The Rise of Forces on a Wedge during the Interaction of a Sliding Discharge with a Supersonic Flow

The force arising on a wedge during the interaction of a sliding discharge with a supersonic flow is investigated. The sliding discharge was created in a supersonic atmospheric-vacuum wind tunnel with Mach number M = 2, a Reynolds number of about 10 6 , and static pressure in the flow p = 0.15 bar....

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Veröffentlicht in:	Technical physics letters 2021-06, Vol.47 (6), p.436-439
Hauptverfasser:	Bocharnikov, V. M., Golub, V. V., Savel’ev, A. S.
Format:	Artikel
Sprache:	eng
Schlagworte:	Classical and Continuum Physics Discharge Flow control Fluid flow Mach number Physics Physics and Astronomy Reynolds number Sliding Static pressure Supersonic flow Wind tunnels
Online-Zugang:	Volltext
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