Publicado 6 números por año
ISSN Imprimir: 1948-2590
ISSN En Línea: 1948-2604
ASYMPTOTIC THEORY OF BOUNDARY LAYER INTERACTION WITH A TRAVELING SHOCK WAVE
SINOPSIS
A theory on the interaction of a laminar boundary layer with a shock wave traveling upstream or downstream is created. A similarity parameter is found and solutions of several tasks are provided, allowing us to determine the dependence of the critical pressure difference causing the boundary layer separation on the speed of the shock wave movement. The essential difference in flow patterns with the movement of a wave downstream versus upstream is shown.
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