Bulletin of the American Physical Society
71st Annual Meeting of the APS Division of Fluid Dynamics
Volume 63, Number 13
Sunday–Tuesday, November 18–20, 2018; Atlanta, Georgia
Session F28: Flow Instability: Rayleigh-Taylor/Richtmyer-Meshkov I
8:00 AM–10:10 AM,
Monday, November 19, 2018
Georgia World Congress Center
Room: B316
Chair: Oleg Schilling, LLNL
Abstract ID: BAPS.2018.DFD.F28.1
Abstract: F28.00001 : The effect of initial conditions on the growth of Richtmyer–Meshkov instability
8:00 AM–8:13 AM
Presenter:
Mohammad M Mansoor
(Los Alamos National Laboratory)
Authors:
Mohammad M Mansoor
(Los Alamos National Laboratory)
Adam A Martinez
(Los Alamos National Laboratory)
Sean Dalton
(Los Alamos National Laboratory)
Tiffany Desjardins
(Los Alamos National Laboratory)
Katherine P Prestridge
(Los Alamos National Laboratory)
The baroclinic generation of vorticity at a stratified interface when subjected to a shock-wave occurs in a process known as the Richtmyer–Meshkov instability. This study investigates the growth of single-mode sinusoidal perturbations on an air/sulfur hexafluoride (SF6) interface by this process using a 7m tall vertical shock tube (1.2 Ma). The perturbations are induced by subjecting the interface to an undulating cross-flow structure produced by steady-state oscillations of a symmetrical motorized airfoil flapper in the cross-stream. For various flapper frequencies and sweeping angles employed, both the initial perturbation wavelength (λ0) and amplitude (η0) produced are noted to affect the late-time growth rates, significantly. The perturbation amplitude (η) follows a power-law dependence with downstream distance and can be collapsed for all flapper conditions by a dimensional-scaling k(η/ η0) = 0.21(kx)0.44 . Turbulent statistics of the mixing region in addition to vortex identification and swirl strength within are also investigated for obtaining correlations with the flapper oscillation characteristics.
To cite this abstract, use the following reference: http://meetings.aps.org/link/BAPS.2018.DFD.F28.1
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