Volume 22 Issue 2
Apr 2015
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ZOU Li-Yong, LIU Jin-Hong, WANG Jian, HUANG Wen-Bin, TAN Duo-Wang, LIU Cang-Li. A Vertical Shock Tube for Experimental Studies on Interfacial Instability[J]. Chinese Journal of High Pressure Physics, 2008, 22(2): 197-202 . doi: 10.11858/gywlxb.2008.02.014
Citation: ZOU Li-Yong, LIU Jin-Hong, WANG Jian, HUANG Wen-Bin, TAN Duo-Wang, LIU Cang-Li. A Vertical Shock Tube for Experimental Studies on Interfacial Instability[J]. Chinese Journal of High Pressure Physics, 2008, 22(2): 197-202 . doi: 10.11858/gywlxb.2008.02.014

A Vertical Shock Tube for Experimental Studies on Interfacial Instability

doi: 10.11858/gywlxb.2008.02.014
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  • Corresponding author: ZOU Li-Yong
  • Received Date: 08 Jun 2007
  • Rev Recd Date: 25 Oct 2007
  • Publish Date: 05 Jun 2008
  • A new vertical shock tube was developed in order to investigate different stages of the development of hydrodynamic interfacial instability. The versatile shock tube permits the execution of three kinds of experiments on the turbulent mixing of fluids induced by the (1) Richtmyer-Meshkov instability at the gas-gas interface (initial perturbations are imposed on a thin nitrocellulose membrane), (2) Rayleigh-Taylor instability at the gas-liquid interface (acceleration of the contact boundary of different density fluids g12104 m/s2), and (3) combined Rayleigh-Taylor and Richtmyer-Meshkov instability at the gas-liquid interface (the first shock wave Mach number ranges from 1.05 to 2.5). The main benefits of such a facility are that it allows, first, to perform multiple experiments of interfacial instability and, second, to measure different transition phases from the beginning to the fully developed turbulent mixing stages.

     

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