Hypersonic aircraft surface temperature prediction method based on electronic transpiration cooling

The invention provides a hypersonic flight vehicle surface temperature prediction method based on electronic transpiration cooling, and relates to the technical field of aerospace, and the method comprises the steps: S1, building a geometric model of a target hypersonic flight vehicle, and setting a...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	HU FENG, WANG JIANGKUN, JIN HUA, SUI ZHUOCHEN, ZHANG SHAOJIE, MI ZHITONG, FENG SHUJIE
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING IMAGE DATA PROCESSING OR GENERATION, IN GENERAL PHYSICS
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