4   Artículos

 
en línea
Oleg Vishnyakov, Pavel Polivanov and Andrey Sidorenko    
The paper focuses on the investigation of unsteady effects in shock wave/boundary layer interaction. The study was carried out using a flat plate model subjected to a free stream Mach number of 1.43 and a unit Reynolds number (Re1) of 11.5 × 106 1/m. To ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Pavel Polivanov, Oleg Vishnyakov and Andrey Sidorenko    
The problem of flow control under conditions of a turbulent boundary layer at transonic and supersonic free-stream velocities is considered. Such flows are integral components of the flight process and exert significant effects on the flow around both th... ver más
Revista: Aerospace    Formato: Electrónico

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