Vortex created by the passage of an aircraft wing, revealed by colored smoke.
Milk vortices in a cup of coffee

In fluid dynamics, a vortex is a region in a fluid medium in which the flow is mostly rotating around an axis line, the vortical flow that occurs either on a straight-axis or a curved-axis.[1][2] The plural of vortex is either vortices or vortexes.[3][4] Vortices form in stirred fluids, such as liquid, gas, and plasma. Examples include:

Vortices are a major component of irrotational vortices, possibly superimposed to larger-scale flows, including larger-scale vortices. In each vortex, the fluid's flow velocity is greatest next to its axis, and decreases in inverse proportion to the distance from the axis. The vorticity (the curl of the flow velocity) is very high in the core region surrounding the axis, and nearly absent in the greater vortex; pressure within the vortex decreases as the proximity from the axis increases.

Once formed, vortices can move, stretch, twist, and interact in complex ways. A moving vortex carries with it some angular and linear momentum, energy, and mass. In a stationary vortex, the streamlines and pathlines are closed. In a moving or evolving vortex the streamlines and pathlines are stretched by the overall flow into loopy yet open curves.


  • Properties 1
    • Vorticity 1.1
    • Vortex types 1.2
      • Irrotational vortices 1.2.1
      • Rotational vortices 1.2.2
    • Vortex geometry 1.3
    • Pressure in a vortex 1.4
    • Evolution 1.5
  • Two-dimensional modeling 2
  • Further examples 3
  • See also 4
  • References 5
    • Notes 5.1
    • Other 5.2
  • External links 6



The Crow Instability of a jet aeroplane's contrail visually demonstrates the vortex created in the atmosphere (gas fluid medium) by the passage of the aircraft.

A key concept in the dynamics of vortices is the vorticity, a vector that describes the local rotary motion at a point in the fluid, as would be perceived by an observer that moves along with it. Conceptually, the vorticity could be observed by placing a tiny rough ball at the point in question, free to move with the fluid, and observing how it rotates about its center. The direction of the vorticity vector is defined to be the direction of the axis of rotation of this imaginary ball (according to the right-hand rule) while its length is twice the ball's angular velocity. Mathematically, the vorticity is defined as the curl (or rotational) of the velocity field of the fluid, usually denoted by \vec \omega and expressed by the vector analysis formula \nabla \times \vec{\mathit{u}}, where \nabla is the nabla operator and \vec{\mathit{u}} is the local flow velocity.[5]

The local rotation measured by the vorticity \vec \omega must not be confused with the angular velocity vector of that portion of the fluid with respect to the external environment or to any fixed axis. In a vortex, in particular, \vec \omega may be opposite to the mean angular velocity vector of the fluid relative to the vortex's axis.

Vortex types

In theory, the speed u of the particles (and, therefore, the vorticity) in a vortex may vary with the distance r from the axis in many ways. There are two important special cases, however:

A rigid-body vortex
  • If the fluid rotates like a rigid body – that is, if the angular rotational velocity Ω is uniform, so that u increases proportionally to the distance r from the axis – a tiny ball carried by the flow would also rotate about its center as if it were part of that rigid body. In such a flow, the vorticity is the same everywhere: its direction is parallel to the rotation axis, and its magnitude is equal to twice the uniform angular velocity Ω of the fluid around the center of rotation.
    \vec{\Omega} = (0, 0, \Omega) , \quad \vec{r} = (x, y, 0) ,
    \vec{u} = \vec{\Omega} \times \vec{r} = (-\Omega y, \Omega x, 0) ,
    \vec \omega = \nabla \times \vec{u} = (0, 0, 2\Omega) = 2\vec{\Omega} .
An irrotational vortex
  • If the particle speed u is inversely proportional to the distance r from the axis, then the imaginary test ball would not rotate over itself; it would maintain the same orientation while moving in a circle around the vortex axis. In this case the vorticity \vec \omega is zero at any point not on that axis, and the flow is said to be irrotational.
    \vec{\Omega} = (0, 0, \alpha r^{-2}) , \quad \vec{r} = (x, y, 0) ,
    \vec{u} = \vec{\Omega} \times \vec{r} = (-\alpha y r^{-2}, \alpha x r^{-2}, 0) ,
    \vec{\omega} = \nabla \times \vec{u} = 0 .

Irrotational vortices

Pathlines of fluid particles around the axis (dashed line) of an ideal irrotational vortex. (See )

In the absence of external forces, a vortex usually evolves fairly quickly toward the irrotational flow pattern, where the flow velocity u is inversely proportional to the distance r. For that reason, irrotational vortices are also called free vortices.

For an irrotational vortex, the circulation is zero along any closed contour that does not enclose the vortex axis and has a fixed value, \Gamma, for any contour that does enclose the axis once.[6] The tangential component of the particle velocity is then u_{\theta} = \Gamma/(2 \pi r). The angular momentum per unit mass relative to the vortex axis is therefore constant, r u_{\theta} = \Gamma/(2 \pi).

However, the ideal irrotational vortex flow is not physically realizable, since it would imply that the particle speed (and hence the force needed to keep particles in their circular paths) would grow without bound as one approaches the vortex axis. Indeed, in real vortices there is always a core region surrounding the axis where the particle velocity stops increasing and then decreases to zero as r goes to zero. Within that region, the flow is no longer irrotational: the vorticity \vec \omega becomes non-zero, with direction roughly parallel to the vortex axis. The Rankine vortex is a model that assumes a rigid-body rotational flow where r is less than a fixed distance r0, and irrotational flow outside that core regions. The Lamb-Oseen vortex model is an exact solution of the Navier–Stokes equations governing fluid flows and assumes cylindrical symmetry, for which

u_{\theta} = (1 - e^{-r^2/(4\nu t)})\Gamma/(2 \pi r).

In an irrotational vortex, fluid moves at different speed in adjacent streamlines, so there is friction and therefore energy loss throughout the vortex, especially near the core.

Rotational vortices

The cloud vortex Saturn's hexagon is at the north pole of the planet Saturn.

A rotational vortex – one which has non-zero vorticity away from the core – can be maintained indefinitely in that state only through the application of some extra force, that is not generated by the fluid motion itself.

For example, if a water bucket is spun at constant angular speed w about its vertical axis, the water will eventually rotate in rigid-body fashion. The particles will then move along circles, with velocity u equal to wr.[6] In that case, the free surface of the water will assume a parabolic shape.

In this situation, the rigid rotating enclosure provides an extra force, namely an extra pressure gradient in the water, directed inwards, that prevents evolution of the rigid-body flow to the irrotational state.

Vortex geometry

In a stationary vortex, the typical streamline (a line that is everywhere tangent to the flow velocity vector) is a closed loop surrounding the axis; and each vortex line (a line that is everywhere tangent to the vorticity vector) is roughly parallel to the axis. A surface that is everywhere tangent to both flow velocity and vorticity is called a vortex tube. In general, vortex tubes are nested around the axis of rotation. The axis itself is one of the vortex lines, a limiting case of a vortex tube with zero diameter.

According to Helmholtz's theorems, a vortex line cannot start or end in the fluid – except momentarily, in non-steady flow, while the vortex is forming or dissipating. In general, vortex lines (in particular, the axis line) are either closed loops or end at the boundary of the fluid. A whirlpool is an example of the latter, namely a vortex in a body of water whose axis ends at the free surface. A vortex tube whose vortex lines are all closed will be a closed torus-like surface.

A newly created vortex will promptly extend and bend so as to eliminate any open-ended vortex lines. For example, when an airplane engine is started, a vortex usually forms ahead of each propeller, or the turbofan of each jet engine. One end of the vortex line is attached to the engine, while the other end usually stretches outs and bends until it reaches the ground.

When vortices are made visible by smoke or ink trails, they may seem to have spiral pathlines or streamlines. However, this appearance is often an illusion and the fluid particles are moving in closed paths. The spiral streaks that are taken to be streamlines are in fact clouds of the marker fluid that originally spanned several vortex tubes and were stretched into spiral shapes by the non-uniform flow velocity distribution.

Pressure in a vortex

A Plughole vortex

The fluid motion in a vortex creates a dynamic pressure (in addition to any hydrostatic pressure) that is lowest in the core region, closest to the axis, and increases as one moves away from it, in accordance with Bernoulli's Principle. One can say that it is the gradient of this pressure that forces the fluid to follow a curved path around the axis.

In a rigid-body vortex flow of a fluid with constant density, the dynamic pressure is proportional to the square of the distance r from the axis. In a constant gravity field, the free surface of the liquid, if present, is a concave paraboloid.

In an irrotational vortex flow with constant fluid density and cylindrical symmetry, the dynamic pressure varies as PK/r2, where P is the limiting pressure infinitely far from the axis. This formula provides another constraint for the extent of the core, since the pressure cannot be negative. The free surface (if present) dips sharply near the axis line, with depth inversely proportional to r2.

The core of a vortex in air is sometimes visible because of a plume of water vapor caused by condensation in the low pressure and low temperature of the core; the spout of a tornado is an example. When a vortex line ends at a boundary surface, the reduced pressure may also draw matter from that surface into the core. For example, a dust devil is a column of dust picked up by the core of an air vortex attached to the ground. A vortex that ends at the free surface of a body of water (like the whirlpool that often forms over a bathtub drain) may draw a column of air down the core. The forward vortex extending from a jet engine of a parked airplane can suck water and small stones into the core and then into the engine.


Vortices need not be steady-state features; they can move and change shape. In a moving vortex, the particle paths are not closed, but are open, loopy curves like helices and cycloids. A vortex flow might also be combined with a radial or axial flow pattern. In that case the streamlines and pathlines are not closed curves but spirals or helices, respectively. This is the case in tornadoes and in drain whirlpools. A vortex with helical streamlines is said to be solenoidal.

As long as the effects of viscosity and diffusion are negligible, the fluid in a moving vortex is carried along with it. In particular, the fluid in the core (and matter trapped by it) tends to remain in the core as the vortex moves about. This is a consequence of Helmholtz's second theorem. Thus vortices (unlike surface and pressure waves) can transport mass, energy and momentum over considerable distances compared to their size, with surprisingly little dispersion. This effect is demonstrated by smoke rings and exploited in vortex ring toys and guns.

Two or more vortices that are approximately parallel and circulating in the same direction will attract and eventually merge to form a single vortex, whose circulation will equal the sum of the circulations of the constituent vortices. For example, an airplane wing that is developing lift will create a sheet of small vortices at its trailing edge. These small vortices merge to form a single wingtip vortex, less than one wing chord downstream of that edge. This phenomenon also occurs with other active airfoils, such as propeller blades. On the other hand, two parallel vortices with opposite circulations (such as the two wingtip vortices of an airplane) tend to remain separate.

Vortices contain substantial energy in the circular motion of the fluid. In an ideal fluid this energy can never be dissipated and the vortex would persist forever. However, real fluids exhibit viscosity and this dissipates energy very slowly from the core of the vortex. It is only through dissipation of a vortex due to viscosity that a vortex line can end in the fluid, rather than at the boundary of the fluid.

Two-dimensional modeling

When the particle velocities are constrained to be parallel to a fixed plane, one can ignore the space dimension perpendicular to that plane, and model the flow as a two-dimensional flow velocity field on that plane. Then the vorticity vector \vec \omega is always perpendicular to that plane, and can be treated as a scalar. This assumption is sometimes made in meteorology, when studying large-scale phenomena like hurricanes.

The behavior of vortices in such contexts is qualitatively different in many ways; for example, it does not allow the stretching of vortices that is often seen in three dimensions.

Further examples

A visible vortex formed when a C-17 uses high engine power at slow speed on a wet runway.

See also



  1. ^ Ting, L. (1991). Viscous Vortical Flows. Lecture notes in physics. Springer-Verlag.  
  2. ^ Kida, Shigeo (2001). Life, Structure, and Dynamical Role of Vortical Motion in Turbulence (PDF). IUTAMim Symposium on Tubes, Sheets and Singularities in Fluid Dynamics. Zakopane, Poland. 
  3. ^ "vortex". Oxford Dictionaries Online (ODO). Oxford University Press. Retrieved 2015-08-29. 
  4. ^ "vortex". Merriam-Webster Online. Merriam-Webster, Inc. Retrieved 2015-08-29. 
  5. ^ Vallis, Geoffrey (1999). Geostrophic Turbulence: The Macroturbulence of the Atmosphere and Ocean Lecture Notes (PDF). Lecture notes.  
  6. ^ a b Clancy 1975, sub-section 7.5


  • Loper, David E. (November 1966). An analysis of confined magnetohydrodynamic vortex flows (PDF) (NASA contractor report NASA CR-646). Washington: National Aeronautics and Space Administration.  
  • Falkovich, G. (2011). Fluid Mechanics, a short course for physicists. Cambridge University Press.  
  • Clancy, L.J. (1975). Aerodynamics. London: Pitman Publishing Limited.  
  • De La Fuente Marcos, C.; Barge, P. (2001). "The effect of long-lived vortical circulation on the dynamics of dust particles in the mid-plane of a protoplanetary disc". Monthly Notices of the Royal Astronomical Society 323 (3): 601–614.  

External links

  • Optical Vortices
  • Video of two water vortex rings colliding (MPEG)
  • Chapter 3 Rotational Flows: Circulation and Turbulence
  • Vortical Flow Research Lab (MIT) – Study of flows found in nature and part of the Department of Ocean Engineering.