Transition from Regular to Mach Reflection of Shock Waves in Laterally Colliding Laser-Produced Plasmas

被引:0
|
作者
Shilpa, S. [1 ]
Gopinath, Pramod [1 ,2 ]
机构
[1] Cochin Univ Sci & Technol, Int Sch Photon, Kochi 682022, India
[2] Cochin Univ Sci & Technol, Inter Univ Ctr Nanomat & Devices, Kochi 682022, India
关键词
laterally colliding laser-produced plasmas; regular reflection; Mach reflection; Mach stem length; DYNAMICS; INTERPENETRATION; PLUMES;
D O I
10.3103/S1541308X23060092
中图分类号
O4 [物理学];
学科分类号
0702 ;
摘要
Shock wave reflections in laterally colliding laser-produced aluminum plasmas at 10(-1) and 1 mbar argon ambient has been studied using fast imaging technique. In 10(-1) mbar pressure regime, the two shock fronts interact to form an intense interaction region. In the case of 1 mbar pressure regime, at early stages of plume expansion, individual shock fronts interact to form a collision front resulting in regular reflection of shock waves. At later times, the collision front split and a channel-like structure was observed and the width of the channel increases with time which is the cause of Mach reflection of shock waves. Incident angle and Mach stem length were measured from ICCD images, and it is found that Mach stem length increases with angle of incidence and time delay. Thus, the transition from regular reflection to Mach reflection of shock waves is reported in this paper.
引用
收藏
页码:434 / 441
页数:8
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