Modelling for couplings of an airframe-propulsion integrated hypersonic vehicle with engine safety boundaries

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Volumn 224, Issue 1, 2010, Pages 43-55

  Yao, Z H ^a   Bao, W ^a   Chang, J ^a   Yu, D ^a   Tang, J ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

Burner flameout; Coupling; Hypersonic vehicle; Inlet unstart; Modelling; Safety boundary

Indexed keywords

AIR BREATHING; COUPLED DYNAMICS; FLIGHT CONTROL; FLIGHT VEHICLES; FUEL COMBUSTION; FUEL SUPPLY; GENERIC HYPERSONIC VEHICLES; HARBIN INSTITUTE OF TECHNOLOGY; INLET UNSTART; MULTIMODE CONTROL; NORMAL OPERATIONS; OPERATION MODE; PROPULSION CONTROL; SAFETY BOUNDARY; SAFETY OPERATIONS; UNSTART; WALL TEMPERATURES;

AIRFRAMES; AUTOMOBILE ENGINES; AUTOMOBILE PARTS AND EQUIPMENT; COMBUSTION; COUPLINGS; ENGINES; FLIGHT DYNAMICS; FUELS; HYPERSONIC AERODYNAMICS; HYPERSONIC INLETS; PROPULSION; STRUCTURAL FRAMES; VEHICLES;

HYPERSONIC VEHICLES;

EID: 74549208556     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/09544100JAERO618     Document Type: Article

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