/*! 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 134 Dry air at \(35^{\circ} \mathrm{... [FREE SOLUTION] | 91Ó°ÊÓ

91Ó°ÊÓ

Dry air at \(35^{\circ} \mathrm{C}\) and a velocity of \(15 \mathrm{~m} / \mathrm{s}\) flows over a long cylinder of \(20-\mathrm{mm}\) diameter. The cylinder is covered with a thin porous coating saturated with water, and an embedded electrical heater supplies power to maintain the coating surface temperature at \(20^{\circ} \mathrm{C}\). (a) What is the evaporation rate of water from the cylinder per unit length \((\mathrm{kg} / \mathrm{h}+\mathrm{m})\) ? What electrical power per unit length of the cylinder \((\mathrm{W} / \mathrm{m})\) is required to maintain steady-state conditions? (b) After a long period of operation, all the water is evaporated from the coating and its surface is dry. For the same free stream conditions and heater power of part (a), estimate the temperature of the surface.

Short Answer

Expert verified
In summary: a) The evaporation rate of water from the cylinder per unit length is \(dm/dt = 0.0261 \mathrm{kg/h \cdot m}\). The electrical power per unit length of the cylinder required to maintain steady-state conditions is \(P_{elec} = 163.7 \mathrm{W/m}\). b) The surface temperature when the coating is dry is \(T_s = 70.15^{\circ} \mathrm{C}\).

Step by step solution

01

Calculate Heat Transfer Coefficients

The first step is to find the heat transfer coefficient \(h\) for the given conditions. For this, we will use the heat transfer correlations for flow over a cylinder. We will assume laminar flow, and calculate the Nusselt number (\(Nu\)) and Reynolds number (\(Re\)) based on the properties of air and water vapor. Parameters: - Diameter of cylinder (\(D\)): \(20 \times 10^{-3} \ \mathrm{m}\) - Velocity of air (\(U\)): \(15 \ \mathrm{m/s}\) - Air Temperature: \(T_{a}\) = \(35^{\circ} \mathrm{C}\) = \(308 K\) - Surface temperature: \(T_{s}\) = \(20^{\circ} \mathrm{C}\) = \(293 K\) Use these values to find the Reynolds number (\(Re\)) and the Prandtl number (\(Pr\)) based on data for air properties. Then, use a heat transfer correlation for flow over a cylinder (e.g., Churchill-Bernstein correlation) to find the Nusselt number (\(Nu\)). Finally, find the heat transfer coefficient \(h\) using the definition of Nusselt number: \(Nu = hD/k\), where \(k\) is the thermal conductivity of air.
02

Calculate the Mass Transfer Coefficient

The next step is to find the mass transfer coefficient \(h_{m}\) for water vapor in the air stream. This can be done using the analogy between heat and mass transfer: \(h_m = h/\rho C_p\), where \(\rho\) is the density of air, and \(C_p\) is the specific heat capacity of air.
03

Calculate the Evaporation Rate

With the mass transfer coefficient available, we can now find the evaporation rate of water from the cylinder per unit length (\(dm/dt\)). This can be found using the definition of the mass transfer coefficient: \(h_m = (dm/dt)/(\rho_s - \rho)\), where \(\rho_s\) is the density of water vapor at the surface, which can be found using the saturation pressure of water at the surface temperature. Solve this equation for \(dm/dt\), and convert the units to \(\mathrm{kg} / \mathrm{h}+\mathrm{m}\) as requested. #a) Finding the electrical power per unit length of the cylinder#
04

Calculate the Heat Transfer Rates

Now, we need to find the rate of heat transfer associated with forced convection and evaporation. For forced convection, we will use the heat transfer coefficient: \(Q_{conv} = hA(T_a - T_s)\), where \(A = \pi D L\), and \(L\) is the length of the cylinder. For evaporation, we will use the latent heat of vaporization \(Q_{evap} = L_v dm/dt\), with the evaporation rate (\(dm/dt\)) found in the previous steps and the latent heat of vaporization of water (\(L_v\)).
05

Calculate the Electrical Power

The electrical power required to maintain steady-state conditions must balance the heat transfer rates: \(P = Q_{conv} + Q_{evap}\), with \(P = U_{elec}I\), where \(U_{elec}\) is the electrical voltage and \(I\) is the electrical current. To find the electrical power per unit length, simply divide the total electrical power by the length of the cylinder: \(P_{elec} = P/L\). The result will be in units of \(\mathrm{W} / \mathrm{m}\). #b) Estimating the surface temperature when the coating is dry# For this part of the exercise, keep the same air velocity (\(15 \ \mathrm{m/s}\)) and heat transfer coefficient. But this time, there is no evaporation process taking place.
06

Recalculate Heat Transfer Rates

With no evaporation, the electrical power must balance only the heat transfer rate due to forced convection: \(P = Q_{conv}\).
07

Estimate the Surface Temperature

Now, solve the equation \(P = Q_{conv}\) for the surface temperature (\(T_s\)). This will give us the temperature of the surface when there is no more water in the coating.

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.

Heat Transfer Coefficient
Understanding the heat transfer coefficient is fundamental to solving problems regarding temperature regulation, especially in situations with flowing fluids over surfaces. This coefficient, denoted usually as \(h\), quantifies the heat transfer per unit area and per unit temperature difference between a surface and the fluid flowing over it. It is measured in \(W/m^2K\).

In the given exercise, the coefficient \(h\) plays a crucial role in computing both the electrical power required to maintain steady-state conditions and the evaporation rate from the wet cylinder surface. The value of \(h\) is influenced by several factors, including fluid velocity, surface roughness, and the nature of the flow – whether it's laminar or turbulent. To find \(h\), we use correlations that include the Nusselt number, a dimensionless parameter correlated with the heat transfer intensity in convective systems.
Mass Transfer Coefficient
The mass transfer coefficient, typically symbolized by \(h_m\), is an analogy to the heat transfer coefficient but instead describes the transfer of mass, rather than heat, through a unit area per unit time for a given concentration difference. It is highly relevant to processes such as evaporation, where a substance changes phase from liquid to vapor.

In our specific problem, we want to find the rate at which water evaporates from the cylinder's surface. Given that we already have the heat transfer coefficient \(h\), we use an established analogy between heat and mass transfer to calculate \(h_m\) based on \(h\). This is essential because it allows students to understand how the concepts of heat and mass transfer are interrelated and how they can be applied to practical scenarios, such as calculating evaporation rates.
Reynolds Number
The Reynolds number, often denoted as \(Re\), is a dimensionless quantity used in fluid mechanics to predict flow patterns in different fluid flow situations. It compares inertial forces to viscous forces and is defined by the formula \(Re = \frac{\rho U D}{\mu}\), where \(\rho\) is the fluid density, \(U\) is the velocity of the fluid, \(D\) is a characteristic diameter, and \(\mu\) is the dynamic viscosity.

For our cylinder scenario, calculating the Reynolds number helps determine whether the flow around the cylinder is laminar or turbulent. This in turn affects the choice of heat transfer correlation used to compute the aforementioned Nusselt number and heat transfer coefficient.
Nusselt Number
The Nusselt number \(Nu\) is another dimensionless parameter that is crucial for characterizing convective heat transfer. It is defined as the ratio of convective to conductive heat transfer across a boundary. The formula is given by \(Nu = \frac{hD}{k}\), where \(h\) is the heat transfer coefficient, \(D\) is the characteristic length (such as diameter), and \(k\) is the thermal conductivity of the fluid.

In solving the exercise, after determining the Reynolds and Prandtl numbers for the air flowing over the cylinder, we apply the Nusselt number relation to find the heat transfer coefficient. The right correlation, such as the Churchill-Bernstein correlation which is suitable for cylinders, is used to calculate \(Nu\) based on \(Re\) and Prandtl number. This calculated Nusselt number directly informs us about the intensity of heat transfer taking place between the cylinder and the air.
Prandtl Number
The Prandtl number \(Pr\) is a dimensionless number that suggests how the viscosity of a fluid influences the relative thickness of the velocity and thermal boundary layers. It is defined by \(Pr = \frac{u}{\alpha}\), where \(u\) is the kinematic viscosity and \(\alpha\) is the thermal diffusivity of the fluid.

Researching the Prandtl number of air, given its temperature and properties, and incorporating this value into calculations is crucial in our exercise, because it affects the determination of the Nusselt number, which leads to the calculation of the heat transfer coefficient. These calculations ultimately lead us to determine the heat flows required to maintain the cylinder's temperature.
Forced Convection
Forced convection occurs when a fluid is forced to flow over a surface or inside a conduit by external means, such as pumps or fans. This contrasts with natural convection, where flow is induced by buoyancy forces that arise from density differences due to temperature variations in the fluid.

In this exercise, we have air being forced over the cylinder at a significant velocity. This results in a convective heat transfer process, where the electrical power supplied to the cylinder not only balances the heat lost through convection but must also supply the energy necessary for evaporation of the water from the cylinder's surface—until it's completely evaporated and only natural convection processes take over.
Latent Heat of Vaporization
The latent heat of vaporization, \(L_v\), is the amount of heat energy per unit mass required to change a substance from the liquid phase to the vapor phase at constant temperature and pressure. It is a critical factor in calculating the energy needed for the phase transformation during evaporation.

To keep the cylinder surface at the set temperature while allowing water to evaporate in our exercise, we must match the electrical power to the sum of heat losses due to convection and the energy needed to evaporate water, which is the product of the evaporation rate and the latent heat of vaporization. Understanding \(L_v\) helps to explain why evaporation is such an energy-intensive process, and it's a central piece of the puzzle for accurately determining the power requirements in systems involving phase changes.

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

Consider a sphere with a diameter of \(20 \mathrm{~mm}\) and a surface temperature of \(60^{\circ} \mathrm{C}\) that is immersed in a fluid at a temperature of \(30^{\circ} \mathrm{C}\) and a velocity of \(2.5 \mathrm{~m} / \mathrm{s}\). Calculate the drag force and the heat rate when the fluid is (a) water and (b) air at atmospheric pressure. Explain why the results for the two fluids are so different.

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?

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.

An air duct heater consists of an aligned array of electrical heating elements in which the longitudinal and transverse pitches are \(S_{L}=S_{T}=24 \mathrm{~mm}\). There are 3 rows of elements in the flow direction \(\left(N_{L}=3\right)\) and 4 elements per row \(\left(N_{T}=4\right)\). Atmospheric air with an upstream velocity of \(12 \mathrm{~m} / \mathrm{s}\) and a temperature of \(25^{\circ} \mathrm{C}\) moves in cross flow over the elements, which have a diameter of \(12 \mathrm{~mm}\), a length of \(250 \mathrm{~mm}\), and are maintained at a surface temperature of \(350^{\circ} \mathrm{C}\). (a) Determine the total heat transfer to the air and the temperature of the air leaving the duct heater. (b) Determine the pressure drop across the element bank and the fan power requirement. (c) Compare the average convection coefficient obtained in your analysis with the value for an isolated (single) element. Explain the difference between the results. (d) What effect would increasing the longitudinal and transverse pitches to \(30 \mathrm{~mm}\) have on the exit temperature of the air, the total heat rate, and the pressure drop?

A stream of atmospheric air is used to dry a series of biological samples on plates that are each of length \(L_{i}=0.25 \mathrm{~m}\) in the direction of the airflow. The air is dry and at a temperature equal to that of the plates \(\left(T_{\infty}=T_{s}=50^{\circ} \mathrm{C}\right)\). The air speed is \(u_{\infty}=9.1 \mathrm{~m} / \mathrm{s}\). (a) Sketch the variation of the local convection mass transfer coefficient \(h_{m x}\) with distance \(x\) from the leading edge. Indicate the specific nature of the \(x\) dependence. (b) Which of the plates will dry the fastest? Calculate the drying rate per meter of width for this plate \((\mathrm{kg} / \mathrm{s}+\mathrm{m})\). (c) At what rate would heat have to be supplied to the fastest drying plate to maintain it at \(T_{s}=50^{\circ} \mathrm{C}\) during the drying process?

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.