Zobrazeno 1 - 10
of 30
pro vyhledávání: '"Ivan Moralev"'
Publikováno v:
Aerospace, Vol 10, Iss 11, p 907 (2023)
The pulse electric arc discharge in an external magnetic field is studied as a vortex generator in the subsonic boundary layer. A pulsed Ampere force induces a hairpin vortex near the wall; its structure depends on the relative direction of arc propa
Externí odkaz:
https://doaj.org/article/9b864ee902614a3391d268401d4c7d67
Publikováno v:
Aerospace, Vol 10, Iss 5, p 469 (2023)
Cancellation of the cross-flow vortices in a swept-wing boundary layer is attempted by plasma actuator array in numerical simulation. The response of the boundary layer to the stationary excitation by a single actuator section is measured experimenta
Externí odkaz:
https://doaj.org/article/5d7df1a7f19f40e5b7eaa654faf5151d
Publikováno v:
SSRN Electronic Journal.
Publikováno v:
IUTAM Laminar-Turbulent Transition ISBN: 9783030679019
The distributed roughness element (DRE) conception based on dielectric barrier discharge (DBD) for the laminarization boundary layer of the swept wing was investigated. “Killer” mode was successfully excited and suppressed the development of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e4ad94703d6c60c3d527f87bd141722d
https://doi.org/10.1007/978-3-030-67902-6_12
https://doi.org/10.1007/978-3-030-67902-6_12
Autor:
Ivan Moralev, Maksim Ustinov, Alexander Kotvitskii, Ilya Popov, Igor Selivonin, Pavel Kazanskii
Publikováno v:
Physics of Fluids. 34:054117
Mechanism of hydrodynamic noise generation in a subsonic flat plate boundary layer by a barrier discharge plasma actuator is described. The origin of the pulsations is an inscintric unsteadiness of the discharge structure caused by wandering of the m
Autor:
Nikolay Popov, Svetlana Starikovskaia, Igor Selivonin, Chenyang Ding, Sergey Shcherbanev, Antonin Jean, Ivan Moralev
Publikováno v:
AIAA Scitech 2020 Forum Session: Plasma Assisted Combustion
AIAA Scitech 2020 Forum Session: Plasma Assisted Combustion, Jan 2020, Orlando, United States. ⟨10.2514/6.2020-1662⟩
AIAA Scitech 2020 Forum Session: Plasma Assisted Combustion, Jan 2020, Orlando, United States. ⟨10.2514/6.2020-1662⟩
International audience
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::fb8282f43ffd04f795b82f104c4c0fbd
https://hal.archives-ouvertes.fr/hal-03042117/document
https://hal.archives-ouvertes.fr/hal-03042117/document
Autor:
Ustinov Maxim, Igor Selivonin, Valentin Bityurin, Ivan Moralev, Alexander A. Firsov, Victoria Sherbakova
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 234:42-57
In this study, a new type of dielectric barrier discharge plasma actuator for boundary layer control, based on the controllable inhomogeneity of the discharge along the exposed electrode, is developed. The structure of the flow, generated by the isol
Publikováno v:
International Journal of Heat and Mass Transfer. 116:1326-1340
The effect of a dielectric barrier discharge at an increased power level on the structure of a two-dimensional subsonic boundary layer is studied. It is shown that the formation of high-current stationary filaments in the discharge plasma (constricti
Publikováno v:
Journal of Physics: Conference Series. 2100:012001
The paper describes the results of the parametric study of the broadband velocity pulsations, induced by DBD plasma actuator in 2D subsonic boundary layer. The presented data include the analysis of the disturbance growth at various pressure gradient
Publikováno v:
Experiments in Fluids. 60
Turbulence generation by plasma actuator is one of the key barriers on the way of their application as virtual roughness elements in boundary layer transition control. Recent application of these devices for the crossflow instability control has show