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Incompressible flow

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Revision as of 08:26, 12 September 2005

A flow is said to be incompressible if the density of a fluid element does not change during its motion. It is a property of the flow and not of the fluid. The rate of change of density of a material fluid element is given by the material derivative


\frac{D \rho}{D t} = \frac{\partial \rho}{\partial t} + u_j \frac{\partial \rho}{\partial x_j}

From the continuity equation we have


\frac{D \rho}{D t} = - \rho \frac{\partial u_j}{\partial x_j}

Hence the flow is incompressible if the divergence of the velocity field is identically zero. Note that the density field need not be uniform in an incompressible flow. All that is required is that the density of a fluid element should not change in time as it moves through space. For example, flow in the ocean can be considered to be incompressible even though the density of water is not uniform due to stratification.

Governing Equations

The Navier Stokes equations for incompressible flow are

  • Continuity equation


\frac{\partial u_j}{\partial x_j} = 0

  • Momentum equation


\frac{\partial u_i}{\partial t} + u_j \frac{\partial u_i}{\partial x_j} + \frac{1}{\rho} \frac{\partial p}{\partial x_i} = \nu \Delta u_i

  • Energy equation


\frac{\partial E}{\partial t} + u_j \frac{\partial E}{\partial x_j} = \Phi + \frac{1}{\rho} \frac{\partial}{\partial x_j} \left( k \frac{\partial T}{\partial x_j} \right)


where

  • \Delta is the Laplacian operator
  • E is the internal energy per unit mass
  • \Phi is the rate of dissipation of mechanical energy per unit mass


\Phi = \nu \left( \frac{\partial u_i}{\partial x_j} + \frac{\partial u_i}{\partial x_j} \right)
\left( \frac{\partial u_i}{\partial x_j} + \frac{\partial u_i}{\partial x_j} \right)

  • \nu is the kinematic viscosity
  • k is the coefficient of thermal conductivity
  • T is the temperature
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