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In flow over a surface, velocity and temperature profiles are of the forms $$ \begin{aligned} &u(y)=A y+B y^{2}-C y^{3} \quad \text { and } \\ &T(y)=D+E y+F y^{2}-G y^{3} \end{aligned} $$ where the coefficients \(A\) through \(G\) are constants. Obtain expressions for the friction coefficient \(C_{f}\) and the convection coefficient \(h\) in terms of \(u_{z}, T_{x}\), and appropriate profile coefficients and fluid properties.

Short Answer

Expert verified
The friction coefficient, \(C_f\), and convection coefficient, \(h\), for a fluid flow over a surface with given velocity and temperature profiles, can be determined as follows: \( C_f = \frac{2 \mu A}{\rho u_z^2} \) \( h = -\frac{kE}{T_x} \) where \(A\) and \(E\) are constants in the velocity and temperature profiles, respectively; \(\mu\) is the dynamic viscosity; \(\rho\) is the fluid density; \(u_z\) is the free-stream velocity; \(k\) is the fluid's thermal conductivity; and \(T_x\) is the difference in temperature between the surface and the fluid.

Step by step solution

01

Calculate the derivative of the velocity profile, \(u'(y)\)

To determine the shear stress at the wall, we need to find the rate of change of the velocity profile with respect to \(y\). Doing this, we find: \( u'(y) = \frac{du}{dy} = A + 2By - 3Cy^2 \)
02

Calculate shear stress at the wall, \(\tau_w\)

Shear stress at the wall, \(\tau_w\) is obtained by evaluating \(u'(y)\) at \(y = 0\). This gives: \( \tau_w = \mu u'(0) = \mu A \) where \(\mu\) is the dynamic viscosity of the fluid.
03

Calculate the friction coefficient, \(C_f\)

The friction coefficient, \(C_f\) is defined as: \( C_f = \frac{2 \tau_w}{\rho u_z^2} \) Substituting the expression for the shear stress at the wall, \(\tau_w\), we get: \( C_f = \frac{2 \mu A}{\rho u_z^2} \) Where \(u_z\) is the free stream velocity and \(\rho\) is the fluid density.
04

Calculate the derivative of the temperature profile, \(T'(y)\)

To determine the convection coefficient, we need to find the temperature gradient along the surface. This is obtained by differentiating the temperature profile with respect to \(y\): \( T'(y) = \frac{dT}{dy} = E + 2Fy - 3Gy^2 \)
05

Calculate heat flux at the wall, \(q_w\)

The heat flux at the wall, \(q_w\), is obtained by evaluating the derivative of the temperature (\(T'(y)\)) at \(y = 0\). The heat flux is given as: \( q_w = -k T'(0) = -kE []) where \(k\) is the fluid's thermal conductivity.
06

Calculate the convection coefficient, \(h\)

The convection heat transfer coefficient, \(h\), can be calculated using the expression for the heat flux at the wall, \(q_w\), as follows: \( h = \frac{q_w}{T_x} \) Substituting the expression for \(q_w\), we get: \( h = -\frac{kE}{T_x} \) where \(T_x\) is the difference in temperature between the surface and the fluid. The expressions for friction coefficient, \(C_f\), and convection coefficient, \(h\), are: \( C_f = \frac{2 \mu A}{\rho u_z^2} \) \( h = -\frac{kE}{T_x} \)

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Key Concepts

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

Velocity and Temperature Profiles
In fluid mechanics and heat transfer, understanding how the velocity and temperature of a fluid change within the boundary layer over a surface is crucial for analyzing and designing systems involving flow and heat exchange. The velocity profile, often denoted as u(y), describes how the speed of the fluid varies with the distance y from the surface. Similarly, the temperature profile, T(y), represents the temperature variation across the boundary layer.

These profiles are crucial because they directly affect the heat transfer rate and the frictional forces experienced by the surface. The profiles given by the equations \[u(y)=Ay+By^2-Cy^3\] and \[T(y)=D+Ey+Fy^2-Gy^3\]involve constants that are indicative of the specific flow and thermal conditions of the system. Appropriate manipulation of these profiles allows engineers to predict the behavior of fluid flows and their thermal interactions with surfaces, leading to essential calculations, such as the friction and convection coefficients.
Friction Coefficient Calculation
The friction coefficient, often denoted as C_f, plays a pivotal role in predicting the resistance a fluid flow encounters as it moves adjacent to a surface. This resistance is due to shear stress, which arises from viscous interactions between fluid layers moving at different velocities. To calculate C_f, an understanding of the fluid's velocity profile and its derivative is needed, as the shear stress is directly related to the rate of change of the velocity at the wall.

The calculation often begins with finding the gradient of the velocity profile at the wall, u'(y), which is evaluated at y=0. This gradient is then used to determine the shear stress, Ï„³å·É, through the relationship involving the fluid's dynamic viscosity, μ. The friction coefficient is subsequently obtained by normalizing the shear stress using the fluid's density, ÒÏ, and the free-stream velocity, u_z. The relevant formula is given by \[C_f = \frac{2 \mu A}{\rho u_z^2}\].
Convection Coefficient Determination
The convection coefficient, denoted as h, is an essential parameter in the study of convection heat transfer. It quantifies the heat transfer rate between a surface and a fluid moving over it. The temperature profile's gradient at the surface, T'(y), provides information on the temperature change rate needed to compute heat flux, q_w, at the wall by utilizing the fluid's thermal conductivity, k.

This heat flux is then used to determine the convection heat transfer coefficient, h, by relating the heat flux to the temperature difference, T_x, between the surface and the fluid. The formula is given as \[h = -\frac{kE}{T_x}\]. Understanding the convection coefficient is vital for engineers to design efficient cooling or heating systems involving fluid flows.
Fluid Properties in Heat Transfer
Fluid properties such as dynamic viscosity (μ), density (ÒÏ), and thermal conductivity (k) are fundamental parameters influencing heat transfer processes. Dynamic viscosity is a measure of a fluid's resistance to flow and is essential in calculating shear stress and the friction coefficient. Density is a measure of a fluid's mass per unit volume and plays a role in various fluid flow equations, including those related to momentum and energy exchange.

Thermal conductivity describes the material's ability to conduct heat and is a key factor in determining the rate of heat transfer through conduction. Each of these properties may vary with temperature, pressure, and fluid composition, making the understanding of these properties imperative when analyzing and calculating heat transfer and fluid flow phenomena.

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Most popular questions from this chapter

Consider conditions for which a fluid with a free stream velocity of \(V=1 \mathrm{~m} / \mathrm{s}\) flows over an evaporating or subliming surface with a characteristic length of \(L=1 \mathrm{~m}\), providing an average mass transfer convection coefficient of \(\bar{h}_{\mathrm{m}}=10^{-2} \mathrm{~m} / \mathrm{s}\). Calculate the dimensionless parameters \(\overline{S h}_{L}, R e_{L}, S c\), and \(j_{m}\) for the following combinations: airflow over water, airflow over naphthalene, and warm glycerol over ice. Assume a fluid temperature of \(300 \mathrm{~K}\) and a pressure of \(1 \mathrm{~atm}\).

If laminar flow is induced at the surface of a disk due to rotation about its axis, the local convection coefficient is known to be a constant, \(h=C\), independent of radius. Consider conditions for which a disk of radius \(r_{o}=100 \mathrm{~mm}\) is rotating in stagnant air at \(T_{\infty}=20^{\circ} \mathrm{C}\) and a value of \(C=20 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) is maintained. If an embedded electric heater maintains a surface temperature of \(T_{x}=50^{\circ} \mathrm{C}\), what is the local heat flux at the top surface of the disk? What is the total electric power requirement? What can you say about the nature of boundary layer development on the disk?

It is known that on clear nights the air temperature need not drop below \(0^{\circ} \mathrm{C}\) before a thin layer of water on the ground will freeze. Consider such a layer of water on a clear night for which the effective sky temperature is \(-30^{\circ} \mathrm{C}\) and the convection heat transfer coefficient due to wind motion is \(h=25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The water may be assumed to have an emissivity of \(1.0\) and to be insulated from the ground as far as conduction is concerned. (a) Neglecting evaporation, determine the lowest temperature the air can have without the water freezing. (b) For the conditions given, estimate the mass transfer coefficient for water evaporation \(h_{\mathrm{m}}(\mathrm{m} / \mathrm{s})\). (c) Accounting now for the effect of evaporation, what is the lowest temperature the air can have without the water freezing? Assume the air to be dry.

The defroster of an automobile functions by discharging warm air on the inner surface of the windshield. To prevent condensation of water vapor on the surface, the temperature of the air and the surface convection coefficient \(\left(T_{\infty, j}, \overline{h_{i}}\right)\) must be large enough to maintain a surface temperature \(T_{s i}\) that is at least as high as the dewpoint \(\left(T_{s, i} \geq T_{d \mathrm{p}}\right)\). Consider a windshield of length \(L=800 \mathrm{~mm}\) and thickness \(t=6 \mathrm{~mm}\) and driving conditions for which the vehicle moves at a velocity of \(V=70 \mathrm{mph}\) in ambient air at \(T_{\infty \rho}=-15^{\circ} \mathrm{C}\). From laboratory experiments performed on a model of the vehicle, the average convection coefficient on the outer surface of the windshield is known to be correlated by an expression of the form \(\overline{N_{L}}=0.030 \operatorname{Re}_{L}^{0.8} \operatorname{Pr}^{1 / 3}\), where \(R e_{L}=V L \nu\). Air properties may be approximated as \(k=0.023 \mathrm{~W} / \mathrm{m}=\mathrm{K}\), \(v=12.5 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}\), and \(\operatorname{Pr}=0.71\). If \(T_{d p}=10^{\circ} \mathrm{C}\) and \(T_{m, j}=50^{\circ} \mathrm{C}\), what is the smallest value of \(\bar{h}_{j}\) required to prevent condensation on the inner surface?

Species A is evaporating from a flat surface into species B. Assume that the concentration profile for species A in the concentration boundary layer is of the form \(C_{\mathrm{A}}(y)=D y^{2}+E y+F\), where \(D, E\), and \(F\) are constants at any \(x\)-location and \(y\) is measured along a normal from the surface. Develop an expression for the mass transfer convection coefficient \(h_{w}\) in terms of these constants, the concentration of \(A\) in the free stream \(C_{\mathrm{A}, \infty}\) and the mass diffusivity \(D_{\mathrm{AB}}\). Write an expression for the molar flux of mass transfer by convection for species \(A\).

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