Skip to main content

Derive differential continuity equation

Short answer

For a fixed cube, net mass outflow plus time-rate density change gives d(rho)/dt + div(rho V)=0. Steady flow drops the time term; incompressible flow becomes div V=0.

Derive the continuity equation in differential form for three-dimensional unsteady compressible flow in Cartesian coordinates. Reduce it for steady and for incompressible flow.

The continuity equation expresses conservation of mass: mass is neither created nor destroyed.

Derivation

Take a fixed small control volume (a cube) of sides dx, dy, dzdx,\ dy,\ dz with density ρ\rho and velocity components u,v,wu,v,w.

        y
        ^   +---------+
        |  /         /|
        | +---------+ |   mass in  : rho*u dy dz
        | |         | |   at x face
        | |         | +   mass out : [rho*u +
        | |         |/      d(rho*u)/dx dx] dy dz
        | +---------+
        +-------------> x

Net mass efflux in the x-direction:

[ρu+∂(ρu)∂xdx]dy dz−ρu dy dz=∂(ρu)∂xdx dy dz\left[\rho u+\frac{\partial(\rho u)}{\partial x}dx\right]dy\,dz-\rho u\,dy\,dz=\frac{\partial(\rho u)}{\partial x}dx\,dy\,dz

Similarly for y and z. Total net outflow of mass per unit time:

[∂(ρu)∂x+∂(ρv)∂y+∂(ρw)∂z]dx dy dz\left[\frac{\partial(\rho u)}{\partial x}+\frac{\partial(\rho v)}{\partial y}+\frac{\partial(\rho w)}{\partial z}\right]dx\,dy\,dz

Rate of decrease of mass inside the element is −∂ρ∂tdx dy dz-\dfrac{\partial\rho}{\partial t}dx\,dy\,dz. Equating the two and dividing by the volume:

∂ρ∂t+∂(ρu)∂x+∂(ρv)∂y+∂(ρw)∂z=0\frac{\partial\rho}{\partial t}+\frac{\partial(\rho u)}{\partial x}+\frac{\partial(\rho v)}{\partial y}+\frac{\partial(\rho w)}{\partial z}=0

or in vector form

∂ρ∂t+∇⋅(ρV⃗)=0\frac{\partial\rho}{\partial t}+\nabla\cdot(\rho\vec V)=0

Special cases

  • Steady flow (∂ρ/∂t=0\partial\rho/\partial t=0):
∂(ρu)∂x+∂(ρv)∂y+∂(ρw)∂z=0\frac{\partial(\rho u)}{\partial x}+\frac{\partial(\rho v)}{\partial y}+\frac{\partial(\rho w)}{\partial z}=0
  • Incompressible flow (ρ\rho constant):
∂u∂x+∂v∂y+∂w∂z=∇⋅V⃗=0\frac{\partial u}{\partial x}+\frac{\partial v}{\partial y}+\frac{\partial w}{\partial z}=\nabla\cdot\vec V=0

This means the velocity field is divergence-free, and volume is conserved for a fluid element.

✓ Answer checked by Claude Opus 5.5 (high effort)

All Applied Computational Fluid Dynamics chapter 2 questions →