Misplaced Pages

Velocity potential

Article snapshot taken from Wikipedia with creative commons attribution-sharealike license. Give it a read and then ask your questions in the chat. We can research this topic together.
This article needs additional citations for verification. Please help improve this article by adding citations to reliable sources. Unsourced material may be challenged and removed.
Find sources: "Velocity potential" – news · newspapers · books · scholar · JSTOR (May 2014) (Learn how and when to remove this message)

A velocity potential is a scalar potential used in potential flow theory. It was introduced by Joseph-Louis Lagrange in 1788.

It is used in continuum mechanics, when a continuum occupies a simply-connected region and is irrotational. In such a case, × u = 0 , {\displaystyle \nabla \times \mathbf {u} =0\,,} where u denotes the flow velocity. As a result, u can be represented as the gradient of a scalar function ϕ: u = φ   = φ x i + φ y j + φ z k . {\displaystyle \mathbf {u} =\nabla \varphi \ ={\frac {\partial \varphi }{\partial x}}\mathbf {i} +{\frac {\partial \varphi }{\partial y}}\mathbf {j} +{\frac {\partial \varphi }{\partial z}}\mathbf {k} \,.}

ϕ is known as a velocity potential for u.

A velocity potential is not unique. If ϕ is a velocity potential, then ϕ + f(t) is also a velocity potential for u, where f(t) is a scalar function of time and can be constant. Velocity potentials are unique up to a constant, or a function solely of the temporal variable.

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, it is often desirable to work with the acoustic wave equation of the velocity potential ϕ instead of pressure p and/or particle velocity u. 2 φ 1 c 2 2 φ t 2 = 0 {\displaystyle \nabla ^{2}\varphi -{\frac {1}{c^{2}}}{\frac {\partial ^{2}\varphi }{\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 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 \varphi }{\partial t}}\,.}

See also

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.

External links


Stub icon

This fluid dynamics–related article is a stub. You can help Misplaced Pages by expanding it.

Categories: