1-Channel flow after a pulsed energy contribution in the region behind the shock front
2-Diffraction of a shock wave on a wedge-shaped model. 3D view
3-Diffraction of a shock wave on a wedge-shaped model. 2D view
4-Unsteady flow around a wedge after the passage of a shock wave. 3D view.
5-Interaction of two counterpropagating plane shock waves generated by pulsed surface discharges.
6-Pressure field during the passage of a shock wave through a channel with rectangular obstacles
7-A pulsed volume discharge occurs in front of the shock front. Above and below - shock waves formed by pulsed sheet discharges. Dуcay of the break.
8-A pulsed volume discharge occurs in front of the shock front. Above and below - shock waves formed by pulsed sheet discharges. Dуcay of the break.
9-The shock wave passes through the shock tube channel with a rectangular obstacle at the bottom of the channel.
10-animation_P_300
11. Motion of a plane shock wave with a Mach number of 2 along a warm layer formed as a result of a pulsed surface discharge of nanosecond duration of the "plasma sheet" type (3D and 2D)
12. Shock wave exit with Mach 1.5 from a rectangular channel (48 mm x 24 mm) (also 2D and 3D)