Computer Science
Scientific paper
Dec 1979
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1979ge%26ae..19..994s&link_type=abstract
Geomagnetizm i Aeronomiia, vol. 19, Nov.-Dec. 1979, p. 994-1000. In Russian.
Computer Science
Environment Simulation, Magnetohydrodynamic Flow, Near Wakes, Nonequilibrium Plasmas, Rarefied Plasmas, Supersonic Flow, Aerodynamics, Ionospheric Currents, Plasma Jet Wind Tunnels, Plasma Jets, Spheres
Scientific paper
A plasma wind tunnel was used to study the near wake of a sphere in the supersonic flow of a nonequilibrium rarefied plasma; the experiment was conducted with a view to investigating the features of wakes of flight vehicles in the ionospheric plasma. The plasma source parameter values were as follows: discharge current of 8 A; discharge voltage of 120 V; maximum magnetic field strength at the source axis of 650 Oe. Experimental data are compared with numerical results for two wake models.
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