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Jan 2 nd, 2019

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For an incompressible flow \rho  = {\rm{constant}}\nabla  \cdot V is physically the time rate of change of volume of a moving fluid element per unit volume. For an incompressible flow, volume of a fluid element is constant, therefore \nabla  \cdot V = 0This can be also shown from continuity equation. Continuity equation is given as\frac{{\partial \rho }}{{\partial t}} + \nabla  \cdot \rho V = 0Since, for an incompressible flow, \rho  = {\rm{constant}} we have \frac{{\partial \rho }}{{\partial t}} = 0therefore the continuity equation becomes 0 + \nabla  \cdot \rho V = 0\nabla  \cdot V = \frac{0}{\rho } = 0For an irrotational flow, velocity potential \phi is defined as V = \nabla \phi Therefore, a flow which is both incompressible and irrotational the equation can be written as \nabla .\left( {\nabla \phi } \right) = 0{\nabla ^2}\phi  = 0This equation {\nabla ^2}\phi  = 0 is called the Laplace’s equation.In Cartesian coordinates \phi  = \phi \left( {x,y,z} \right) therefore{\nabla ^2}\phi  = \frac{{{\partial ^2}\phi }}{{\partial {x^2}}} + \frac{{{\partial ^2}\phi }}{{\partial {y^2}}} + \frac{{{\partial ^2}\phi }}{{\partial {z^2}}} = 0Also, u = \frac{{\partial \psi }}{{\partial y}},v =  – \frac{{\partial \psi }}{{\partial x}}For an incompressible and irrotational flow \frac{{\partial v}}{{\partial x}} – \frac{{\partial u}}{{\partial y}} = 0\frac{\partial }{{\partial x}}\left( { – \frac{{\partial \psi }}{{\partial x}}} \right) – \frac{\partial }{{\partial y}}\left( {\frac{{\partial \psi }}{{\partial y}}} \right) = 0 \Rightarrow \frac{{{\partial ^2}\psi }}{{\partial {x^2}}} + \frac{{{\partial ^2}\psi }}{{\partial {y^2}}} = 0Therefore, velocity potential as well as stream functions both satisfies Laplace’s equation, for an incompressible and irrotational flow.

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