Plane blast wave propagation in air with a transverse thermal inhomogeneity

被引:5
|
作者
Sembian, S. [1 ]
Liverts, M. [1 ]
Apazidis, N. [1 ]
机构
[1] KTH Royal Inst Technol, Dept Mech, Stockholm, Sweden
基金
瑞典研究理事会;
关键词
Thermal inhomogeneity; Shock curvature; Shock broadening/splitting; Exploding wire; SHOCK-WAVE; SPLITTING SCHEME; GLOW-DISCHARGE; DYNAMICS; PLASMAS;
D O I
10.1016/j.euromechflu.2017.09.011
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
An alternate mechanism explaining the shock broadening and splitting effects observed during its propagation through an elongated region with transverse thermal inhomogeneity is described. The shock wave is generated by exploding wire technique and its propagation is captured optically using shadowgraph method. Visualizing the flow provided distinct advantage not only for obtaining detailed information on the propagation characteristics but also for validating the numerical scheme used in the analysis. Three physical features namely shock jump, precursor region and vorticity induced flow, are identified to contribute to the shock structure with the latter two being responsible for the pressure profile 'broadening'. The physical behavior of the incident shock is also analyzed along with other factors like temperature and curvature effects. (C) 2017 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:220 / 230
页数:11
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