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Дата последнего поиска статьи во внешних источниках: 10 июня 2020 г.
Аннотация:The influence of the creeping discharge on the air flow in the boundary layer and the adjoining region of a plate with a cylindrical wedge has been investigated experimentally. Experiments were carried out in a supersonic wind tunnel at a Mach number M = 3.0. The processes of initiation and propagation of such a discharge and boundary layer development on the above objects under the action of this discharge have been investigated. The data on the flow around a wedge-shape projection on the plate are presented.