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Define incompressible flow and incompressible fluid. Must the flow of a compressible fluid necessarily be treated as compressible?

Short Answer

Expert verified
Answer: No, the flow of a compressible fluid is not always treated as compressible. In certain conditions where the density changes are small enough, the compressible fluid flow can be approximated as an incompressible flow for analysis purposes.

Step by step solution

01

Define Incompressible Fluid

An incompressible fluid is a fluid with a constant density, meaning its volume does not change when subjected to pressure variations. This is an idealization since all real fluids are compressible to some extent.
02

Define Incompressible Flow

Incompressible flow refers to fluid flow where the density of the fluid remains constant throughout the flow field. In such a flow, the fluid properties like density, pressure, and temperature can change, but the volume of the fluid elements remains unchanged.
03

Relationship between Compressible Fluid and Compressible Flow

A compressible fluid is a fluid whose density can change significantly as a result of pressure or temperature variations. The flow of a compressible fluid is considered compressible flow when the density variations are significant and cannot be neglected during analysis.
04

Must a Compressible Fluid Flow Necessarily be Treated as Compressible

No, the flow of a compressible fluid does not necessarily need to be treated as compressible in all situations. There are certain conditions in which the density changes are small enough that they can be neglected for analysis purposes. In such cases, a compressible fluid flow can be approximated as an incompressible flow.

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Key Concepts

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

Incompressible Fluid
In the world of fluid mechanics, understanding the characteristics of different types of fluids is crucial. An incompressible fluid is one whose density does not change significantly when pressure is applied. This is a fundamental concept because it simplifies many fluid dynamics problems. When dealing with incompressible fluids, you can assume that the mass of fluid traveling through a pipe in a given amount of time remains constant, no matter the pressure changes.

This idealization is key in studying fluid behavior in situations like water flow through pipes or the airflow over an aircraft wing at lower speeds. While in reality, all fluids are slightly compressible, for many fluids like water or slow-moving air, the density changes are so minimal that they can be considered incompressible for practical calculations.
Compressible Fluid
Contrastingly, a compressible fluid displays significant changes in density when subjected to different pressures or temperatures. This characteristic is particularly critical when analyzing high-speed flows, such as the sound-speed airflow around a jet. In these scenarios, the density of the fluid can vary greatly throughout the flow field, impacting the aerodynamic forces involved.

Understanding when to consider a fluid's compressibility is essential for accurate predictions in aerodynamics and other high-speed applications. It affects how shock waves form and propagate, how energy is transferred, and even the fluid's temperature. As such, engineers and scientists expend considerable effort to include these intricacies in their models for precise analyses.
Fluid Mechanics
At the heart of these discussions is fluid mechanics, the branch of physics concerned with the behavior of fluids at rest and in motion. It encompasses the study of various properties such as velocity, pressure, density, and temperature, and how they influence the fluid flow. Fluid mechanics is split into two primary branches: fluid statics, dealing with fluids at rest, and fluid dynamics, addressing fluids in motion.

Fluid mechanics is the foundation for disciplines ranging from hydrology to aeronautical engineering. Whether designing irrigation systems, predicting weather patterns, or constructing high-speed aircraft, the principles of fluid mechanics serve as a guide for understanding and manipulating fluid behavior.
Density Variations in Fluids
Understanding density variations in fluids is important for accurately characterizing fluid behavior under different conditions. Density, the mass per unit volume, can vary in fluid due to changes in temperature, pressure, or composition. In incompressible fluids, these variations are deemed negligible, yet in compressible fluids, they are significant enough to affect flow characteristics.

Density variations can lead to interesting phenomena like buoyancy, thermal expansion, and variable acoustic speed. In engineering, considering these variations is crucial for designing systems that can handle the corresponding changes in flow properties, such as the expansion of gases in a turbine or the buoyancy of ships. Having a deep understanding of density variations also aids in predicting the behavior of fluids in natural processes, like ocean currents and atmospheric circulation.

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Most popular questions from this chapter

Air at \(5^{\circ} \mathrm{C}\), with a convection heat transfer coefficient of \(30 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), is used for cooling metal plates coming out of a heat treatment oven at an initial temperature of \(300^{\circ} \mathrm{C}\). The plates \((k=180 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), \(\rho=2800 \mathrm{~kg} / \mathrm{m}^{3}\), and \(c_{p}=880 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\) ) have a thickness of \(10 \mathrm{~mm}\). Using EES (or other) software, determine the effect of cooling time on the temperature gradient in the metal plates at the surface. By varying the cooling time from 0 to \(3000 \mathrm{~s}\), plot the temperature gradient in the plates at the surface as a function of cooling time. Hint: Use the lumped system analysis to calculate the plate surface temperature. Make sure to verify the application of this method to this problem.

The convection heat transfer coefficient for a clothed person standing in moving air is expressed as \(h=14.8 \mathrm{~V}^{0.69}\) for \(0.15

What fluid property is responsible for the development of the velocity boundary layer? For what kind of fluids will there be no velocity boundary layer on a flat plate?

Consider an airplane cruising at an altitude of \(10 \mathrm{~km}\) where standard atmospheric conditions are \(-50^{\circ} \mathrm{C}\) and \(26.5 \mathrm{kPa}\) at a speed of \(800 \mathrm{~km} / \mathrm{h}\). Each wing of the airplane can be modeled as a \(25-\mathrm{m} \times 3-\mathrm{m}\) flat plate, and the friction coefficient of the wings is \(0.0016\). Using the momentum-heat transfer analogy, determine the heat transfer coefficient for the wings at cruising conditions. Answer: \(89.6 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\)

Mercury at \(0^{\circ} \mathrm{C}\) is flowing over a flat plate at a velocity of \(0.1 \mathrm{~m} / \mathrm{s}\). Using EES (or other) software, determine the effect of the location along the plate \((x)\) on the velocity and thermal boundary layer thicknesses. By varying \(x\) for \(0

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