Parameters of transverse-longitudinal discharge in supersonic airflow

Parameters of transverse-longitudinal discharge in supersonic airflow

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 pla...

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Veröffentlicht in:Moscow University physics bulletin 2007-10, Vol.62 (5), p.326-328
Hauptverfasser: Aleksandrov, A. F., Ershov, A. P., Kolesnikov, E. B., Logunov, A. A., Chernikov, V. A., Shibkov, V. M.
Format: Artikel
Sprache:eng
Schlagworte:
Air flow
Discharge
Gas temperature
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Zusammenfassung: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.
ISSN:0027-1349
1934-8460
DOI:10.3103/S002713490705013X