Fluid dynamics (also called fluid mechanics) is the study of fluids ,that is liquids and gases . The solution of a fluiddynamic problem normally involves calculating for various properties of the fluid, such as velocity , pressure , density , and temperature , as functions of space and time.
Applications of fluid dynamics
Fluid dynamics and its subdisciplines aerodynamics , hydrostatics , hydrodynamics , and hydraulics have a wide range ofapplications. For example, they are used in calculating forces and moments on aircraft , themass flow of petroleum through pipelines, and prediction of weather patterns.
The concept of a fluid is surprisingly general. For example, some of the basic mathematical concepts in traffic engineering are derived from consideringtraffic as a continuous fluid.
The continuity assumption
Gases are composed of molecules which collide with one another and solidobjects. The continuity assumption, however, considers fluids to be continuous .That is, properties such as density, pressure, temperature, and velocity are taken to be well-defined at infinitely small points,and are assumed to vary continuously from one point to another. The discrete, molecular nature of a fluid is ignored.
Those problems for which the continuity assumption does not give answers of desired accuracy are solved using statistical mechanics . In order to determine whether to useconventional fluid dynamics (a subdiscipline of continuummechanics ) or statistical mechanics, the Knudsen number isevaluated for the problem. Problems with Knudsen numbers at or above unity must be evaluated using statistical mechanics forreliable solutions.
Equations of fluid dynamics
The foundational axioms of fluid dynamics are the conservationlaws , specifically, conservation of mass , conservationof momentum (also known as Newton's second law orthe balance law), and conservation of energy . These arebased on classical mechanics and are modified in relativisticmechanics .
The central equations for fluid dynamics are the Navier-Stokes equations , which are non-linear differential equations that describe the flow of afluid whose stress depends linearly on velocity and on pressure. The unsimplified equations do not have a general closed-formsolution, so they are only of use in computational fluid dynamics . The equations can be simplified in a number of ways. All of thesimplifications make the equations easier to solve. Some of them allow appropriate fluid dynamics problems to be solved in closedform.
Compressible vs incompressible flow
A fluid problem is called compressible if changes in thedensity of the fluid have significant effects on the solution. If the density changes have negligible effects on the solution,the fluid is called incompressible and the changes in densityare ignored.
In order to determine whether to use compressible or incompressible fluid dynamics, the Mach number of the problem is evaluated. As a rough guide, compressible effects can be ignored at Mach numbersbelow approximately 0.3. Nearly all problems involving liquids are in this regime and modeled as incompressible.
The incompressible Navier-Stokes equations are simplifications of the Navier-Stokes equations in which the density has beenassumed to be constant. These can be used to solve incompressible problems.
Viscous vs inviscid flow
Viscous problems are those in which fluid friction have significant effects on thesolution. Problems for which friction can safely be neglected are called inviscid.
The Reynolds number can be used to evaluate whether viscous or inviscid equations are appropriateto the problem. High Reynolds numbers indicate that the inertial forces are more significant than the viscous forces. However,even in high Reynolds number regimes certain problems require that viscosity be included. In particular, problems calculating netforces on bodies (such as wings) should use viscous equations. As illustrated by d'Alembert's paradox , a body in an inviscid fluid will experience no force.
The standard equations of inviscid flow are the Euler equations .Another often used model, especially in computational fluid dynamics, is to use the Euler equations far from the body and the boundarylayer equations close to the body.
The Euler equations can be integrated along a streamline to get Bernoulli's equation . When the flow is everywhereirrotational as well as inviscid, Bernoulli's equation can be used to solve the problem.
Steady vs unsteady flow
Another simplification of fluid dynamics equations is to set all changes of fluid properties with time to zero. This is calledsteady flow, and is applicable to a large class of problems, such as lift and drag on a wing or flow through a pipe. Both theNavier-Stokes equations and the Euler equations become simpler when their steady forms are used.
If a problem is incompressible, irrotational, inviscid, and steady, it can be solved using potential flow , governed by Laplace'sequation . Problems in this class have elegant solutions which are linear combinations of well-studied elementary flows.
Laminar vs turbulent flow
It is believed that turbulent flows obey the Navier-Stokes equations. However, the flow is so complex that it is not possibleto solve turbulent problems from first principles with the computational tools available today or likely to be available in thenear future. Turbulence is instead modeled using one of a number of turbulence models and coupledwith a flow solver that assumes laminar flow outside a turbulent region.
There are a large number of other possible approximations to fluid dynamic problems. Stokes flow is flow at very low Reynold'snumbers, such that inertial forces can be neglected compared to viscous forces. The Boussinesq approximation neglects compressibility except to calculate buoyancy forces.
Fields of study
Mathematical equations and objects
Types of fluid flow
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