WANG Tao, LIU Jin-hong, BAI Jing-song, JIANG Yang, LI Ping, LIU Kun. Experimental and Numerical Investigation of the Inclined Air/SF-6 Interface Instability Under Shock Wave[J]. Applied Mathematics and Mechanics, 2012, 33(1): 35-47. doi: 10.3879/j.issn.1000-0887.2012.01.004
Citation: WANG Tao, LIU Jin-hong, BAI Jing-song, JIANG Yang, LI Ping, LIU Kun. Experimental and Numerical Investigation of the Inclined Air/SF-6 Interface Instability Under Shock Wave[J]. Applied Mathematics and Mechanics, 2012, 33(1): 35-47. doi: 10.3879/j.issn.1000-0887.2012.01.004

Experimental and Numerical Investigation of the Inclined Air/SF-6 Interface Instability Under Shock Wave

doi: 10.3879/j.issn.1000-0887.2012.01.004
  • Received Date: 2011-01-18
  • Rev Recd Date: 2011-11-08
  • Publish Date: 2012-01-15
  • Shock tube experiments of inclined Air/SF-6 interface instability under shock wave with mach numbers 1.23 and 1.41 were conducted, and were numerically simulated by the parallel algorithm and code MVFT (multi-viscous-fluid and turbulence) of large-eddy simulation (LES). The developing process of interface accelerated by shock wave was reproduced by simulations, the complex waves structure, e.g. the propagation, refraction and reflection of shock wave were revealed clearly in flows. The simulated evolving images of interface are consistent with experimental ones. The simulated width of turbulent mixing zone (TMZ), the displacements of bubble and spike also agree well with the experimental data. And the reliability and effectiveness of MVFT to simulate this problem of interface instability are validated. The more energy is injected into the TMZ when the shock wave has a larger mach number, the perturbed interface is developing faster.
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