2014
DOI: 10.1134/s106378501401026x
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Nonuniformity of the pressure wave formed during electric explosion of a foil

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“…The presented shock waves are calculated and explained in the model as being due to supersonic boundary conditions being taken into account. Shock waves were also observed in [7,9,55,56]. The shock waves are concentrated at the nozzle region and there are none in other regions.…”
Section: The Distribution Of Plasma Static Pressurementioning
confidence: 94%
“…The presented shock waves are calculated and explained in the model as being due to supersonic boundary conditions being taken into account. Shock waves were also observed in [7,9,55,56]. The shock waves are concentrated at the nozzle region and there are none in other regions.…”
Section: The Distribution Of Plasma Static Pressurementioning
confidence: 94%