The continuity equation for a two-dimensional steady incompressible flow is given by:
∂u∂x+∂v∂y=0\frac{\partial u}{\partial x} + \frac{\partial v}{\partial y} = 0∂x∂u+∂y∂v=0
Explanation:
Two-Dimensional Flow:
- The flow has two velocity components: uuu (velocity in the xxx-direction) and vvv (velocity in the yyy-direction).
Steady Flow:
- The flow properties do not change with time, i.e., ∂∂t=0\frac{\partial}{\partial t} = 0∂t∂=0.
Incompressible Flow:
- The density of the fluid remains constant, so mass conservation simplifies to the divergence of the velocity field being zero.
Derivation:
From the principle of conservation of mass:
∂ρ∂t+∇⋅(ρV⃗)=0\frac{\partial \rho}{\partial t} + \nabla \cdot (\rho \vec{V}) = 0∂t∂ρ+∇⋅(ρV)=0
For steady (∂ρ/∂t=0\partial \rho / \partial t = 0∂ρ/∂t=0) and incompressible flow (ρ=constant\rho = \text{constant}ρ=constant):
∇⋅V⃗=0\nabla \cdot \vec{V} = 0∇⋅V=0
Expanding in two dimensions (V⃗=ui^+vj^\vec{V} = u \hat{i} + v \hat{j}V=ui^+vj^):
∂u∂x+∂v∂y=0\frac{\partial u}{\partial x} + \frac{\partial v}{\partial y} = 0∂x∂u+∂y∂v=0
This equation ensures that the fluid entering a region equals the fluid leaving it, maintaining mass conservation.