Active magnetic control thermal protection device of hypersonic aircraft and flow field parameter calculation method

The invention belongs to the field of fluid mechanics flow control and the field of plasma physical application, and discloses an active magnetic control thermal protection device of a hypersonic aircraft and a flow field parameter calculation method. The device comprises an insulating layer, an ele...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	LUO SHICHAO, ZHANG ZHIGANG, CHANG YU, LEE HYUN, HU SHOUCHAO, WU LIYIN, HUANG CHENGYANG, KONG XIAOPING, LYU MINGLEI
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING PHYSICS
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