2022
DOI: 10.1016/j.actaastro.2022.03.031
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Pulse volume discharge behind shock wave in channel flow with obstacle

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Cited by 8 publications
(4 citation statements)
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“…A rectangular obstacle was placed on the bottom wall of the test section in a supersonic flow. At a specific point in time, an electric discharge was switched on the lower wall of the test section initiating a shock wave spreading from the discharge [27]. Figure 3…”
Section: Methodsmentioning
confidence: 99%
“…A rectangular obstacle was placed on the bottom wall of the test section in a supersonic flow. At a specific point in time, an electric discharge was switched on the lower wall of the test section initiating a shock wave spreading from the discharge [27]. Figure 3…”
Section: Methodsmentioning
confidence: 99%
“…The resulting quasi-two-dimensional flow around an obstacle can be split by a set of unsteady gas-dynamic structures: a bow shock, an oblique shock, a recirculation zone in the obstacle leeward region, an expanding wave fan (Prandtl-Meyer fan), reattachment shock, etc. [14]. In front of the reflected shock wave, a bifurcated structure is formed due to the propagation of the reflected shock along the boundary layer that developed behind the incident shock wave (Fig.…”
Section: Numerical Simulationmentioning
confidence: 99%
“…A rectangular obstacle was placed on the bottom wall of the test section in a supersonic flow. At a specific point in time, an electric discharge was switched on the lower wall of the test section initiating a shock wave spreading from the discharge [27].…”
Section: Figure 2 Shock Tube Scheme and X-t Plot Of Gas Flow Developm...mentioning
confidence: 99%