Krylov subspace: Difference between revisions

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In [[fluid dynamics]], the '''enstrophy''' <math>\mathcal{E}</math> can be described as the integral of the square of the [[vorticity]] <math>\eta</math> given a velocity field <math>\mathbf{u}</math> as,
 
:<math> \mathcal{E}(\mathbf{u}) =\frac{1}{2} \int_{S} \eta^{2}dS. </math>
 
Here, since the curl gives a [[scalar field]] in 2-dimensions ([[vortex]]) corresponding to the vector-valued [[velocity]] solving in the incompressible [[Navier–Stokes equations]], we can integrate its square over a surface S to retrieve a [[continuous linear operator]] on the space of possible velocity fields, known as a ''current''. This equation is however somewhat misleading.  Here we have chosen a simplified version of the enstrophy derived from the [[Incompressible fluid|incompressibility condition]], which is equivalent to vanishing divergence of the velocity field,
 
:<math> \nabla \cdot \mathbf{u} = 0. </math>
 
More generally, when not restricted to the incompressible condition, or to two spatial dimensions, the enstrophy may be computed by:
 
:<math> \mathcal{E}(\mathbf{u}) = \int_{S} |\nabla (\mathbf{u})|^{2}dS. </math>
 
where
 
:<math> |\nabla (\mathbf{u})| </math>
 
is the [[Frobenius norm]] of the gradient of the velocity field <math>\mathbf{u}</math>.
 
The enstrophy can be interpreted as another type of [[potential density]] (''ie''. see [[probability density function|probability density]]); or, more concretely, the quantity directly related to the [[kinetic energy]] in the flow model that corresponds to [[dissipation]] effects in the fluid. It is particularly useful in the study of [[turbulence|turbulent flows]], and is often identified in the study of [[Electrostatic ion thruster|thruster]]s as well as the field of [[flame theory]].<ref>[http://courseware.mech.ntua.gr/ml22058/pdfs/combustion-flame.pdf Overview of Flame Theory] (class notes, National Technical University of Athens, Greece)</ref>
 
== External links ==
* [http://aanda.u-strasbg.fr:2002/articles/aa/full/2004/45/aa0573-04/aa0573-04.right.html Hydrodynamic stability of rotationally supported flows]
* [http://www2.appmath.com:8080/site/frisch/frisch.html The dynamics of enstrophy transfer in two dimensional hydrodynamics]
 
== References ==
 
{{reflist}}
 
[[Category:Fluid dynamics]]
[[Category:Spacecraft propulsion]]
 
 
{{fluiddynamics-stub}}

Revision as of 06:08, 23 November 2013

In fluid dynamics, the enstrophy can be described as the integral of the square of the vorticity η given a velocity field u as,

(u)=12Sη2dS.

Here, since the curl gives a scalar field in 2-dimensions (vortex) corresponding to the vector-valued velocity solving in the incompressible Navier–Stokes equations, we can integrate its square over a surface S to retrieve a continuous linear operator on the space of possible velocity fields, known as a current. This equation is however somewhat misleading. Here we have chosen a simplified version of the enstrophy derived from the incompressibility condition, which is equivalent to vanishing divergence of the velocity field,

u=0.

More generally, when not restricted to the incompressible condition, or to two spatial dimensions, the enstrophy may be computed by:

(u)=S|(u)|2dS.

where

|(u)|

is the Frobenius norm of the gradient of the velocity field u.

The enstrophy can be interpreted as another type of potential density (ie. see probability density); or, more concretely, the quantity directly related to the kinetic energy in the flow model that corresponds to dissipation effects in the fluid. It is particularly useful in the study of turbulent flows, and is often identified in the study of thrusters as well as the field of flame theory.[1]

External links

References

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Template:Fluiddynamics-stub

  1. Overview of Flame Theory (class notes, National Technical University of Athens, Greece)