|
Control of a flow in a supersonic boundary layer
I. I. Lipatovab, V. Kh. Phama a Moscow Institute of Physics and Technology (National Research University), Dolgoprudny, Moscow Region
b Central Aerohydrodynamic Institute
Abstract:
A method of flow control in a two-dimensional hypersonic boundary layer under strong viscous-inviscid interaction is considered. The effect of blocking the process of transferring disturbances upstream due to a decrease in the propagation velocity of disturbances with a decrease in the temperature factor of the surface area is shown.
Keywords:
asymptotic theory of viscous gas, controlling of flow, propagation of perturbations, viscous–inviscid interaction.
Received: 07.06.2019 Revised: 17.03.2020 Accepted: 17.03.2020
Citation:
I. I. Lipatov, V. Kh. Pham, “Control of a flow in a supersonic boundary layer”, Pisma v Zhurnal Tekhnicheskoi Fiziki, 46:11 (2020), 47–50; Tech. Phys. Lett., 46:6 (2020), 564–567
Linking options:
https://www.mathnet.ru/eng/pjtf5093 https://www.mathnet.ru/eng/pjtf/v46/i11/p47
|
Statistics & downloads: |
Abstract page: | 39 | Full-text PDF : | 18 |
|