Hostname: page-component-76fb5796d-2lccl Total loading time: 0 Render date: 2024-04-26T06:35:43.694Z Has data issue: false hasContentIssue false

RFNC–VNIITF multifunctional shock tube for investigating the evolution of instabilities in nonstationary gas dynamic flows

Published online by Cambridge University Press:  03 March 2004

Yu.A. KUCHERENKO
Affiliation:
Russian Federal Nuclear Center, Academician E.I. Zababakhin, All-Russian Research Institute of Technical Physics (RFNC–VNIITF), Chelyabinsk, Russia
O.E. SHESTACHENKO
Affiliation:
Russian Federal Nuclear Center, Academician E.I. Zababakhin, All-Russian Research Institute of Technical Physics (RFNC–VNIITF), Chelyabinsk, Russia
S.I. BALABIN
Affiliation:
Russian Federal Nuclear Center, Academician E.I. Zababakhin, All-Russian Research Institute of Technical Physics (RFNC–VNIITF), Chelyabinsk, Russia
A.P. PYLAEV
Affiliation:
Russian Federal Nuclear Center, Academician E.I. Zababakhin, All-Russian Research Institute of Technical Physics (RFNC–VNIITF), Chelyabinsk, Russia

Abstract

The design, operation, and functionality of the multifunctional shock tube (MST) facility at the Russian Federal Nuclear Center–VNIITF are described. When complete, the versatile MST consists of three different driver sections that permit the execution of three different classes of experiments on the compressible turbulent mixing of gases induced by the (1) Richtmyer–Meshkov instability (generated by a stationary shock wave with shock Mach numbers <5), (2) Rayleigh–Taylor instability (generated by compression wave such that acceleration of the interface is <105g0, where g0 = 9.8 m/s2), and (3) combined Richtmyer–Meshkov and Rayleigh–Taylor instability (generated by a nonstationary shock wave with initial pressure at the front 5 × 106 Pa and acceleration of ≤106g0 of the interface). For each of these types of experiments, the density ratio of the gases is ρ21 ≤ 34. Perturbations are imposed on a thin membrane, embedded in a thin wire array of microconductors that is destroyed by an electric current. In addition, various limitations of experimental techniques used in the study of interfacial instability generated turbulent mixing are also briefly discussed.

Type
Research Article
Copyright
© 2003 Cambridge University Press

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

REFERENCES

Anuchina, N.N. et al. (1997). Three-dimensional numerical simulation of Rayleigh–Taylor instability by MAH-3 code. Proc. 6th Int. Workshop on Physics of Compressible Turbulent Mixing.
Kucherenko, Yu.A. et al. (1988). Experimental investigation of the gravitational turbulent mixing in self-similar mode. Rus. J. VANT, Series Theoretical and Applied Physics 1.
Kucherenko, Yu.A. et al. (1991). Experimental study of the gravitational turbulent mixing in self-similar mode. Proc. 3rd Int. Workshop on Physics of Compressible Turbulent Mixing.
Read, K. (1984). Experimental investigation of turbulent mixing by Rayleigh–Taylor instability. Physica D 12.Google Scholar
Vasilenko, A.M. et al. (1991). Experimental investigations for turbulent mixing of gases at the interface under the influence of the decelerating shock wave. Proc. 3rd Int. Workshop on Physics of Compressible Turbulent Mixing.
Youngs, D.L. (1991). Three-dimensional numerical simulation of turbulent mixing by Rayleigh–Taylor instability. Phys. Fluids A 3.Google Scholar
Zaitsev, S.G. et al. (2000). Evolution of the Rayleigh–Taylor instability in compressible media. Report under ISTC Project No. 96-029.