Affiliation:
1. Department of Aerospace and Mechanical Engineering, University of Arizona, Tucson, AZ 85721
Abstract
AbstractExperiments were performed to observe the growth of the turbulent, Rayleigh–Taylor unstable mixing layer generated between air and SF6, with an Atwood number of A=(ρ2−ρ1)/(ρ2+ρ1)=0.64, where ρ1 and ρ2 are the densities of air and SF6, respectively. A nonconstant acceleration with an average value of 2300g0, where g0 is the acceleration due to gravity, was generated by interaction of the interface between the two gases with a rarefaction wave. Three-dimensional, multimode perturbations were generated on the diffuse interface, with a diffusion layer thickness of δ=3.6 mm, using a membraneless vertical oscillation technique, and 20 experiments were performed to establish a statistical ensemble. The average perturbation from this ensemble was extracted and used as input for a numerical simulation using the Lawrence Livermore National Laboratory (LLNL) Miranda code. Good qualitative agreement between the experiment and simulation was observed, while quantitative agreement was best at early to intermediate times. Several methods were used to extract the turbulent growth constant α from experiments and simulations while accounting for time varying acceleration. Experimental, average bubble and spike asymptotic self-similar growth rate values range from α=0.022 to α=0.032 depending on the method used, and accounting for variable acceleration. Values found from the simulations range from α=0.024 to α=0.041. Values of α measured in the experiments are lower than what are typically measured in the literature but are more in line with those found in recent simulations.
Reference46 articles.
1. Investigation of the Character of the Equilibrium of an Incompressible Heavy Fluid of Variable Density;Proc. London Math Soc.,1883
2. The Instability of Liquid Surfaces When Accelerated in a Direction Perpendicular to Their Planes 1;Proc. R. Soc. A,1950
3. Fuel Gain Exceeding Unity in an Inertially Confined Fusion Implosion;Nature,2014
4. Direct-Drive Target Designs for the National Ignition Facility;LLE Rev. Q.,1999
5. The Experimental Plan for Cryogenic Layered Target Implosions on the National Ignition Facility—The Inertial Confinement Approach to Fusion;Phys. Plasmas,2011
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