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Formation of ion-acoustic shocks

Authors :
White, R. B
Fried, B. D
Coroniti, F. V
Source :
Physics of Fluids. 17
Publication Year :
1974
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1974.

Abstract

The formation of an ion-acoustic shock in a numerically modeled two-chamber double plasma device is investigated for a plasma of cold ions and isothermal Boltzmann electrons. An initial potential ramp applied to the driver chamber launches an ion-acoustic pulse into the target chamber which steepens into a shock. The quasi-steady shock structure agrees with observed double plasma shocks. An upper limit of Mach 1.6 is observed independent of the potential ramp magnitude, in agreement with theory.

Subjects

Subjects :
Physics, Plasma

Details

Language :
English
Volume :
17
Database :
NASA Technical Reports
Journal :
Physics of Fluids
Notes :
N00014-69-A-0200-4023, , NGL-05-007-190
Publication Type :
Report
Accession number :
edsnas.19740048716
Document Type :
Report
Full Text :
https://doi.org/10.1063/1.1694590