Experimental and numerical investigation of inclined air/SF6 interface instability under shock wave
Experimental and numerical investigation of inclined air/SF6 interface instability under shock wave
复制标题
冲击波作用下倾斜空气/SF6界面失稳的实验与数值研究
DOI:
10.1007/s10483-012-1532-x
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发表时间:
2012-01
期刊:
影响因子:
--
通讯作者:
Liu, Kun
中科院分区:
文献类型:
--
作者:
Wang, Tao;Liu, Jin-hong;Bai, Jing-song;Jiang, Yang;Li, Ping;Liu, Kun
The shock tube experiments of inclined air/SF6 interface instability under the shock wave with the Mach numbers 1.23 and 1.41 are conducted. The numerical simulation is done with the parallel algorithm and the multi-viscous-fluid and turbulence (MVFT) code of the large-eddy simulation (LES). The developing process of the interface accelerated by the shock wave is reproduced by the simulations. The complex wave structures, e.g., the propagation, refraction, and reflection of the shock wave, are clearly revealed in the flows. The simulated evolving images of the interface are consistent with the experimental ones. The simulated width of the turbulent mixing zone (TMZ) and the displacements of the bubble and the spike also agree well with the experimental data. Also, the reliability and effectiveness of the MVFT in simulating the problem of interface instability are validated. The more energies are injected into the TMZ when the shock wave has a larger Mach number. Therefore, the perturbed interface develops faster.
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影响因子:
4.6
作者:
J. Jacobs
通讯作者:
J. Jacobs
影响因子:
3
作者:
RICHTMYER, RD
通讯作者:
RICHTMYER, RD
影响因子:
4.6
作者:
J. Jacobs;J. Sheeley
通讯作者:
J. Jacobs;J. Sheeley
影响因子:
4.6
作者:
M. A. Jones;J. Jacobs
通讯作者:
M. A. Jones;J. Jacobs
DOI:
10.1016/j.physd.2007.04.023
发表时间:
2007-11
期刊:
Physica D: Nonlinear Phenomena
影响因子:
--
作者:
Sanjay Kumar;P. Vorobieff;G. Orlicz;A. Palekar;C. Tomkins;C. Goodenough;M. Marr‐Lyon;K. Prestridge-K.-P
通讯作者:
Sanjay Kumar;P. Vorobieff;G. Orlicz;A. Palekar;C. Tomkins;C. Goodenough;M. Marr‐Lyon;K. Prestridge-K.-P