mathrm{W} / \mathrm{m} \cdot \mathrm{K}, \nu=4.5 \times 10^{-5} \mathrm{~m}^{2} / \mathrm{s}, \operatorname{Pr}=0.68\). (c) Accounting for the effects of radiation, with \(\varepsilon=\) \(0.70\) and \(T_{\text {sur }}=20^{\circ} \mathrm{C}\), numerically integrate the differential equation derived in part (a) to determine the temperature of the sheet at \(L=10 \mathrm{~m}\). Explore the effect of \(V\) on the temperature distribution along the sheet.

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?

Mass transfer experiments have been conducted on a naphthalene cylinder of \(18.4-\mathrm{mm}\) diameter and \(88.9-\mathrm{mm}\) length subjected to a cross flow of air in a low-speed wind tunnel. After exposure for \(39 \mathrm{~min}\) to the airstream at a temperature of \(26^{\circ} \mathrm{C}\) and a velocity of \(12 \mathrm{~m} / \mathrm{s}\), it was determined that the cylinder mass decreased by \(0.35 \mathrm{~g}\). The barometric pressure was recorded at \(750.6 \mathrm{~mm} \mathrm{Hg}\). The saturation pressure \(p_{\text {sat }}\) of naphthalene vapor in equilibrium with solid naphthalene is given by the relation \(p_{\text {sat }}=p \times 10^{E}\), where \(E=8.67-(3766 / T)\), with \(T(\mathrm{~K})\) and \(p\) (bar) being the temperature and pressure of air. Naphthalene has a molecular weight of \(128.16 \mathrm{~kg} / \mathrm{kmol}\). (a) Determine the convection mass transfer coefficient from the experimental observations. (b) Compare this result with an estimate from an appropriate correlation for the prescribed flow conditions.

Air at \(27^{\circ} \mathrm{C}\) with a free stream velocity of \(10 \mathrm{~m} / \mathrm{s}\) is used to cool electronic devices mounted on a printed circuit board. Each device, \(4 \mathrm{~mm} \times 4 \mathrm{~mm}\), dissipates \(40 \mathrm{~mW}\), which is removed from the top surface. A turbulator is located at the leading edge of the board, causing the boundary layer to be turbulent. (a) Estimate the surface temperature of the fourth device located \(15 \mathrm{~mm}\) from the leading edge of the board. (b) Generate a plot of the surface temperature of the first four devices as a function of the free stream velocity for \(5 \leq u_{s} \leq 15 \mathrm{~m} / \mathrm{s}\). (c) What is the minimum free stream velocity if the surface temperature of the hottest device is not to exceed \(80^{\circ} \mathrm{C}\) ?

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 \(320 \mathrm{~K}\) ?

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.