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A computer code is being developed to analyze a temperature sensor of \(12.5-\mathrm{mm}\) diameter experiencing cross flow of water with a free stream temperature of \(80^{\circ} \mathrm{C}\) and variable velocity. Derive an expression for the convection heat transfer coefficient as a function of the sensor surface temperature \(T_{s}\) for the range \(20

Short Answer

Expert verified
In this problem, we derived an expression for the convection heat transfer coefficient (h) using the Zukauskas correlation given the temperature and velocity range for a water flow around a temperature sensor. The final expression for h is: \(h = \frac{k_f C_1}{D} \left(\frac{VD}{\nu}\right)^{m_1}(Pr_0 + k(T - T_0))^{1/3}\) where h depends on the fluid properties, velocity (V), diameter of the temperature sensor (D), and the surface temperature (T_s) of the sensor for the given temperature and velocity range.

Step by step solution

01

Zukauskas Correlation

The Zukauskas Correlation provides the convection heat transfer coefficient for a particular flow. In this case, it is given for a range of Reynolds number (40 < Re_D < 1000) and embodies both laminar and turbulent flow regimes. The Zukauskas correlation is as follows: \(Nu_D = C_1 Re_D^{m_1} Pr^{1/3}\) where Nu_D is the Nusselt number, Re_D is the Reynolds number, Pr is the Prandtl number of water, and C_1 and m_1 are constants.
02

Express the Reynolds number (Re_D) and Prandtl number (Pr)

The Reynolds number (Re_D) for a fluid in cross flow over a cylinder is given by: \(Re_D = \frac{VD}{\nu}\) where V is the velocity of the fluid, D is the diameter of the temperature sensor, and ν is the kinematic viscosity of the fluid. For water, as we have variable velocity and temperature, we will assume a linear temperature dependence for the Prandtl number as follows: \(Pr(T) = Pr_0 + k(T - T_0)\) where Pr_0 is the reference Prandtl number at reference temperature T_0, k is the linear temperature coefficient, and T is the fluid temperature.
03

Substitute Re_D and Pr into the Zukauskas Correlation

Now, we will substitute our expressions for Re_D and Pr into the Zukauskas correlation: \(Nu_D = C_1\left(\frac{VD}{\nu}\right)^{m_1}(Pr_0 + k(T - T_0))^{1/3}\)
04

Express Nu_D in terms of h

The Nusselt number (Nu_D) is expressed as a function of the convection heat transfer coefficient (h) and the diameter of the temperature sensor (D): \(Nu_D = \frac{hD}{k_f}\) where k_f is the thermal conductivity of the fluid. Now, substitute this expression for Nu_D into our previous equation: \(\frac{hD}{k_f} = C_1\left(\frac{VD}{\nu}\right)^{m_1}(Pr_0 + k(T - T_0))^{1/3}\)
05

Isolate h and simplify

Finally, isolate h in the above equation: \(h = \frac{k_f C_1}{D} \left(\frac{VD}{\nu}\right)^{m_1}(Pr_0 + k(T - T_0))^{1/3}\) Here we have an expression for the convection heat transfer coefficient (h) in terms of the fluid properties, velocity (V), diameter of the temperature sensor (D), and the surface temperature (T_s) of the sensor for the given temperature and velocity range.

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Key Concepts

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

Zukauskas Correlation
The Zukauskas Correlation is a relation used in determining the convection heat transfer coefficient for flows over objects such as cylinders or spheres. It is especially useful when analyzing the heat transfer characteristics in cross flow situations where the fluid is not moving parallel to the object, but rather flows across it.

The general form of the correlation combines the Nusselt, Reynolds, and Prandtl numbers, which signify the dimensionless heat transfer, fluid flow, and fluid property characteristics, respectively. The correlation itself is represented by the equation:

\[Nu_D = C_1 Re_D^{m_1} Pr^{n}\]
Here, if we consider the Prandtl number exponent to be 1/3 (as typically assumed for turbulent flow), our equation simplifies to the expression provided in the textbook solution. The constants \(C_1\) and \(m_1\) vary with the specific flow regime and geometry. Knowing the correct form of the Zukauskas Correlation is crucial for accurately predicting the heat transfer coefficient in engineering applications.
Nusselt Number
The Nusselt number \(Nu\) is a dimensionless parameter that describes the ratio of convective to conductive heat transfer across a boundary layer. Mathematically, it can be expressed as:

\[Nu = \frac{hL}{k}\]
where \(h\) is the convective heat transfer coefficient, \(L\) is a characteristic length (which can be the diameter of the cylinder in the case of cross flow), and \(k\) is the thermal conductivity of the fluid.

The Nusselt number provides us with an understanding of the efficiency of heat transfer from a surface to the surrounding fluid flow. Large Nusselt numbers suggest efficient convective heat transfer, either due to strong fluid motion or significantly different fluid and surface temperatures. Understanding the Nusselt number's significance is key for designing effective heat exchangers and other thermal management systems.
Reynolds Number
The Reynolds number \(Re\) is another dimensionless quantity used to predict flow patterns in different fluid flow situations. It helps determine whether the flow is laminar or turbulent. The Reynolds number for flow over a cylinder is given as:

\[Re_D = \frac{VD}{u}\]
In this equation, \(V\) represents the flow velocity, \(D\) represents a characteristic diameter (such as that of a cylinder), and \(u\) is the kinematic viscosity of the fluid.

In the context of the exercise, understanding the relationship between fluid velocity, sensor diameter, and fluid properties such as viscosity helps to determine the flow regime and subsequently the convection heat transfer behavior.
Prandtl Number
The Prandtl number \(Pr\), another dimensionless number, is a key player when it comes to characterizing the fluid's thermal and momentum diffusivity. It is defined as:

\[Pr = \frac{u}{\alpha}\]
where \(u\) represents the kinematic viscosity, and \(\alpha\) denotes the thermal diffusivity of the fluid. High Prandtl numbers indicate that momentum diffusivity outweighs thermal diffusivity, which typically occurs in viscous fluids like oils, while low Prandtl numbers are characteristic of fluids like liquid metals where heat diffuses quickly compared to the fluid's momentum.

In the exercise, a linear temperature dependence for the Prandtl number is assumed, which suggests a need to understand how fluid properties change with temperature when dealing with heat transfer problems.
Cross Flow Heat Transfer
When a fluid flows perpendicular to a surface, the phenomenon is known as cross flow. This type of flow is particularly important in the context of heat transfer because it is associated with different characteristics than parallel flow.

Cross flow heat transfer is often complex due to the formation of boundary layers on the object's surface, which impacts the efficiency of heat transfer. Variables such as the shape and size of the object, fluid velocity, and properties all play a crucial role in determining the convective heat transfer coefficient.

For cylindrical objects, like the temperature sensor in our exercise, the cross flow situation requires special attention due to the development of a varied flow pattern around the object that influences the heat transfer rate. Engineering applications such as heat exchangers and cooling systems in electronics rely on understanding and manipulating cross flow for optimal performance.

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

Consider laminar, parallel flow past an isothermal flat plate of length \(L\), providing an average heat transfer coefficient of \(\bar{h}_{L^{-}}\)If the plate is divided into \(N\) smaller plates, each of length \(L_{N}=L / N\), determine an expression for the ratio of the heat transfer coefficient averaged over the \(N\) plates to the heat transfer coefficient averaged over the single plate, \(\bar{h}_{L, N} / \bar{h}_{L, 1}\).

A circular pipe of 25 -mm outside diameter is placed in an airstream at \(25^{\circ} \mathrm{C}\) and 1 -atm pressure. The air moves in cross flow over the pipe at \(15 \mathrm{~m} / \mathrm{s}\), while the outer surface of the pipe is maintained at \(100^{\circ} \mathrm{C}\). What is the drag force exerted on the pipe per unit length? What is the rate of heat transfer from the pipe per unit length?

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 \(k=\) \(51 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\).

To augment heat transfer between two flowing fluids, it is proposed to insert a 100 -mm-long, 5 -mm-diameter 2024 aluminum pin fin through the wall separating the two fluids. The pin is inserted to a depth of \(d\) into fluid 1 . Fluid 1 is air with a mean temperature of \(10^{\circ} \mathrm{C}\) and velocity of \(10 \mathrm{~m} / \mathrm{s}\). Fluid 2 is air with a mean temperature of \(40^{\circ} \mathrm{C}\) and velocity of \(3 \mathrm{~m} / \mathrm{s}\). (a) Determine the rate of heat transfer from the warm air to the cool air through the pin fin for \(d=50 \mathrm{~mm}\). (b) Plot the variation of the heat transfer rate with the insertion distance, \(d\). Does an optimal insertion distance exist?

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