The Two-Parameter Integral Method for Unsteady Laminar Incompressible Boundary Layer over a Semi-Infinite Flat Plate

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概要

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• This paper deals with an unsteady laminar incompressible boundary layer over a semi-infinite plate set in motion impulsively, in order to elucidate an unsteady boundary layer which develops over a flat plate inserted into a shock tube. Expressing the velocity profiles in the boundary layer by polynomials with two unknown parameters (a boundary layer thickness and a form parameter) and dividing the boundary layer into two regions, there are obtained two momentum integrals, which are reduced to simultaneous differential equations. And the solutions making a smooth transition from upstream (Blasius'solution) to downstream (Rayleigh's solution) are obtained.

• 一般社団法人日本機械学会の論文

著者

• Akamatsu Teruaki

  Faculty Of Engineering Kyoto University

• Akamatsu Teruaki

  Faculty of Engineering, Kyoto University

関連論文

• The Two-Parameter Integral Method for Unsteady Laminar Incompressible Boundary Layer over a Semi-Infinite Flat Plate
• A Generalized Solution of Quasi-Steady Laminar Flat Plate Boundary Layer in a Shock Tube
• Effects of Shock Waves on Living Tissues : Numerical Analysis of a Propagating Pressure Wave toward Living Tissue

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