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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 of the Russian Academy of Sciences, Novosibirsk, Russia
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.
Keywords:
direct numerical simulation, shock wave – laminar boundary layer interaction, thermal source of perturbations.
Received: 19.04.2023 Revised: 25.04.2023 Accepted: 29.05.2023
Citation:
A. I. Kutepova, D. V. Khotyanovsky, A. A. Sidorenko, “Numerical simulation of the development of perturbations induced by a periodic heat source in a supersonic boundary layer”, Prikl. Mekh. Tekh. Fiz., 64:5 (2023), 139–143; J. Appl. Mech. Tech. Phys., 64:5 (2024), 853–857
Linking options:
https://www.mathnet.ru/eng/pmtf1816 https://www.mathnet.ru/eng/pmtf/v64/i5/p139
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Abstract page: | 39 | References: | 10 | First page: | 8 |
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