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A pump steadily delivers water through a hose terminated by a nozzle. The exit of the nozzle has a diameter of \(2.5 \mathrm{~cm}\) and is located \(4 \mathrm{~m}\) above the pump inlet pipe, which has a diameter of \(5.0 \mathrm{~cm}\). The pressure is equal to 1 bar at both the inlet and the exit, and the temperature is constant at \(20^{\circ} \mathrm{C}\). The magnitude of the power input required by the pump is \(8.6 \mathrm{~kW}\), and the acceleration of gravity is \(g=9.81 \mathrm{~m} / \mathrm{s}^{2}\). Determine the mass flow rate delivered by the pump, in \(\mathrm{kg} / \mathrm{s}\).

Short Answer

Expert verified
The mass flow rate delivered by the pump is approximately 4.48 kg/s.

Step by step solution

01

Define the known variables

List all the known values: - Inlet diameter, \(D_1 = 5.0 \text{ cm} = 0.05 \text{ m}\) - Nozzle exit diameter, \(D_2 = 2.5 \text{ cm} = 0.025 \text{ m}\) - Height difference, \(z = 4 \text{ m}\) - Pressure at inlet and exit, \(P = 1 \text{ bar} = 100000 \text{ Pa}\) - Power input, \(P_{\text{pump}} = 8.6 \text{ kW} = 8600 \text{ W}\) - Gravity, \(g = 9.81 \text{ m/s}^2\) - Temperature, \(T = 20^\text{°}C\) - Density of water at \(20^\text{°}C\), \(\rho = 998 \text{ kg/m}^3\)
02

Calculate the cross-sectional areas

Compute the cross-sectional areas at the inlet and the exit: Given the diameter at each point, use the formula for the area of a circle, \(A = \pi \frac{D^2}{4}\): For the inlet, \(D_1 = 0.05 \text{ m}\): \(A_1 = \pi \frac{(0.05)^2}{4} = 1.9635 \times 10^{-3} \text{ m}^2\) For the nozzle exit, \(D_2 = 0.025 \text{ m}\): \(A_2 = \pi \frac{(0.025)^2}{4} = 4.9087 \times 10^{-4} \text{ m}^2\)
03

Apply Bernoulli’s Equation

Utilize Bernoulli’s equation to relate the fluid dynamic properties between two points along the streamline: \[ \frac{{P_1}}{{\rho}} + \frac{{v_1^2}}{{2}} + gz_1 = \frac{{P_2}}{{\rho}} + \frac{{v_2^2}}{{2}} + gz_2 \] Since \(P_1 = P_2 = 100000 \text{ Pa}\) and \(z_1 = 0 \text{ m}\) while \(z_2 = 4 \text{ m}\): \[ 0 + \frac{{v_1^2}}{{2}} = \frac{{v_2^2}}{{2}} + (4 \times 9.81) \] Hence, after simplification: \[ \frac{{v_1^2}}{{2}} = \frac{{v_2^2}}{{2}} + 39.24 \] Solve for \(v_1\) in terms of \(v_2\): \[ v_1^2 = v_2^2 + 78.48 \]
04

Apply Continuity Equation

By using the continuity equation, the relationship can be established between the velocities and cross-sectional areas: \[ A_1 v_1 = A_2 v_2 \] Substitute \(A_1\) and \(A_2\) into the equation: \[ 1.9635 \times 10^{-3} v_1 = 4.9087 \times 10^{-4} v_2 \] Solve for \(v_1\): \[ v_1 = \frac{ 4.9087 \times 10^{-4} v_2 }{ 1.9635 \times 10^{-3}} = 0.25 v_2 \] Also, substitute \(v_1 = 0.25v_2\) into the Bernoulli’s equation from Step 3: \[ (0.25v_2)^2 = v_2^2 + 78.48 \rightarrow 0.0625v_2^2 = v_2^2 + 78.48 \rightarrow 0.9375v_2^2 = 78.48 \rightarrow v_2^2 = 83.66 \rightarrow v_2 \approx 9.14 \text{ m/s} \]
05

Solve for \(v_1\)

Using the continuity equation value substituted for \(v_1\): \[ v_1 = 0.25 \times v_2 = 0.25 \times 9.14 \approx 2.285 \text{ m/s} \]
06

Calculate the mass flow rate

Use the relation \(\dot{m} = \rho A_1 v_1\): \[ \dot{m} = 998 \times 1.9635 \times 10^{-3} \times 2.285 \] Compute the product: \[ \dot{m} \approx 4.48 \text{ kg/s} \]

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Key Concepts

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

Bernoulli’s equation
Bernoulli’s equation is a fundamental principle in fluid dynamics that helps us understand how fluid properties like pressure, velocity, and height change along a streamline. It’s particularly useful when analyzing fluid flow through pumps and hoses. The equation is expressed as:
\[ \frac{{P_1}}{{\rho}} + \frac{{v_1^2}}{{2}} + gz_1 = \frac{{P_2}}{{\rho}} + \frac{{v_2^2}}{{2}} + gz_2 \]
Where:
  • \( P_1 \) and \( P_2 \) are the fluid pressures at two points
  • \( \rho \) is the fluid density
  • \( v_1 \) and \( v_2 \) are the fluid velocities
  • \( z_1 \) and \( z_2 \) are the heights above a reference level
  • \( g \) is the acceleration due to gravity
By simplifying the equation appropriately, we can find unknowns such as the velocity of the fluid at different points which is crucial for determining the mass flow rate.
Continuity equation
The continuity equation ensures that the mass flow rate is conserved in a fluid flow. For incompressible fluids like water, it tells us that the product of cross-sectional area and velocity remains constant. Mathematically, it is represented as:
\[ A_1 v_1 = A_2 v_2 \]
Where:
  • \( A_1 \) and \( A_2 \) are the cross-sectional areas at two points
  • \( v_1 \) and \( v_2 \) are the velocities at these points
This is particularly useful for calculating the velocity at the nozzle exit when the diameter and initial velocity are known.
Fluid dynamics
Fluid dynamics is the study of how fluids (liquids and gases) move. Understanding fluid dynamics allows us to analyze the behavior of fluids in various situations, such as the flow through pipes and nozzles. When utilizing the principles of fluid dynamics, concepts like Bernoulli’s equation and the continuity equation become invaluable. These principles help explain how variables like pressure, velocity, and height influence fluid flow within different regions of a system.
Cross-sectional area calculation
To determine the velocity and mass flow rate of fluid, it's essential to calculate the cross-sectional area of the points where measurements are made. The area for a circular pipe or nozzle can be found using the formula:
\[ A = \frac{{\text{π} D^2}}{4} \]
Where:
  • \( A \) is the cross-sectional area
  • \( D \) is the diameter
  • π (pi) is approximately 3.14159
Accurate calculation of areas is crucial in applying the continuity equation. For instance, in the exercise, the areas were needed to find fluid velocities at different sections of the hose.
Density of water
The density of water is a significant property when performing fluid dynamic calculations. At 20°C, water has a density of approximately 998 kg/m³. This value is essential when using Bernoulli’s equation and the mass flow rate formula:
\[ \text{Mass flow rate} = \rho A v \]
Where:
  • \( \rho \) is the fluid density
  • \( A \) is the cross-sectional area
  • \( v \) is the fluid velocity
Understanding the density helps in determining the amount of fluid mass flowing through the system per unit time. It’s a key factor when transitioning from volume flow rate to mass flow rate.

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Most popular questions from this chapter

Methods for measuring mass flow rates of gases and liquids flowing in pipes and ducts include: rotameters, turbine flowmeters, orifice-type flowmeters, thermal flowmeters, and Coriolis-type flowmeters. Determine the principles of operation of each of these flow-measuring devices. Consider the suitability of each for measuring liquid or gas flows. Can any be used for two-phase liquid- vapor mixtures? Which measure volumetric flow rate and require separate measurements of pressure and temperature to determine the state of the substance? Summarize your findings in a brief report.

Nitrogen gas is contained in a rigid 1-m tank, initially at 10 bar, \(300 \mathrm{~K}\). Heat transfer to the contents of the tank occurs until the temperature has increased to \(400 \mathrm{~K}\). During the process, a pressure-relief valve allows nitrogen to escape, maintaining constant pressure in the tank. Neglecting kinetic and potential energy effects, and using the ideal gas model with constant specific heats evaluated at \(350 \mathrm{~K}\), determine the mass of nitrogen that escapes, in \(\mathrm{kg}\), and the amount of energy transfer by heat, in \(\mathrm{kJ}\).

Air enters a 0.6-m-diameter fan at \(16^{\circ} \mathrm{C}, 101 \mathrm{kPa}\), and is discharged at \(18^{\circ} \mathrm{C}, 105 \mathrm{kPa}\), with a volumetric flow rate of \(0.35 \mathrm{~m}^{3} / \mathrm{s}\). Assuming ideal gas behavior, determine for steadystate operation (a) the mass flow rate of air, in \(\mathrm{kg} / \mathrm{s}\). (b) the volumetric flow rate of air at the inlet, in \(\mathrm{m}^{3} / \mathrm{s}\). (c) the inlet and exit velocities, in \(\mathrm{m} / \mathrm{s}\).

Pumped-hydraulic storage power plants use relatively inexpensive off-peak baseload electricity to pump water from a lower reservoir to a higher reservoir. During periods of peak demand, electricity is produced by discharging water from the upper to the lower reservoir through a hydraulic turbinegenerator. A single device normally plays the role of the pump during upper-reservoir charging and the turbine-generator during discharging. The ratio of the power developed during discharging to the power required for charging is typically much less than \(100 \%\). Write a report describing the features of the pump-turbines used for such applications and their size and cost. Include in your report a discussion of the economic feasibility of pumped-hydraulic storage power plants,

A control volume has one inlet and one exit. The mass flow rates in and out are, respectively, \(\dot{m}_{i}=1.5\) and \(\dot{m}_{\mathrm{e}}=\) \(1.5\left(1-e^{-0.002}\right.\) ), where \(t\) is in seconds and \(\dot{m}\) is in \(\mathrm{kg} / \mathrm{s}\). Plot the time rate of change of mass, in \(\mathrm{kg} / \mathrm{s}\), and the net change in the amount of mass, in \(\mathrm{kg}\), in the control volume versus time, in s, ranging from 0 to \(3600 \mathrm{~s}\).

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