/*! 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 8 A flat plate of width \(1 \mathr... [FREE SOLUTION] | 91Ó°ÊÓ

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A flat plate of width \(1 \mathrm{~m}\) is maintained at a uniform surface temperature of \(T_{s}=150^{\circ} \mathrm{C}\) by using independently controlled, heat-generating rectangular modules of thickness \(a=10 \mathrm{~mm}\) and length \(b=50 \mathrm{~mm}\). Each module is insulated from its neighbors, as well as on its back side. Atmospheric air at \(25^{\circ} \mathrm{C}\) flows over the plate at a velocity of \(30 \mathrm{~m} / \mathrm{s}\). The thermophysical properties of the module are \(k=5.2 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, c_{p}=320 \mathrm{~J} / \mathrm{kg}+\mathrm{K}\), and \(\rho=2300 \mathrm{~kg} / \mathrm{m}^{3}\). (a) Find the required power generation, \(\dot{q}\left(\mathrm{~W} / \mathrm{m}^{3}\right)\), in a module positioned at a distance \(700 \mathrm{~mm}\) from the leading edge. (b) Find the maximum temperature \(T_{\max }\) in the heatgenerating module.

Short Answer

Expert verified
The required heat generation in the module is \(\dot{q} = 480.96 \mathrm{~W/m^2}\) and the maximum temperature in the heat-generating module is \(T_{max} = 275.25^\circ \mathrm{C}\).

Step by step solution

01

Determine the Reynolds number at 700 mm from the leading edge

First, we need to determine the Reynolds number at \(x = 700 \mathrm{~mm}\) from the leading edge. The Reynolds number is given by: \[Re_x = \frac{Ux}{\nu}\] where \(U = 30 \mathrm{~m/s}\) is the flow velocity, \(x = 0.7 \mathrm{~m}\) is the distance from the leading edge, and \(\nu\) is the kinematic viscosity of the air. Assuming the air viscosity to be \(\nu = 1.5 \times 10^{-5} \mathrm{~m^2/s}\), we have: \[Re_x = \frac{30 \times 0.7}{1.5 \times 10^{-5}} = 1.4 \times 10^6\]
02

Calculate the Nusselt number using a correlation for laminar flow over a flat plate

Since the Reynolds number is larger than \(5\times10^5\), the flow is turbulent. We can use the correlation for turbulent flow over a flat plate to find the Nusselt number: \[\frac{Nu_x}{Re_x^{1/5}} = 0.037Pr^{1/3}\] where \(Nu_x = \frac{h x}{k_f}\) is the Nusselt number, \(h\) is the convective heat transfer coefficient, and \(k_f\) is the thermal conductivity of the fluid. For air, we have \(k_f = 0.026 \mathrm{~W/m \cdot K}\) and \(Pr = 0.7\). Thus, the Nusselt number is: \[Nu_x = 0.037(1.4\times10^6)^{1/5}Pr^{1/3}=103.6\]
03

Determine the convective heat transfer coefficient

Now we can find the convective heat transfer coefficient \(h\): \[h = \frac{Nu_x k_f}{x}\] \[h = \frac{103.6 \times 0.026}{0.7} = 3.84 \mathrm{~W/m^2 \cdot K}\]
04

Calculate the required power generation in the module

We can now find the required power generation in the module using the following equation: \[\dot{q} = h(T_s - T_\infty)\] where \(T_s = 150^\circ \mathrm{C}\) is the surface temperature, and \(T_\infty = 25^\circ \mathrm{C}\) is the atmospheric temperature. Thus, we have: \[\dot{q} = 3.84 (150 -25) = 480.96 \mathrm{~W/m^2}\]
05

Find the maximum temperature in the heat-generating module

We can find the maximum temperature in the module by adding the temperature rise produced by the heat generation to the surface temperature \(T_s\). First, we need to find the temperature rise using the equation: \[\Delta T = \frac{\dot{q}}{h} = \frac{480.96}{3.84} = 125.25^\circ \mathrm{C}\] Then, the maximum temperature in the module is: \[T_{max} = T_s + \Delta T = 150 + 125.25 = 275.25^\circ \mathrm{C}\] Finally, we have found that the required heat generation in the module is \(\dot{q} = 480.96 \mathrm{~W/m^2}\) and the maximum temperature in the heat-generating module is \(T_{max} = 275.25^\circ \mathrm{C}\).

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Key Concepts

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

Reynolds Number
Understanding the Reynolds Number is key when analyzing fluid flow over surfaces. It is a dimensionless number that helps predict flow patterns. The Reynolds Number, denoted by \(Re \), is determined using the formula: \[ Re_x = \frac{Ux}{u} \] where \( U \) is the velocity of the fluid, \( x \) is the characteristic length (in this case, the distance from the leading edge), and \( u \) is the kinematic viscosity of the fluid. The Reynolds Number indicates whether the flow is laminar or turbulent. For flow over a flat plate, a \(Re \) less than \(5 \times 10^5\) suggests laminar flow, while a \(Re \) greater than \(5 \times 10^5\) indicates turbulent flow. Turbulent flow is characterized by chaotic and eddying motion, which enhances mixing and thus affects heat transfer rates.
  • Laminar Flow: Streamlined and orderly.
  • Turbulent Flow: Disordered and mixed.
Nusselt Number
The Nusselt Number \(Nu\), another dimensionless number, provides insight into the convective heat transfer occurring at the surface. It is defined as: \[ Nu_x = \frac{hx}{k_f} \] where \( h \) is the convective heat transfer coefficient and \( k_f \) is the thermal conductivity of the fluid. The Nusselt Number represents the ratio of convective to conductive heat transfer across a boundary. The larger the \(Nu \), the more significant the convective heat transfer. In this context, a higher Nusselt Number typically results when the flow is turbulent.
The relationship between the Reynolds Number and the Nusselt Number is often given through empirical correlations depending on whether the flow is laminar or turbulent. For turbulent flow over a flat plate, the correlation used is: \[ \frac{Nu_x}{Re_x^{1/5}} = 0.037 Pr^{1/3} \] where \(Pr \) is the Prandtl Number, a measure of fluid flow properties that links viscosity and thermal diffusivity. This correlation helps determine \(Nu_x\), essential for calculating the heat transfer coefficient.
Convective Heat Transfer Coefficient
The Convective Heat Transfer Coefficient \(h\) is a fundamental part of analyzing heat transfer between a surface and a fluid. It is found from the Nusselt Number with the expression: \[ h = \frac{Nu_x k_f}{x} \] The coefficient \(h\) represents the heat transfer capability due to convection, measured in \( \text{W/m}^2 \cdot \text{K} \). It is indicative of the rate at which heat dissipates from the surface to a fluid in motion. Higher values of \(h\) suggest more efficient heat dissipation. In our context, achieving a higher \(h\) is crucial for preventing overheating of surfaces, especially when dealing with heat-generating components.
Understanding \(h\) is essential for designing cooling processes, improving thermal performance, and ensuring safe operating temperatures in technological applications.
Thermophysical Properties
Thermophysical Properties of materials are crucial in determining how heat is transferred in systems. They include:
  • Thermal conductivity \(k\): Measures a material's ability to conduct heat. High \(k\) indicates good thermal conducting ability.
  • Specific heat \(c_p\): The amount of heat per unit mass required to raise the temperature by one degree Celsius. Important for understanding heat capacity.
  • Density \(\rho\): The mass per unit volume, impacting how a material absorbs and retains heat.
These properties define how components in thermal systems interact, affecting heat diffusion and overall thermal performance. Understanding these helps in selecting materials for specific thermal requirements, ensuring stability and efficiency in heat-related applications.
Turbulent Flow
Turbulent Flow occurs when a fluid moves in a chaotic, irregular manner, often described as having swirling vortices. This type of flow significantly enhances heat transfer compared to laminar flow. The transition to turbulence typically occurs at higher Reynolds Numbers, as observed in our exercise.
Turbulent flow leads to:
  • Enhanced mixing of fluid layers.
  • Increased heat and mass transfer rates.
  • Greater energy dissipation.
The turbulence's chaotic nature promotes mixing, making it easier for heat to move from the surface to the moving fluid, resulting in a higher convective heat transfer coefficient. As such, understanding and predicting turbulent behavior is vital for engineering processes, as it directly influences the design of heat exchangers and cooling systems.

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Most popular questions from this chapter

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 \(80^{\circ} \mathrm{C}\) ?

Motile bacteria are equipped with flagella that are rotated by tiny, biological electrochemical engines which, in turn, propel the bacteria through a host liquid. Consider a nominally spherical Escherichia coli bacterium that is of diameter \(D=2 \mu \mathrm{m}\). The bacterium is in a water-based solution at \(37^{\circ} \mathrm{C}\) containing a nutrient which is characterized by a binary diffusion coefficient of \(D_{\mathrm{AB}}=0.7 \times 10^{-9} \mathrm{~m}^{2} / \mathrm{s}\) and a food energy value of \(\mathcal{N}=16,000 \mathrm{~kJ} / \mathrm{kg}\). There is a nutrient density difference between the fluid and the shell of the bacterium of \(\Delta \rho_{\mathrm{A}}=860 \times 10^{-12} \mathrm{~kg} / \mathrm{m}^{3}\). Assuming a propulsion efficiency of \(\eta=0.5\), determine the maximum speed of the E. coli. Report your answer in body diameters per second.

Consider a flat plate subject to parallel flow (top and bottom) characterized by \(u_{\infty}=5 \mathrm{~m} / \mathrm{s}, T_{\infty}=20^{\circ} \mathrm{C}\). (a) Determine the average convection heat transfer coefficient, convective heat transfer rate, and drag force associated with an \(L=2\)-m-long, \(w=2-\mathrm{m}\) wide flat plate for airflow and surface temperatures of \(T_{s}=50^{\circ} \mathrm{C}\) and \(80^{\circ} \mathrm{C}\). (b) Determine the average convection heat transfer coefficient, convective heat transfer rate, and drag force associated with an \(L=0.1\)-m-long, \(w=0.1\)-m-wide flat plate for water flow and surface temperatures of \(T_{s}=50^{\circ} \mathrm{C}\) and \(80^{\circ} \mathrm{C}\).

Consider the packed bed of aluminum spheres described in Problem \(5.12\) under conditions for which the bed is charged by hot air with an inlet velocity of \(V=1 \mathrm{~m} / \mathrm{s}\) and temperature of \(T_{g, i}=300^{\circ} \mathrm{C}\), but for which the convection coefficient is not prescribed. If the porosity of the bed is \(\varepsilon=0.40\) and the initial temperature of the spheres is \(T_{i}=25^{\circ} \mathrm{C}\), how long does it take a sphere near the inlet of the bed to accumulate \(90 \%\) of its maximum possible energy?

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.

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