Interaction of a supersonic, radiatively cooled plasma jet with an ambient medium
Author(s) -
F. Suzuki-Vidal,
M. Bocchi,
S. V. Lebedev,
G. F. Swadling,
G. Burdiak,
S. N. Bland,
P. de Grouchy,
G. N. Hall,
A. J. Harvey-Thompson,
E. Khoory,
S. Patankar,
L. Pickworth,
J. Skidmore,
R. A. Smith,
J. P. Chittenden,
M. Krishnan,
R. Madden,
K. Wilson-Elliot,
A. Ciardi,
Adam Frank
Publication year - 2012
Publication title -
physics of plasmas
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.75
H-Index - 160
eISSN - 1089-7674
pISSN - 1070-664X
DOI - 10.1063/1.3685607
Subject(s) - supersonic speed , jet (fluid) , plasma , argon , atomic physics , shock (circulatory) , physics , shock wave , mach number , mechanics , nuclear physics , medicine
An experimental investigation into the interaction of a supersonic, radiatively cooled plasma jet with argon gas is presented. The jet is formed by ablation of an aluminum foil driven by a 1.4 MA, 250 ns current pulse in a radial foil Z-pinch configuration. The outflow consists of a supersonic (Mach number ∼3–5), dense (ion density ni ∼ 1018 cm−3), highly collimated (half-opening angle ∼2°−5°) jet surrounded by a lower density halo plasma moving with the same axial velocity as the jet. The addition of argon above the foil leads to the formation of a shock driven by the ablation of halo plasma, together with a bow-shock driven by the dense jet. Experimental data with and without the presence of argon are compared with three-dimensional, magneto-hydrodynamic simulations using the GORGON code.
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