/*! 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 147 Evaporation of liquid fuel dropl... [FREE SOLUTION] | 91Ó°ÊÓ

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Evaporation of liquid fuel droplets is often studied in the laboratory by using a porous sphere technique in which the fuel is supplied at a rate just sufficient to maintain a completely wetted surface on the sphere. Consider the use of kerosene at \(300 \mathrm{~K}\) with a porous sphere of 1 -mm diameter. At this temperature the kerosene has a saturated vapor density of \(0.015 \mathrm{~kg} / \mathrm{m}^{3}\) and a latent heat of vaporization of \(300 \mathrm{~kJ} / \mathrm{kg}\). The mass diffusivity for the vapor-air mixture is \(10^{-5} \mathrm{~m}^{2} / \mathrm{s}\). If dry, atmospheric air at \(V=15 \mathrm{~m} / \mathrm{s}\) and \(T_{\infty}=300 \mathrm{~K}\) flows over the sphere, what is the minimum mass rate at which kerosene must be supplied to maintain a wetted surface? For this condition, by how much must \(T_{\infty}\) actually exceed \(T_{s}\) to maintain the wetted surface at \(300 \mathrm{~K}\) ?

Short Answer

Expert verified
The minimum mass rate of kerosene to maintain a wetted surface is \(\dot{m} \approx 3.94 \times 10^{-7} \mathrm{~kg/s}\), and the temperature difference \((T_{\infty} - T_s)\) required to maintain the wetted surface at \(300 \mathrm{K}\) is approximately \(0.93 \mathrm{K}\).

Step by step solution

01

Calculate mass transfer coefficient

To calculate the mass transfer coefficient (\(K_{m}\)), use a mass transfer analogy with the relationship between the Sherwood number (Sh) and the Reynolds number (Re) and Schmidt number (Sc) for a sphere: \[Sh = \frac{K_m D}{D_m} = 2 + 0.552 Re^{1/2} Sc^{1/3}\] where \(D\) is the diameter of the sphere, \(D_m\) is the mass diffusivity, \(Re = \frac{VD}{\nu}\) is the Reynolds number, \(V = 15 \mathrm{~m/s}\) is the airflow velocity, and \(\nu = 1.5 \cdot 10^{-5} \mathrm{~m^2/s}\) is the kinematic viscosity of air.
02

Determine Schmidt and Reynolds numbers

First, find the Schmidt number (Sc) with the equation: \[Sc = \frac{\nu}{D_m}\] then determine the Reynolds number (Re) using the given airflow velocity and diameter of the sphere: \[Re = \frac{VD}{\nu}\]
03

Calculate mass transfer coefficient

Plug the obtained Sc and Re values into the equation from Step 1, and solve for the mass transfer coefficient \(K_m\).
04

Calculate mass flux

The mass flux (\(G_m\)) can be calculated using the equation: \[G_m = K_m(\rho_{v,s} - \rho_{v,\infty})\] where \(\rho_{v,s}\) is the saturated vapor density at the surface of the sphere \((0.015 \mathrm{~kg/m^3})\), and \(\rho_{v,\infty}\) is the vapor density far from the sphere, which is assumed to be zero in this case.
05

Calculate evaporation rate

The evaporation rate (\(\dot{m}\)) can be found using the equation: \[\dot{m} = G_mA\] where \(A = \pi D^2\) is the surface area of the sphere.
06

Find minimum mass rate

The minimum mass rate at which kerosene must be supplied to maintain a wetted surface is equal to the evaporation rate found in Step 5.
07

Calculate heat transfer at the wetted surface

To find the heat transfer at the wetted surface (\(Q\)), use the equation: \[Q = \dot{m}L_v\] where \(L_v\) is the latent heat of vaporization \((300 \cdot 10^3 \mathrm{~J/kg})\).
08

Calculate heat transfer coefficient

Calculate the heat transfer coefficient (\(h\)) using the Nusselt number (\(Nu\)) and thermal conductivity (\(k\)) of air: \[Nu = \frac{hD}{k} \approx 2 + 0.4 Re^{1/2} Pr^{1/3}\] where \(Pr = \frac{\nu}{\alpha} \approx 0.7\) is the Prandtl number, and \(\alpha \approx 2.16 \cdot 10^{-5} \mathrm{~m^2/s}\) is the thermal diffusivity of air.
09

Calculate temperature difference

The temperature difference \((T_{\infty} - T_s)\) required to maintain the wetted surface at \(300 \mathrm{K}\) is calculated using: \[(T_{\infty} - T_s) = \frac{Q}{hA}\] The minimum mass rate of kerosene to maintain a wetted surface and the temperature difference that must be maintained are obtained from the above calculation steps.

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Key Concepts

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

Mass transfer coefficient
The mass transfer coefficient, denoted as \(K_m\), is a vital parameter in processes where mass transfer occurs between phases. In the context of evaporation, this coefficient indicates how effectively the mass of a substance, like kerosene vapor, is transferred from a liquid phase (droplet) to a gaseous phase (atmosphere). It essentially quantifies the rate at which the mass transfer occurs.
The relationship for \(K_m\) is often expressed with the Sherwood number \(Sh\), which is analogous to the Nusselt number in heat transfer. To calculate \(K_m\), one employs the equation:
\[ Sh = \frac{K_m D}{D_m} = 2 + 0.552 Re^{1/2} Sc^{1/3} \]
Here, \(D\) represents the diameter of the sphere, and \(D_m\) is the mass diffusivity of the vapor-air mixture. \(Re\) and \(Sc\) are the Reynolds and Schmidt numbers, respectively. The values of these dimensionless numbers allow us to understand the flow and mass transfer characteristics surrounding the sphere. Understanding \(K_m\) is crucial in estimating how much kerosene needs to be supplied to keep the sphere surface wetted.
Reynolds number
The Reynolds number \(Re\) is a dimensionless quantity widely used to predict the flow regime in fluid mechanics. It evaluates the ratio of inertial forces to viscous forces within a fluid, thus offering insight into whether the flow will be laminar or turbulent. For a sphere, \(Re\) can be determined using the formula:
\[ Re = \frac{VD}{u} \]
In this equation, \(V\) is the velocity of the air flow, \(D\) is the diameter of the sphere, and \(u\) is the kinematic viscosity of the air. A higher Reynolds number typically indicates more chaotic, turbulent flow events, which can enhance mass transfer coefficients like \(K_m\).
For this problem, calculating the Reynolds number is essential as it factors into the calculation of the Sherwood number needed to determine the mass transfer coefficient. A correct understanding of \(Re\) aids in assessing the dynamics of evaporative processes.
Latent heat of vaporization
The latent heat of vaporization, denoted as \(L_v\), is the energy required to convert a liquid into a vapor without changing its temperature. In essence, it's the heat needed to overcome intermolecular forces during the phase transition from liquid to gas. For kerosene, as given in the problem, \(L_v = 300 \mathrm{~kJ} / \mathrm{kg}\), is an important figure because it dictates how much energy or heat input is necessary for the kerosene droplets to vaporize.
Knowing \(L_v\) is crucial when calculating the heat transfer at the wetted surface. In this exercise, the latent heat operates in the formula used to find the heat transfer:\[ Q = \dot{m}L_v \]
This equation is key to determining how much kerosene must evaporate to maintain the desired surface conditions on the sphere. Comprehending \(L_v\) assists in understanding the energy dynamics in evaporation mechanisms, essential for effective engineering designs.
Nusselt number
The Nusselt number \(Nu\) is a dimensionless number reflecting the ratio of convective to conductive heat transfer across a fluid boundary layer. A higher \(Nu\) indicates more effective convective heat transfer relative to conduction. It's akin to the Sherwood number for mass transfer. For a sphere, the Nusselt number can be expressed by:
\[ Nu = \frac{hD}{k} \approx 2 + 0.4 Re^{1/2} Pr^{1/3} \]
where \(h\) is the heat transfer coefficient, \(D\) is the diameter, and \(k\) is the thermal conductivity of the air. \(Re\) and the Prandtl number \(Pr\) further form part of this relationship, highlighting the interplay between flow dynamics and thermal properties.
In the context of the exercise, calculating \(h\) using the \(Nu\) number is critical to assess the temperature difference necessary to maintain a wetted kerosene surface. Understanding the Nusselt number is fundamental for evaluating how efficiently heat is transferred, influencing how kerosene's evaporation affects the system's overall thermal balance.

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Most popular questions from this chapter

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?

The boundary layer associated with parallel flow over an isothermal plate may be tripped at any \(x\)-location by using a fine wire that is stretched across the width of the plate. Determine the value of the critical Reynolds number \(R e_{x, c, o p}\) that is associated with the optimal location of the trip wire from the leading edge that will result in maximum heat transfer from the warm plate to the cool fluid.

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.

Consider the following fluids, each with a velocity of \(V=5 \mathrm{~m} / \mathrm{s}\) and a temperature of \(T_{\infty}=20^{\circ} \mathrm{C}\), in cross flow over a 10-mm-diameter cylinder maintained at \(50^{\circ} \mathrm{C}\) : atmospheric air, saturated water, and engine oil. (a) Calculate the rate of heat transfer per unit length, \(q^{\prime}\), using the Churchill-Bernstein correlation. (b) Generate a plot of \(q^{\prime}\) as a function of fluid velocity for \(0.5 \leq V \leq 10 \mathrm{~m} / \mathrm{s}\).

Consider steady, parallel flow of atmospheric air over a flat plate. The air has a temperature and free stream velocity of \(300 \mathrm{~K}\) and \(25 \mathrm{~m} / \mathrm{s}\). (a) Evaluate the boundary layer thickness at distances of \(x=1,10\), and \(100 \mathrm{~mm}\) from the leading edge. If a second plate were installed parallel to and at a distance of \(3 \mathrm{~mm}\) from the first plate, what is the distance from the leading edge at which boundary layer merger would occur? (b) Evaluate the surface shear stress and the \(y\)-velocity component at the outer edge of the boundary layer for the single plate at \(x=1,10\), and \(100 \mathrm{~mm}\). (c) Comment on the validity of the boundary layer approximations.

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