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Effects of shock waves on Rayleigh-Taylor instability
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10.1063/1.2201063
/content/aip/journal/pop/13/6/10.1063/1.2201063
http://aip.metastore.ingenta.com/content/aip/journal/pop/13/6/10.1063/1.2201063
View: Figures

Figures

Image of FIG. 1.
FIG. 1.

Rayleigh-Taylor flow at different time. (a) ; (b) ; (c) . Density ; equally spaced contour lines.

Image of FIG. 2.
FIG. 2.

Mach 6 shock interacting with a Rayleigh-Taylor flow. Shock hits the head of the RT interface at . From left to right, the Rayleigh-Taylor interface at (a) ; (b) ; (c) ; (d) . Density ; equally spaced contour lines.

Image of FIG. 3.
FIG. 3.

Mach 12 shock interacting with a Rayleigh-Taylor flow. Shock hits the head of the RT interface at . From left to right, the Rayleigh-Taylor interface at (a) ; (b) ; (c) ; (d) . Density ; equally spaced contour lines.

Image of FIG. 4.
FIG. 4.

Mach 18 shock interacting with a Rayleigh-Taylor flow. Shock hits the head of the RT interface at . From left to right, the Rayleigh-Taylor interface at (a) ; (b) ; (c) ; (d) . Density ; equally spaced contour lines.

Image of FIG. 5.
FIG. 5.

Mach 24 shock interacting with a Rayleigh-Taylor flow. Shock hits the head of the RT interface at . From left to right, the Rayleigh-Taylor interface at (a) ; (b) ; (c) ; (d) . Density ; equally spaced contour lines.

Image of FIG. 6.
FIG. 6.

(Color online) (a) The Rayleigh-Taylor flow at ; (b) Mach 12 shock hitting the Rayleigh-Taylor interface from the top, ; (c) Mach 12 shock hitting the Rayleigh-Taylor interface from the bottom, . The time when shock hits the RT interface is for both cases of the shock coming from the top and from the bottom. Density .

Image of FIG. 7.
FIG. 7.

(Color online) Mach 6 shock interacts with Rayleigh-Taylor flows. Top: shock just hits the head of the RT interface at ; bottom: shock just leaves the tail of the RT interface at . Left: temperature; middle: entropy; right: vorticity.

Image of FIG. 8.
FIG. 8.

Mach 6 shock interacts with Rayleigh-Taylor flows. 1D-cut pictures. .

Image of FIG. 9.
FIG. 9.

(Color online) Mach 24 shock interacts with Rayleigh-Taylor flows. Top: shock just hits the head of the RT interface at ; bottom: shock just leaves the tail of the RT interface at . Left: temperature; middle: entropy; right: vorticity.

Image of FIG. 10.
FIG. 10.

Mach 24 shock interacts with Rayleigh-Taylor flows. 1D-cut pictures. .

Image of FIG. 11.
FIG. 11.

(Color online) Shock interacts with Rayleigh-Taylor flows. Left: Mach 6 shock; right: Mach 24 shock. Top: shock just hits the head of the RT interface; bottom: shock just leaves the tail of the RT interface. Baroclinic vorticity source.

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/content/aip/journal/pop/13/6/10.1063/1.2201063
2006-06-14
2014-04-17
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752b84549af89a08dbdd7fdb8b9568b5 journal.articlezxybnytfddd
Scitation: Effects of shock waves on Rayleigh-Taylor instability
http://aip.metastore.ingenta.com/content/aip/journal/pop/13/6/10.1063/1.2201063
10.1063/1.2201063
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