Article · Wikipedia archive · Last revised May 27, 2026

Velocity potential

Within the applied mathematical study of fluid dynamics and continuum mechanics, a velocity potential is a scalar potential used in potential flow theory. It was introduced by Joseph-Louis Lagrange in 1788.

Last revised
May 27, 2026
Read time
≈ 2 min
Length
448 w
Citations
2
Source

Within the applied mathematical study of fluid dynamics and continuum mechanics, a velocity potential is a scalar potential used in potential flow theory. It was introduced by Joseph-Louis Lagrange in 1788.1

Suppose a smooth vector field u {\displaystyle \mathbf {u} } in a simple connected region represents the flow velocity of a fluid at each point. This flow field is said to be irrotational when × u = 0 . {\displaystyle \nabla \times \mathbf {u} =0\,.} If the flow field is irrotational, then it can be also be represented as the gradient of a scalar function ϕ {\displaystyle \phi } : u = ϕ   = ϕ x i + ϕ y j + ϕ z k . {\displaystyle \mathbf {u} =\nabla \phi \ ={\frac {\partial \phi }{\partial x}}\mathbf {i} +{\frac {\partial \phi }{\partial y}}\mathbf {j} +{\frac {\partial \phi }{\partial z}}\mathbf {k} \,.}

ϕ {\displaystyle \phi } is known as a velocity potential for u. Velocity potentials are unique up to a constant and a function solely of the temporal variable. So if ϕ ( x , y , z ) {\displaystyle \phi (x,y,z)} is a velocity potential, then ϕ ( x , y , z ) + f ( t ) + C {\displaystyle \phi (x,y,z)+f(t)+C} generates the same flow field as ϕ ( x , y , z ) {\displaystyle \phi (x,y,z)} .

The Laplacian of a velocity potential is equal to the divergence of the corresponding flow. Hence if a velocity potential satisfies Laplace equation, the flow is incompressible.

Unlike a stream function, a velocity potential can exist in three-dimensional flow.

Usage in acoustics

In theoretical acoustics,2 it is often desirable to work with the acoustic wave equation of the velocity potential ϕ {\displaystyle \phi } instead of pressure p and/or particle velocity u. 2 ϕ 1 c 2 2 ϕ t 2 = 0 {\displaystyle \nabla ^{2}\phi -{\frac {1}{c^{2}}}{\frac {\partial ^{2}\phi }{\partial t^{2}}}=0} Solving the wave equation for either p field or u field does not necessarily provide a simple answer for the other field. On the other hand, when ϕ {\displaystyle \phi } is solved for, not only is u found as given above, but p is also easily found—from the (linearised) Bernoulli equation for irrotational and unsteady flow—as p = ρ ϕ t . {\displaystyle p=-\rho {\frac {\partial \phi }{\partial t}}\,.}

See also

See also

Notes

Notes

  1. Anderson, John (1998). A History of Aerodynamics. Cambridge University Press. ISBN 978-0521669559.
  2. Pierce, A. D. (1994). Acoustics: An Introduction to Its Physical Principles and Applications. Acoustical Society of America. ISBN 978-0883186121.