FIELD: aero-space engineering; supersonic and hypersonic flying vehicles.
SUBSTANCE: proposed method consists in change of structure of airflow over flying vehicle by supply of energy near surface of flying vehicle by means of plasma generator ensuring continuous discharge between electrodes or changing the plasma ignition frequency. At control of streamlining due to local action by energy, flying vehicle characteristics are followed-up in different modes.
EFFECT: enhanced efficiency of self-contained gas discharge generator.
7 cl, 5 dwg
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