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Parameters of transverse-longitudinal discharge in supersonic airflow
Authors:A F Aleksandrov  A P Ershov  E B Kolesnikov  A A Logunov  V A Chernikov  V M Shibkov
Institution:(1) Department of Physical Electronics, Moscow State University, Leninskie gory, Moscow, 119992, Russia
Abstract:Plasma of transverse-longitudinal direct-current discharge in a supersonic aerodynamic channel with a reverse step is studied experimentally. For deposited powers of 2–3 kW, the gas temperature in the discharge achieves 2000 ± 500 K. The results obtained testify to the applicability of discharge plasma for the ignition of supersonic air-fuel flows.
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