In fluid dynamics, circulation is the line integral around a closed curve of the fluid velocity. Circulation is normally denoted <math>\Gamma</math>. If <math>\mathbf{V}</math> is the fluid velocity and <math>\mathbf{ds}</math> is a unit vector along the closed curve <math>C</math>:
- <math>\Gamma=\oint_{C}\mathbf{V}\cdot\mathbf{ds}</math>
The dimensions of circulation are length squared over time. Circulation was first used independently by Frederick Lanchester, Wilhelm Kutta, and Nikolai Zhukovsky.
Kutta-Joukowski Theorem
The lift force acting per unit span on a body in an inviscid flow field can be expressed as the product of the circulation (<math> \Gamma </math>) about the body, the fluid density (<math> \rho </math> ), and the speed of the body relative to the free-stream (<math> V </math>). Thus,
- <math>l = \rho V \Gamma </math>
This is known as the Kutta-Joukowski theorem. This equation applies both around airfoils, where the circulation is generated by airfoil action, and around spinning objects, experiencing the Magnus effect, where the circulation is induced mechanically. Circulation is often used in computational fluid dynamics as an intermediate variable to calculate forces on an airfoil or other body. The circulation around an airfoil can be finite, but the vorticity of the fluid outside of the airfoil can be zero.
Relation to vorticity
Circulation can be related to vorticity by Stokes' theorem:
- <math>\Gamma=\oint_{C}\mathbf{V}\cdot\mathbf{ds}=\int\!\!\!\int_S(\nabla\times\mathbf{V})\cdot\mathbf{dS}</math>
but only if the integration path is a boundary, not just a closed cycle. Thus vorticity is the circulation per unit area, taken around an infinitesimal loop.
