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When air enters a diffuser and decelerates, does its pressure increase or decrease?

Short Answer

Expert verified
The pressure increases.

Step by step solution

01

Understanding a Diffuser

A diffuser is a device that slows down the speed of an incoming fluid, such as air, causing it to decelerate.
02

Applying Bernoulli's Principle

According to Bernoulli's principle, within a streamline flow of an incompressible fluid, an increase in the flow speed occurs simultaneously with a decrease in pressure and vice versa.
03

Analyzing Air Deceleration

When air decelerates in a diffuser, its speed decreases. Based on Bernoulli's principle, if the velocity of the air decreases, the pressure must increase.
04

Concluding the Pressure Change

Since the speed of air decreases in a diffuser, the pressure increases according to Bernoulli’s principle.

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Key Concepts

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

Bernoulli's principle
Bernoulli's principle is a fundamental concept in fluid dynamics. It explains the behavior of fluid flow and is especially useful in understanding how pressure and velocity are related in a fluid system.
Bernoulli's principle states that within a steady flow of an incompressible fluid, an increase in the fluid's velocity leads to a decrease in pressure and vice versa. Mathematically, it is represented as:
\[ P + \frac{1}{2} \rho v^2 + \rho gh = \text{constant} \]
Here, P represents the fluid pressure, \( \rho \) is the fluid density, v is the fluid velocity, g is the acceleration due to gravity, and h is the height above a reference point.
This principle is critical in various applications, including explaining how airfoils generate lift and predicting fluid behavior in piping systems. In the case of a diffuser, the principle helps us understand that as the airflow slows down, its pressure increases.
Fluid Dynamics
Fluid dynamics is the study of fluids (liquids and gases) in motion. It encompasses a wide range of phenomena, from the simple flow of water in a pipe to complex behaviors like weather patterns and blood circulation in the human body.
Key concepts in fluid dynamics include:
  • Continuity equation: Establishes that the mass of fluid remains constant as it flows. It asserts that the product of cross-sectional area and fluid velocity at any point along the flow is constant for incompressible fluids, represented as \( A_1 v_1 = A_2 v_2 \).
  • Viscosity: Describes a fluid's resistance to flow. Fluids with higher viscosity (like honey) flow slower than those with lower viscosity (like water).
  • Laminar vs. turbulent flow: Laminar flow is smooth and orderly, while turbulent flow is chaotic and characterized by vortices and eddies.
Understanding these concepts allows engineers and scientists to design efficient systems for transporting fluids and predicting the behavior of natural fluid systems.
Pressure-Velocity Relationship
The pressure-velocity relationship in fluid dynamics is pivotal to understanding how fluids interact with various environments and devices. As highlighted by Bernoulli’s principle, there is an inverse relationship between pressure and velocity within a flowing fluid.
When the velocity of a fluid decreases, its pressure increases, and vice versa. This relationship is crucial in the function of numerous devices:
  • Diffusers: These devices slow down the flow of a fluid, thereby increasing its pressure. They are often used in HVAC systems and jet engines to control airflow.
  • Nozzles: In contrast to diffusers, nozzles accelerate fluid flow, decreasing its pressure. They find applications in rocket engines and garden hoses.
  • Venturi meters: These meters utilize the pressure-velocity relationship to measure flow rates by observing changes in pressure within a narrowed section of pipe.
Through this relationship, engineers can design systems to optimize fluid flow for various applications, from industrial processes to everyday appliances.
In summary, understanding how pressure and velocity interact within a fluid system allows for the effective control and utilization of fluids in a wide array of settings.

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Most popular questions from this chapter

The inlet ducting to a jet engine forms a diffuser that steadily decelerates the entering air to zero velocity relative to the engine before the air enters the compressor. Consider a jet airplane flying at \(1000 \mathrm{~km} / \mathrm{h}\) where the local atmospheric pressure is \(0.6\) bar and the air temperature is \(8^{\circ} \mathrm{C}\). Assuming ideal gas behavior and neglecting heat transfer and potential energy effects, determine the temperature, in \({ }^{\circ} \mathrm{C}\), of the air entering the compressor.

Nitrogen gas enters a turbine operating at steady state with a velocity of \(60 \mathrm{~m} / \mathrm{s}\), a pressure of \(0.345 \mathrm{Mpa}\), and a temperature of \(700 \mathrm{~K}\). At the exit, the velocity is \(0.6 \mathrm{~m} / \mathrm{s}\), the pressure is \(0.14 \mathrm{Mpa}\), and the temperature is \(390 \mathrm{~K}\). Heat transfer from the surface of the turbine to the surroundings occurs at a rate of \(36 \mathrm{~kJ}\) per \(\mathrm{kg}\) of nitrogen flowing. Neglecting potential energy effects and using the ideal gas model, determine the power developed by the turbine, in \(\mathrm{kW}\).

What practical measures can be taken by manufacturers to use energy resources more efficiently? List several specific opportunities, and discuss their potential impact on profitability and productivity.

Prepare a memorandum providing guidelines for selecting fans for cooling electronic components. Consider the advantages and disadvantages of locating the fan at the inlet of the enclosure containing the electronics. Repeat for a fan at the enclosure exit. Consider the relative merits of alternative fan types and of fixed- versus variable-speed fans. Explain how characteristic curves assist in fan selection.

The intake to a hydraulic turbine installed in a flood control dam is located at an elevation of \(10 \mathrm{~m}\) above the turbine exit. Water enters at \(20^{\circ} \mathrm{C}\) with negligible velocity and exits from the turbine at \(10 \mathrm{~m} / \mathrm{s}\). The water passes through the turbine with no significant changes in temperature or pressure between the inlet and exit, and heat transfer is negligible. The acceleration of gravity is constant at \(g=9.81 \mathrm{~m} / \mathrm{s}^{2}\). If the power output at steady state is \(500 \mathrm{~kW}\), what is the mass flow rate of water, in \(\mathrm{kg} / \mathrm{s}\) ?

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