Integrated design method for inverted double-module mandibular inward rotation air inlet channel/cone-like forebody

The invention discloses an integrated design method for an inverted double-module mandibular inward turning air inlet channel/cone-like forebody, and relates to an air-breathing hypersonic aircraft. The method comprises the following steps: 1) designing conical precursor configuration; 2) designing...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	YOU YANCHENG, CHENG JIANRUI, ZHU CHENGXIANG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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