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The continuity equation of two- dimensional steady incompressible flow is_______

The question was posed to me in an interview for internship.

Question is from Turbulent Boundary Layer on a Flat Plate topic in portion Boundary Layer Flow & Forces on Sub-merged Bodies of Fluid Mechanics

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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


Explanation:

  1. Two-Dimensional Flow:

    • The flow has two velocity components: uu (velocity in the xx-direction) and vv (velocity in the yy-direction).
  2. Steady Flow:

    • The flow properties do not change with time, i.e., ∂∂t=0\frac{\partial}{\partial t} = 0.
  3. 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

For steady (∂ρ/∂t=0\partial \rho / \partial t = 0) and incompressible flow (ρ=constant\rho = \text{constant}):

∇⋅V⃗=0\nabla \cdot \vec{V} = 0

Expanding in two dimensions (V⃗=ui^+vj^\vec{V} = u \hat{i} + v \hat{j}):

∂u∂x+∂v∂y=0\frac{\partial u}{\partial x} + \frac{\partial v}{\partial y} = 0


This equation ensures that the fluid entering a region equals the fluid leaving it, maintaining mass conservation.

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