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Vorticity

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:<math>
:<math>
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\omega := \textrm{curl}(u) = \nabla \times u
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\omega \equiv \textrm{curl}(u) \equiv  \nabla \times u
</math>
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In tensor notation, vorticity is given by
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In tensor notation, vorticity is given by:
:<math>
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</math>
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where <math>\epsilon_{ijk}</math> is the [[alternating tensor]]. The components of vorticity in Cartesian coordinates are
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where <math>\epsilon_{ijk}</math> is the [[alternating tensor]]. The components of vorticity in Cartesian coordinates are;:
:<math>
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== Physical Significance ==
== Physical Significance ==
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The vorticity can be seen as a vector having magnitude equal to the maximum "circulation" at each point and to be oriented perpendicularly to this plane of circulation for each point.
== Related Pages ==
== Related Pages ==
*[[Vorticity transport equation]]
*[[Vorticity transport equation]]

Latest revision as of 10:07, 14 June 2007

Vorticity is a vector field variable which is derived from the velocity vector. Mathematically, it is defined as the curl of the velocity vector


\omega \equiv \textrm{curl}(u) \equiv  \nabla \times u

In tensor notation, vorticity is given by:


\omega_i = \epsilon_{ijk} \frac{\partial u_k}{\partial x_j}

where \epsilon_{ijk} is the alternating tensor. The components of vorticity in Cartesian coordinates are;:


\omega_1 = \frac{\partial u_3}{\partial x_2} - \frac{\partial u_2}{\partial x_3}

\omega_2 = \frac{\partial u_1}{\partial x_3} - \frac{\partial u_3}{\partial x_1}

\omega_3 = \frac{\partial u_2}{\partial x_1} - \frac{\partial u_1}{\partial x_2}

This can be obtained by using determinants


\omega =
\begin{vmatrix}
\hat{e}_1 & \hat{e}_2 & \hat{e}_3 \\
\frac{\partial}{\partial x_1} & \frac{\partial}{\partial x_2} & \frac{\partial}{\partial x_3} \\
u_1 & u_2 & u_3
\end{vmatrix}

where \hat{e}_1, \hat{e}_2, \hat{e}_3 are the unit vectors for the Cartesian coordinate system.

Physical Significance

The vorticity can be seen as a vector having magnitude equal to the maximum "circulation" at each point and to be oriented perpendicularly to this plane of circulation for each point.

Related Pages

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