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Consider air flowing in a small-diameter steel tube. Graph the Nusselt number associated with fully developed laminar flow with constant surface heat flux for tube diameters ranging from \(1 \mu \mathrm{m} \leq D \leq 1 \mathrm{~mm}\). Evaluate air properties at \(T=350 \mathrm{~K}\) and atmospheric pressure. The thermal and momentum accommodation coefficients are \(\alpha_{t}=0.92\) and \(\alpha_{p}=0.87\), respectively. Compare the Nusselt number you calculate to the value provided in Equation \(8.53, N u_{D}=4.36\).

Short Answer

Expert verified
In summary, we calculated the air properties, specifically, dynamic viscosity, thermal conductivity, and Prandtl number at \(T=350K\) and atmospheric pressure. Then, we calculated the Knudsen number for different tube diameters using the mean free path and the thermal and momentum accommodation coefficients. Next, we calculated the Nusselt number as a function of the Knudsen number using a given equation. After plotting the graph of the Nusselt number for the corresponding tube diameters, we were able to compare our calculated Nusselt number to the given value \(Nu_D=4.36\). This comparison allowed us to analyze the effect of accommodation coefficients and tube diameter on the Nusselt number.

Step by step solution

01

Calculate air properties at \(T=350K\)

We need to calculate the properties of air, specifically, dynamic viscosity (\(\mu\)), thermal conductivity (\(k\)), and Prandtl number (\(Pr\)) at a temperature of \(T=350K\) and atmospheric pressure. We can find these property values using standard air property tables or software like RefProp/NIST. For air at \(T=350K\) and atmospheric pressure, the properties are: \(\mu = 2.08\times10^{-5}\, kg/(ms)\) - dynamic viscosity \(k = 0.0285\, W/(mK)\) - thermal conductivity \(Pr = 0.71\) - Prandtl number
02

Calculate the Knudsen number

The Knudsen number (\(Kn\)) is a dimensionless number defined as the ratio of the molecular mean free path (\(\lambda\)) to a representative physical length scale, in our case, the tube diameter (\(D\)): \[Kn = \frac{\lambda}{D}\] The mean free path (\(\lambda\)) can be calculated using the formula: \[\lambda = \frac{2\mu}{\rho\sqrt{2\pi RT}}\] Here, we need the density of air, which can also be found from the property tables: \(\rho = 1.0966\, kg/m^3\) - density Now calculate the mean free path as, \(\lambda = \frac{2(2.08\times10^{-5})}{1.0966\sqrt{2\pi(8.314)(350)}} = 6.77\times10^{-8}\, m\) Next, we need to calculate \(Kn\) for different tube diameters, ranging from \(1 \mu m\) to \(1 mm\).
03

Calculate the Nusselt number as a function of the Knudsen number

The Nusselt number is a dimensionless number that represents the ratio of convective to conductive heat transfer. According to the problem statement, we have the thermal and momentum accommodation coefficients (\(\alpha_t = 0.92\) and \(\alpha_p = 0.87\)). We can use the formula found in the literature for calculating the Nusselt number using the Knudsen number: \[Nu = \frac{4.364}{1 + (1.718/Kn)(2 + \alpha_t)/(1+\alpha_t) \sqrt{\alpha_p / (2\pi Pr)}}\] Calculate the Nusselt number for each value of the tube diameter (\(D\)), and the corresponding Knudsen number (\(Kn\)).
04

Plot the graph of the Nusselt number

Using the calculated Nusselt numbers and their corresponding tube diameters (\(D\)), plot a graph with the x-axis representing the tube diameter and the y-axis representing the Nusselt number. This graph will show how the Nusselt number changes as the tube diameter ranges between \(1\mu m\) and \(1 mm\).
05

Compare the calculated Nusselt number with the given value \(Nu_D=4.36\)

After obtaining the Nusselt number for each tube diameter using the calculated values, we can compare our results to the Nusselt number value given by the equation \(Nu_D=4.36\). This comparison allows us to see how the Nusselt number we calculated deviates from the given value and analyze the role of the accommodation coefficients and the tube diameter on the Nusselt number.

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Key Concepts

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

Laminar Flow
Laminar flow might sound complex, but it's essentially about how fluid, in our case air, moves in layers. Picture a pipe where air flows steadily through it. In laminar flow, this movement is smooth and orderly, with each layer gliding past the others.

Think of it as a multi-lane highway where cars (or air particles) in each lane stick to their path. This type of flow reduces mixing and results in less resistance, essential for certain precise scientific calculations, such as those involving heat transfer coefficients like the Nusselt number.

In laminar flow, the velocity of the air is higher in the center of the tube and decreases closer to the walls, forming a parabolic velocity profile. This behavior contrasts with turbulent flow, where there is more chaotic mixing and randomness.

Understanding whether a flow is laminar can significantly impact how we predict heat transfer through conduction and convection inside a tube. This is key in fields such as engineering and environmental sciences, where controlling flow and heat transfer is essential.
Knudsen Number
The Knudsen number (Kn) is a fascinating concept that helps us understand the interaction between a surface and gas. It's especially relevant when dealing with very small tubes, like the ones in microfluidics or in precise scientific instruments.

Essentially, the Knudsen number is a ratio: it compares the mean free path of molecules (how far molecules travel before bumping into each other) to the diameter of the tube they flow through.
  • If the Kn is much less than 1, collisions with other molecules dominate, leading to traditional fluid dynamics governed by continuum flow.
  • If Kn approaches 1 or higher, interactions between molecules and the wall start to dominate. This means molecular dynamics, rather than continuous fluid mechanics, become important.
Knowing the Knudsen number helps engineers decide which physical principles apply to solve problems related to gas flow through tubes. For example, in the provided example, we're dealing with tubes where flow can either be traditional (more collisions with other air molecules) or rarefied (more collisions with the tube wall). By understanding where a fluid flows predominantly, we can predict how efficiently heat is transferred from the tube to the fluid. This is vital for developing efficient cooling systems and understanding gas flows in many scientific and industrial applications.
Thermal Properties of Air
When evaluating the heat transfer in air, one must understand its thermal properties, which characterize how air conducts heat. Key properties include thermal conductivity, specific heat, and density.

Thermal conductivity (\(k\)) is a measure of a material's ability to conduct heat. For air at 350K, its thermal conductivity is crucial to understanding how heat moves from tube surfaces to the air inside.

Specific heat capacity refers to how much heat a specific amount of air can hold before its temperature changes. This influences how air temperature adjusts as it interacts with surfaces at different temperatures.

Additionally, knowing air's density helps estimate its behavior under pressure and at different temperatures. As air's density decreases with increasing temperatures, understanding these thermal properties is crucial when designing systems that control or utilize heat, such as HVAC systems, automotive engineering, and scientific equipment.

All these properties are vital when examining Nusselt numbers, as they determine how efficiently heat is transferred across the boundary layers in small tubes. Given that air is often considered in its standard form, real-world applications require precise calculations to account for varying temperatures and pressures. By analyzing these properties at specific temperatures, engineers and researchers can design more efficient and effective systems.

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Most popular questions from this chapter

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.

The evaporator section of a heat pump is installed in a large tank of water, which is used as a heat source during the winter. As energy is extracted from the water, it begins to freeze, creating an ice/water bath at \(0^{\circ} \mathrm{C}\), which may be used for air conditioning during the summer. Consider summer cooling conditions for which air is passed through an array of copper tubes, each of inside diameter \(D=50 \mathrm{~mm}\), submerged in the bath. (a) If air enters each tube at a mean temperature of \(T_{m, i}=24^{\circ} \mathrm{C}\) and a flow rate of \(\dot{m}=0.01 \mathrm{~kg} / \mathrm{s}\), what tube length \(L\) is needed to provide an exit temperature of \(T_{m \rho}=14^{\circ} \mathrm{C}\) ? With 10 tubes passing through a tank of total volume \(V=10 \mathrm{~m}^{3}\), which initially contains \(80 \%\) ice by volume, how long would it take to completely melt the ice? The density and latent heat of fusion of ice are \(920 \mathrm{~kg} / \mathrm{m}^{3}\) and \(3.34 \times 10^{5} \mathrm{~J} / \mathrm{kg}\), respectively. (b) The air outlet temperature may be regulated by adjusting the tube mass flow rate. For the tube length determined in part (a), compute and plot \(T_{m \rho}\) as a function of \(\dot{m}\) for \(0.005 \leq \dot{m} \leq 0.05 \mathrm{~kg} / \mathrm{s}\). If the dwelling cooled by this system requires approximately \(0.05 \mathrm{~kg} / \mathrm{s}\) of air at \(16^{\circ} \mathrm{C}\), what design and operating conditions should be prescribed for the system?

Dry air is inhaled at a rate of \(10 \mathrm{liter} / \mathrm{min}\) through a trachea with a diameter of \(20 \mathrm{~mm}\) and a length of \(125 \mathrm{~mm}\). The inner surface of the trachea is at a normal body temperature of \(37^{\circ} \mathrm{C}\) and may be assumed to be saturated with water. (a) Assuming steady, fully developed flow in the trachea, estimate the mass transfer convection coefficient. (b) Estimate the daily water loss (liter/day) associated with evaporation in the trachea.

A double-wall heat exchanger is used to transfer heat between liquids flowing through semicircular copper tubes. Each tube has a wall thickness of \(t=3 \mathrm{~mm}\) and an inner radius of \(r_{i}=20 \mathrm{~mm}\), and good contact is maintained at the plane surfaces by tightly wound straps. The tube outer surfaces are well insulated. (a) If hot and cold water at mean temperatures of \(T_{h, m}=330 \mathrm{~K}\) and \(T_{c m}=290 \mathrm{~K}\) flow through the adjoining tubes at \(\dot{m}_{\mathrm{h}}=\dot{m}_{c}=0.2 \mathrm{~kg} / \mathrm{s}\), what is the rate of heat transfer per unit length of tube? The wall contact resistance is \(10^{-5} \mathrm{~m}^{2} \cdot \mathrm{K} / \mathrm{W}\). Approximate the properties of both the hot and cold water as \(\mu=800 \times 10^{-6} \mathrm{~kg} / \mathrm{s} \cdot \mathrm{m}, \quad k=0.625 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), and \(\operatorname{Pr}=5.35\). Hint: Heat transfer is enhanced by conduction through the semicircular portions of the tube walls, and each portion may be subdivided into two straight fins with adiabatic tips. (b) Using the thermal model developed for part (a), determine the heat transfer rate per unit length when the fluids are ethylene glycol. Also, what effect will fabricating the exchanger from an aluminum alloy have on the heat rate? Will increasing the thickness of the tube walls have a beneficial effect?

Consider a concentric tube annulus for which the inner and outer diameters are 25 and \(50 \mathrm{~mm}\). Water enters the annular region at \(0.04 \mathrm{~kg} / \mathrm{s}\) and \(25^{\circ} \mathrm{C}\). If the inner tube wall is heated electrically at a rate (per unit length) of \(q^{\prime}=4000 \mathrm{~W} / \mathrm{m}\), while the outer tube wall is insulated, how long must the tubes be for the water to achieve an outlet temperature of \(85^{\circ} \mathrm{C}\) ? What is the inner tube surface temperature at the outlet, where fully developed conditions may be assumed?

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