Numerical Simulation of the Development of Perturbations Induced by a Periodic Heat Source in a Supersonic Boundary Layer
A. I. Kutepova, D. V. Khotyanovsky, A. A. Sidorenko
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences, Novosibirsk, Russia
Keywords: direct numerical simulation, shock wave - laminar boundary layer interaction, thermal source of perturbations
Abstract
Direct numerical simulation of interaction between a laminar boundary layer and a shock wave at a Mach number of 1.45 is performed. The influence of a periodic thermal source on the nature of this interaction is described.
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