/*! 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 55 A pump steadily delivers water t... [FREE SOLUTION] | 91Ó°ÊÓ

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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 is approximately 219.4 kg/s.

Step by step solution

01

- Understand the problem

We need to find the mass flow rate delivered by the pump. Given are: diameters of inlet and nozzle, height difference, pressures, temperature, power input, and gravity.
02

- Convert diameters to areas

Calculate the cross-sectional areas of both the nozzle (A2) and the inlet pipe (A1) using the formula for the area of a circle, \( A = \pi \left( \frac{d}{2} \right)^2 \). For the nozzle: \[ d2 = 2.5 \text{ cm} = 0.025 \text{ m} \] \[ A2 = \pi \left( \frac{0.025}{2} \right)^2 \approx 4.91 \times 10^{-4} \text{ m}^2 \] For the inlet pipe: \[ d1 = 5.0 \text{ cm} = 0.05 \text{ m} \] \[ A1 = \pi \left( \frac{0.05}{2} \right)^2 \approx 1.96 \times 10^{-3} \text{ m}^2 \]
03

- Apply the Bernoulli equation

Apply the Bernoulli equation between the inlet and the nozzle exit. The Bernoulli equation for this problem simplifies as follows, \[ \frac{p_1}{\rho} + g z_1 + \frac{V_1^2}{2} = \frac{p_2}{\rho} + g z_2 + \frac{V_2^2}{2} \] Given that the pressure \( p_1 = p_2 \) and the elevation difference from the pump to the exit \( z_2 - z_1 = 4 \text{ m} \): Rearrange to solve for the velocity at the nozzle exit \( V_2 \) \[ g(z_2 - z_1) = \frac{V_2^2 - V_1^2}{2} \] Since \( V_2 = \frac{Q}{A_2} \) and \( V_1 = \frac{Q}{A_1} \), substitute to find \( V_2 \).
04

- Relate volumetric flow rate to power

Using the power input to the pump \( P = \rho g Q (z_2 - z_1) \), solve for volumetric flow rate, \( Q \): \[ Q = \frac{P}{\rho g (z_2 - z_1)} \] Substituting values \( P = 8.6 \times 10^3 \text{ W} \), \( \rho = 1000 \text{ kg/m}^3 \), \( g = 9.81 \text{ m/s}^2 \), and \( z_2 - z_1 = 4 \text{ m} \): \[ Q = \frac{8.6 \times 10^3}{1000 \times 9.81 \times 4} \approx 0.2194 \text{ m}^3/\text{s} \]
05

- Find mass flow rate

Convert volumetric flow rate to mass flow rate using the formula \( \dot{m} = \rho Q \). Substituting \( Q \approx 0.2194 \text{ m}^3/\text{s} \) and \( \rho = 1000 \text{ kg/m}^3 \): \[ \dot{m} = 1000 \times 0.2194 \approx 219.4 \text{ kg/s} \]

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Key Concepts

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

Bernoulli equation
The Bernoulli equation is a fundamental principle in fluid dynamics that describes the behavior of a moving fluid. It relates the pressure, velocity, and height of the fluid at different points along its flow. In this exercise, the Bernoulli equation enables us to connect the velocity at the pump inlet and the nozzle by considering energy conservation. The simplified form of the Bernoulli equation used here is:

\[ \frac{p_1}{\rho} + g z_1 + \frac{V_1^2}{2} = \frac{p_2}{\rho} + g z_2 + \frac{V_2^2}{2} \]

In this case, we know the pressures (\( p_1 \) and \( p_2 \)) at both points are equal, allowing us to cancel them out. The equation thus relates the height difference between the nozzle and the pump (\( z_2 - z_1 \)) to the kinetic energies at those points, ultimately helping to determine the fluid velocities.
Cross-sectional area
Understanding cross-sectional areas is key to determining various fluid properties like velocity and flow rate. In this exercise, we calculate the areas of the inlet pipe and the nozzle using the formula for the area of a circle:

\[ A = \pi \left( \frac{d}{2} \right)^2 \]

For the nozzle, with a diameter \( d_2 = 2.5 \text{ cm} \):

\[ A_2 = \pi \left( \frac{0.025}{2} \right)^2 \approx 4.91 \times 10^{-4} \text{ m}^2 \]

For the inlet pipe, with a diameter \( d_1 = 5.0 \text{ cm} \):

\[ A_1 = \pi \left( \frac{0.05}{2} \right)^2 \approx 1.96 \times 10^{-3} \text{ m}^2 \]

These areas are crucial for determining the velocities at these points using the relationship between volumetric flow rate and velocity.
Volumetric flow rate
The volumetric flow rate, \( Q \), is the volume of fluid that passes through a cross-sectional area per unit time. It is a key quantity in describing fluid flow and is given by:

\[ Q = \frac{P}{\rho g \left( z_2 - z_1 \right)} \]

Given the problem's values:

\[ P = 8.6 \times 10^3 \text{ W}, \ \rho = 1000 \text{ kg/m}^3, \ g = 9.81 \text{ m/s}^2, \ \left( z_2 - z_1 \right) = 4 \text{ m} \]

The volumetric flow rate is:

\[ Q = \frac{8.6 \times 10^3}{1000 \times 9.81 \times 4} \approx 0.2194 \text{ m}^3/\text{s} \]

This value provides the volume of water being pumped per second, essential for determining the other parameters like velocity and mass flow rate.
Pump power input
Pump power input is the energy supplied to the pump to move the fluid. It's given in watts (W) and in this problem, it's provided as \( 8.6 \text{ kW} \) or \( 8.6 \times 10^3 \text{ W} \). This value is used to calculate the volumetric flow rate using the formula:

\[ Q = \frac{P}{\rho g \left( z_2 - z_1 \right)} \]

The power input indicates how much work the pump does to move the water through the height difference \( z_2 - z_1 \). By knowing this, we can understand how effective the pump is in generating the necessary flow rate, which directly influences the velocities and eventual mass flow rate.
Fluid dynamics
Fluid dynamics involves the study of fluids (liquids and gases) and the forces acting on them. In this problem, fluid dynamics principles help us understand how the pump pushes water through the hose and nozzle. Key concepts include:
  • Velocity: Speed of water at both the inlet and outlet.
  • Pressure: Constant in this exercise but crucial in many fluid flow problems.
  • Flow rate: Combines velocity and cross-sectional area.
  • Energy conservation: Basis of Bernoulli's equation.
Incorporating these ideas allows us to apply the Bernoulli equation and calculate velocities using the known pump power, elevation difference, and areas. This comprehensive approach ensures accurate calculations and a deeper understanding of fluid behavior.

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Most popular questions from this chapter

Carbon dioxide gas enters a well-insulated diffuser at \(138 \mathrm{kPa}, 278 \mathrm{~K}\), with a velocity of \(244 \mathrm{~m} / \mathrm{s}\) through a flow area of \(9 \mathrm{~cm}^{2}\). At the exit, the flow area is 30 times the inlet area, and the velocity is \(6 \mathrm{~m} / \mathrm{s}\). The potential energy change from inlet to exit is negligible. For steady-state operation, determine the exit temperature, in \({ }^{\circ} \mathrm{K}\), the exit pressure, in \(\mathrm{kPa}\), and the mass flow rate, in \(\mathrm{kg} / \mathrm{s}\).

Air expands through a turbine operating at steady state on an instrumented test stand. At the inlet, \(p_{1}=1103 \mathrm{kPa}\), \(T_{1}=867 \mathrm{~K}\), and at the exit, \(p_{2}=102 \mathrm{kPa}\). The mass flow rate of air entering the turbine is \(4.8 \mathrm{~kg} / \mathrm{s}\), and the power developed is measured as \(1900 \mathrm{~kW}\). Neglecting heat transfer and kinetic and potential energy effects, determine the exit temperature, \(T_{2}\), in \({ }^{\circ} \mathrm{K}\).

Why is it that when air at \(1 \mathrm{~atm}\) is throttled to a pressure of \(0.5 \mathrm{~atm}\), its temperature at the valve exit is close to the temperature at the valve inlet, yet when air at \(1 \mathrm{~atm}\) leaks into an insulated, rigid, initially evacuated tank until the tank pressure is \(0.5 \mathrm{~atm}\), the temperature of the air in the tank is greater than the air temperature outside the tank?

At steady state, a stream of liquid water at \(20^{\circ} \mathrm{C}, 1 \mathrm{bar}\) is mixed with a stream of ethylene glycol \((M=62.07)\) to form a refrigerant mixture that is \(50 \%\) glycol by mass. The water molar flow rate is \(4.2 \mathrm{kmol} / \mathrm{min}\). The density of ethylene glycol is \(1.115\) times that of water. Determine (a) the molar flow rate, in \(\mathrm{kmol} / \mathrm{min}\), and volumetric flow rate, in \(\mathrm{m}^{3} / \mathrm{min}\), of the entering ethylene glycol. (b) the diameters, in \(\mathrm{cm}\), of each of the supply pipes if the velocity in each is \(2.5 \mathrm{~m} / \mathrm{s}\).

Air enters a water-jacketed air compressor operating at steady state with a volumetric flow rate of \(37 \mathrm{~m}^{3} / \mathrm{min}\) at \(136 \mathrm{kPa}, 305 \mathrm{~K}\) and exits with a pressure of \(680 \mathrm{kPa}\) and a temperature of \(400 \mathrm{~K}\). The power input to the compressor is \(155 \mathrm{~kW}\). Energy transfer by heat from the compressed air to the cooling water circulating in the water jacket results in an increase in the temperature of the cooling water from inlet to exit with no change in pressure. Heat transfer from the outside of the jacket as well as all kinetic and potential energy effects can be neglected. (a) Determine the temperature increase of the cooling water, in \(\mathrm{K}\), if the cooling water mass flow rate is \(82 \mathrm{~kg} / \mathrm{min}\). (b) Plot the temperature increase of the cooling water, in \(\mathrm{K}\), versus the cooling water mass flow rate ranging from 75 to \(90 \mathrm{~kg} / \mathrm{min}\).

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