Computational and experimental investigation of plasma deflagration jets and detonation shocks in coaxial plasma accelerators

Journal Article · 22 February 2018 · Plasma Sources Science and Technology

DOI: https://doi.org/10.1088/1361-6595/aaabec · OSTI ID:1485496

Subramaniam, Vivek  ^[1]; Underwood, Thomas C. ^[2]; Raja, Laxminarayan L. ^[3]; Cappelli, Mark A. ^[2]

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1. Univ. of Texas, Austin, TX (United States). Dept. of Aerospace Engineering and Engineering Mechanics; Stanford University
2. Stanford Univ., CA (United States). Dept. of Mechanical Engineering
3. Univ. of Texas, Austin, TX (United States). Dept. of Aerospace Engineering and Engineering Mechanics

Here, we present a magnetohydrodynamic (MHD) numerical simulation to study the physical mechanisms underlying plasma acceleration in a coaxial plasma gun. Coaxial plasma accelerators are known to exhibit two distinct modes of operation depending on the delay between gas loading and capacitor discharging. Shorter delays lead to a high velocity plasma deflagration jet and longer delays produce detonation shocks. During a single operational cycle that typically consists of two discharge events, the plasma acceleration exhibits a behavior characterized by a mode transition from deflagration to detonation. The first of the discharge events, a deflagration that occurs when the discharge expands into an initially evacuated domain, requires a modification of the standard MHD algorithm to account for rarefied regions of the simulation domain. The conventional approach of using a low background density gas to mimic the vacuum background results in the formation of an artificial shock, inconsistent with the physics of free expansion. To this end, we present a plasma-vacuum interface tracking framework with the objective of predicting a physically consistent free expansion, devoid of the spurious shock obtained with the low background density approach. The interface tracking formulation is integrated within the MHD framework to simulate the plasma deflagration and the second discharge event, a plasma detonation, formed due to its initiation in a background prefilled with gas remnant from the deflagration. The mode transition behavior obtained in the simulations is qualitatively compared to that observed in the experiments using high framing rate Schlieren videography. The deflagration mode is further investigated to understand the jet formation process and the axial velocities obtained are compared against experimentally obtained deflagration plasma front velocities. The simulations are also used to provide insight into the conditions responsible for the generation and sustenance of the magnetic pinch. The pinch width and number density distribution are compared to experimentally obtained data to calibrate the inlet boundary conditions used to set up the plasma acceleration problem.

• Research Organization: Stanford Univ., CA (United States)
• Sponsoring Organization: USDOE National Nuclear Security Administration (NNSA)
• Grant/Contract Number: NA0002011
• OSTI ID: 1485496
• Journal Information: Plasma Sources Science and Technology, Journal Name: Plasma Sources Science and Technology Journal Issue: 2 Vol. 27; ISSN 1361-6595
• Publisher: IOP PublishingCopyright Statement
• Country of Publication: United States
• Language: English