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Water vapor at \(0^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\) is flowing over a flat plate at a velocity of \(10 \mathrm{~m} / \mathrm{s}\). Using appropriate software, determine the effect of the location along the plate \((x)\) on the velocity and thermal boundary layer thicknesses. By varying \(x\) for $0

Short Answer

Expert verified
Answer: As the location along the flat plate (x) increases, both the velocity and thermal boundary layer thicknesses grow. The growth may be more rapid in the initial stages, while at further distances, the growth rate may start to stabilize. This behavior is significant in understanding fluid dynamics and heat transfer phenomena.

Step by step solution

01

Identifying key parameters

The key parameters to analyze are the effect of x (the location along the plate) on the velocity and thermal boundary layer thicknesses. The given information includes the temperature \(0^{\circ} \mathrm{C}\), pressure \(1 \mathrm{~atm}\), and velocity \(10 \mathrm{~m} / \mathrm{s}\) for water vapor flow.
02

Select appropriate software

For this exercise, appropriate software needs to be selected, such as ANSYS Fluent, MATLAB, or a similar program that can handle fluid dynamics and heat transfer simulations. It is essential to choose software familiar to the student and capable of performing the necessary calculations.
03

Setup the simulation in the software

Set up the simulation by entering the given parameters: temperature, pressure, and velocity of the water vapor flow. Create a flat plate geometry, with x ranging from \(0\) to \(0.5 \mathrm{~m}\).
04

Run the simulation and determine boundary layer thicknesses

Execute the simulation for various x values between the given range (\(0 < x \leq 0.5 \mathrm{~m}\)). Ensure to capture both the velocity and thermal boundary layer thicknesses as a function of \(x\).
05

Plot the results

Use the obtained data from the simulation to create a plot of the velocity and thermal boundary layer thicknesses versus x. This can be done using the plotting tools available in the selected software.
06

Analysis and interpretation of results

Analyze the generated plot: as \(x\) increases, both the velocity and thermal boundary layer thicknesses will grow. In the initial stages, the growth may display more rapid behavior, while at further distances, the growth rate may start to stabilize. Discuss the implications of these behaviors in the context of fluid dynamics and heat transfer. By following these steps, the student will be able to understand the effect of the location along the plate \((x)\) on the velocity and thermal boundary layer thicknesses and create a graphical representation of these dependencies for given operating conditions.

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Most popular questions from this chapter

Atmospheric air with a velocity of \(10 \mathrm{~m} / \mathrm{s}\) and a temperature of \(20^{\circ} \mathrm{C}\) is in parallel flow over a flat heater surface which is maintained at \(80^{\circ} \mathrm{C}\). The surface area of the heater is \(0.30 \mathrm{~m}^{2}\). The drag force induced by the airflow on the heater is measured to be \(0.2 \mathrm{~N}\). Using the momentum-heat transfer analogy, determine the electrical power needed to maintain the prescribed heater surface temperature of \(80^{\circ} \mathrm{C}\). Evaluate the air properties at \(50^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\).

Consider a laminar ideal gas flow over a flat plate, where the local Nusselt number can be expressed as $\mathrm{Nu}_{x}=0.332 \mathrm{Re}_{x}^{1 / 2} \operatorname{Pr}^{1 / 3}$. Using the expression for the local Nusselt number, show that it can be rewritten in terms of local convection heat transfer coefficient as \(h_{x}=C[V /(x T)]^{w}\), where \(C\) and \(m\) are constants.

An airfoil with a characteristic length of \(0.2 \mathrm{ft}\) is placed in airflow at 1 atm and \(60^{\circ} \mathrm{F}\) with free stream velocity of $150 \mathrm{ft} / \mathrm{s}\( and convection heat transfer coefficient of \)21 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2} \cdot{ }^{\circ} \mathrm{F}$. If a second airfoil with a characteristic length of \(0.4 \mathrm{ft}\) is placed in the airflow at \(1 \mathrm{~atm}\) and \(60^{\circ} \mathrm{F}\) with free stream velocity of \(75 \mathrm{ft} / \mathrm{s}\), determine the heat flux from the second airfoil. Both airfoils are maintained at a constant surface temperature of \(180^{\circ} \mathrm{F}\).

What does the friction coefficient represent in flow over a flat plate? How is it related to the drag force acting on the plate?

A \(15-\mathrm{cm} \times 20\)-cm circuit board is being cooled by forced convection of air at \(1 \mathrm{~atm}\). The heat from the circuit board is estimated to be \(1000 \mathrm{~W} / \mathrm{m}^{2}\). If the airstream velocity is \(3 \mathrm{~m} / \mathrm{s}\) and the shear stress of the circuit board surface is \(0.075 \mathrm{~N} / \mathrm{m}^{2}\), determine the temperature difference between the circuit board surface temperature and the airstream temperature. Evaluate the air properties at \(40^{\circ} \mathrm{C}\) and $1 \mathrm{~atm}$.

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