Computational Simulation of Imploding Current Sheath Trajectory at the Radial Phase of Plasma Focus Performance
Commenced in January 2007
Frequency: Monthly
Edition: International
Paper Count: 32804
Computational Simulation of Imploding Current Sheath Trajectory at the Radial Phase of Plasma Focus Performance

Authors: R. Amrollahi, M. Habibi

Abstract:

When the shock front (SF) hits the central electrode axis of plasma focus device, a reflected shock wave moves radially outwards. The current sheath (CS) results from ionization of filled gas between two electrodes continues to compress inwards until it hits the out-going reflected shock front. In this paper the Lagrangian equations are solved for a parabolic shock trajectory yielding a first and second approximation for the CS path. To determine the accuracy of the approximation, the same problem is solved for a straight shock.

Keywords: Radial compression, Shock wave trajectory, Current sheath, Slog model.

Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1084688

Procedia APA BibTeX Chicago EndNote Harvard JSON MLA RIS XML ISO 690 PDF Downloads 1202

References:


[1] Mather J. W., Methods of Experimental Physics, P. 187(1971), 9B, Academic Press, New York
[2] Leopoldo Soto, New trends and future perspectives on plasma focus research, Plasma Physics and Control Fusion, 47,361-381(2005)
[3] Lee S., T. Y. Tou, S. P. Moo, et al, a simple facility for the teaching of plasma dynamics and plasma nuclear fusion, Am. J. Phys. 56,1,62- 68(1988)
[4] Freeman, N. C., On the Theory of Hypersonic Flow Past Plane and Axially Symmetric Bluff Bodies, J. Fluid Mech. A, 366-386 (1956).
[5] Freeman, N. C., On the Theory of Hypersonic Flow Past Plane and Axially Symmetric Bluff Bodies, J. Fluid Mech. A, 366-386 (1956).