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In a mixing chamber, Carbon dioxide flows into the tank at \(A\) at \(V_{A}=12 \mathrm{~m} / \mathrm{s}\), and nitrogen flows in at \(B\) at \(V_{B}=6 \mathrm{~m} / \mathrm{s}\). Both enter at a gage pressure of \(310 \mathrm{kPa}\) and a temperature of \(260^{\circ} \mathrm{C}\). Determine the average velocity of the mixed gas at \(C\). The mixture has a density of \(\rho=1.546 \mathrm{~kg} / \mathrm{m}^{3}\).

Short Answer

Expert verified
The average velocity of the mixed gas at point C can be found via the continuity equation. It's a weighted average based on the mass flow rates at points A and B.

Step by step solution

01

Calculate the mass flow rates

We calculate the mass flow rates at points A and B using the equation: \(\dot{m}=\rho \times V\), where \(\dot{m}\) represents the mass flow rate, \(\rho\) stands for the gas density and V is the velocity. The density \(\rho\) is given as 1.546 kg/m^3, the velocity at point A (\(V_A\)) is 12 m/s and at point B (\(V_B\)) is 6 m/s. Thus, we get \(\dot{m}_A = \rho \times V_A = 1.546 \times 12\) kg/s and \(\dot{m}_B = \rho \times V_B = 1.546 \times 6\) kg/s.
02

Calculate the total mass flow rate

The total mass flow rate \(\dot{m}_{total}\) is the sum of the mass flow rates at points A and B, i.e., \(\dot{m}_{total} = \dot{m}_A + \dot{m}_B\).
03

Calculate the velocity at C

The continuity equation states that the mass flow rate must be the same at all points in a pipe system. Thus, the velocity at point C (\(V_C\)) can be calculated using the equation \(\dot{m}_{total} = \rho \times V_C\), where \(\rho\) is the density of the mixture and \(V_C\) is the velocity at point C. Rearranging for \(V_C\), we get \(V_C = \frac{\dot{m}_{total}}{\rho}\).

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Key Concepts

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

Mass Flow Rate
The mass flow rate, denoted as \( \dot{m} \), is a key concept in fluid mechanics. It corresponds to the amount of mass passing through a given surface per time unit. It's often described with the simple equation \( \dot{m} = \rho \times V \), where \( \rho \) signifies the fluid's density and \( V \) the flow velocity. In practical applications, knowing the mass flow rate is essential for calculations involving chemical reactions, heating or cooling processes, and even for determining the power of a jet engine. Imagine liquid in a pipe or gas through an air duct; the mass flow rate would tell us how much of that fluid is moving through the system, enabling us to design and control the process efficiently.

Understanding mass flow rate is also crucial in our original exercise, allowing us to determine how much Carbon dioxide and nitrogen enter the mixing chamber. Thereby, ensuring the proper mixture of gases for industrial processes or environmental controls.
Continuity Equation
The continuity equation is a fundamental principle in fluid dynamics, representing the conservation of mass. This mathematical statement ensures that the mass flow rate for an incompressible fluid remains constant along a pipeline. In essence, what goes into a pipe must come out, provided the fluid is not being added or removed in the middle. The continuity equation can be expressed in its simplest form as \( A_1V_1 = A_2V_2 \) for an incompressible flow, where \( A \) is the cross-sectional area and \( V \) is the velocity.

When applied to gases, a modified version accounts for changes in density due to pressure and temperature variations. In our example, the equation allows us to calculate the velocity of the mixed gases at point C by ensuring that the mass flow into the chamber equals the mass flow out at any given point.
Gas Density
Gas density \(\rho\) is another crucial factor in fluid mechanics, significantly influencing the behaviors of gases in various conditions. Density is defined as mass per unit volume and is affected by temperature, pressure, and the gas's molecular structure. For instance, colder gases are denser, assuming pressure remains constant. High pressures, conversely, can compress a gas and increase its density, given a constant temperature.

However, gases are compressible, meaning their density can change significantly with varying temperature and pressure—distinguishing them from liquids. Our exercise specifies the density of the mixed gas, which is critical in calculating both the mass flow rates and the exit velocity at point C.
Velocity of Fluids
Velocity in fluid mechanics describes how swiftly a fluid's particles travel through space. It's one of the vital parameters since it affects other factors such as flow rate and dynamic pressure. The velocity of fluids can vary extensively within a system due to changes in diameter, obstructions, or manipulations in flow direction, adhering to the principles like Bernoulli's equation and the continuity equation.

In our scenario, the exercise necessitates finding the average velocity of a mixed gas at a certain point, requiring the integration of the mass flow rate and gas density. The velocities at the inlet points may vary, but the continuity equation helps us determine the resultant velocity, thereby achieving a balanced and controlled system.

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Most popular questions from this chapter

The jet engine is moving forward with a constant speed of \(800 \mathrm{~km} / \mathrm{h}\). Fuel from a tank enters the engine and is mixed with the intake air, burned, and exhausted with an average relative velocity of \(1200 \mathrm{~km} / \mathrm{h}\). Outline the control volume as the jet engine and the air and fuel within it. For an analysis, why is it best to consider this control volume to be moving? Indicate the open control surfaces, and show the positive direction of their areas. Also, indicate the magnitudes of the relative velocities and their directions through these surfaces. Identify the local and convective changes that occur. Assume the fuel is incompressible and the air is compressible.

Water is drawn steadily through the pump. The average velocities are indicated. Select a control volume that contains the water in the pump and extends slightly past it. Indicate the open control surfaces, and show the positive direction of their areas. Also, indicate the direction of the velocities through these surfaces. Identify the local and convective changes that occur. Assume water to be incompressible.

The 2 -m-diameter cylindrical emulsion tank is being filled at \(A\) with cyclohexanol at an average rate of \(V_{A}=4 \mathrm{~m} / \mathrm{s}\) and at \(B\) with thiophene at an average rate of \(V_{B}=2 \mathrm{~m} / \mathrm{s}\). Determine the rate at which the depth of the mixture is increasing when \(h=1 \mathrm{~m} .\) Also, what is the average density of the mixture? Take \(\rho_{c y}=779 \mathrm{~kg} / \mathrm{m}^{3},\) and \(\rho_{t}=1051 \mathrm{~kg} / \mathrm{m}^{3}\)

Compressed air is being released from the tank, and at the instant shown it has a velocity of \(3 \mathrm{~m} / \mathrm{s}\). Select a control volume that contains the air in the tank. Indicate the open control surface, and show the positive direction of its area. Also, indicate the direction of the velocity through this surface. Identify the local and convective changes that occur. Assume the air to be compressible.

The average velocities of water flowing steadily through the nozzle are indicated. If the nozzle is connected onto the end of the hose, outline the control volume to be the entire nozzle and the water inside it. Also, select another control volume to be just the water inside the nozzle. In each case, indicate the open control surfaces, and show the positive direction of their areas. Specify the direction of the velocities through these surfaces. Identify the local and convective changes that occur. Assume water to be incompressible.

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