Feasibility of an experiment on clumping induced by the Crow instability along a shocked cylinder

Author:

Wadas M.1ORCID,LeFevre H.2ORCID,Elmore Y.3,Xie X.3ORCID,White W.3ORCID,Kuranz C.2ORCID,Johnsen E.3ORCID

Affiliation:

1. Department of Mechanical and Civil Engineering, California Institute of Technology 1 , Pasadena, California 91125, USA

2. Department of Nuclear Engineering & Radiological Sciences, University of Michigan 2 , Ann Arbor, Michigan 48109, USA

3. Department of Mechanical Engineering, University of Michigan 3 , Ann Arbor, Michigan 48109, USA

Abstract

The growth of three-dimensional perturbations subject to the Crow instability along a vortex dipole resulting from the passage of a shock wave through a heavy gaseous cylinder is examined numerically. A linear stability analysis is performed based on geometric parameters extracted from two-dimensional simulations to determine the range of unstable wavenumbers, which is found to extend from 0.0 to 1.3 when normalized by the core separation distance. The analysis is then verified by comparison to three-dimensional simulations, which clearly show the development of the instability and the pinch-off of the vortex dipole into isolated vortex rings, which manifest as clumps of the original cylinder material. A scaling law is developed to determine the relevant spatiotemporal scales of the instability development, which is then used to assess the feasibility of a high-energy-density experiment visualizing clump formation. Specifically, a shocked cylinder with an initial diameter of 100 μm consisting of a perturbation of approximate wavelength and amplitude of 600 and 10 μm, respectively, is expected to form clumps resulting from the Crow instability approximately 40 ns after it is shocked, with dynamics which can be readily visualized on the Omega EP laser facility.

Publisher

AIP Publishing

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