Control of triple-shock configurations in high-speed flows over a cylindrically blunted plate in gases for different Mach numbers
Author:
Affiliation:
1. Dorodnicyn Computing Centre, Federal Research Center “Computer Science and Control” of Russian Academy of Sciences, Moscow, Russia
2. Joint Institute for High Temperatures of the Russian Academy of Sciences, Moscow, Russia
Publisher
SAGE Publications
Subject
Mechanical Engineering,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/0954410018795942
Reference18 articles.
1. Survey of Aerodynamic Drag Reduction at High Speed by Energy Deposition
2. Joule heating flow control methods for high-speed flows
3. Unsteady triple-shock configurations and vortex contact structures initiated by the interaction of an energy source with a shock layer in gases
4. Control of Triple-Shock Configurations and Vortex Structures Forming in High Speed Flows of Gaseous Media past an AD Body under the Action of External Energy Sources
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1. The Use of Spatially Multi-Component Plasma Structures and Combined Energy Deposition for High-Speed Flow Control: A Selective Review;Energies;2024-03-28
2. Near-surface gas discharge effect on a steady bow shock wave position in a supersonic flow past a cylindrically blunted body in the air;Physics of Fluids;2022-06
3. Dynamics of Shock Structure and Frontal Drag Force in a Supersonic Flow Past a Blunt Cone under the Action of Plasma Formation;Fluids;2021-11-04
4. Turbulent mixing and transition criteria of flows induced by hydrodynamic instabilities;Physics of Plasmas;2019-08
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