Boundary Layer Theory

By J. Spurk. Fluid Mechanics, 2019

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The boundary layer equations for plane, incompressible, and steady flow are $$\matrix{ {u{{\partial u} \over {\partial x}} + v{{\partial u} \over {\partial y}} = - {1 \over \varrho }{{\partial p} \over {\partial x}} + v{{{\partial ^2}u} \over {\partial {y^2}}},} \cr {0 = {{\partial p} \over {\partial y}},} \cr {{{\partial u} \over {\partial x}} + {{\partial v} \over {\partial y}} = 0.} \cr }$$

View Paper: https://www.semanticscholar.org/paper/540abb465fcc0fb4498e2d7c9aa92a1c4f58dc30

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