Research on integrated optimization design of hypersonic cruise vehicle

Aerospace Science and Technology

Volumn 12, Issue 7, 2008, Pages 567-572

  Che, Jing ^a   Tang, Shuo ^a  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

Airframe scramjet integration; Hypersonic cruise vehicle; Integrated optimization design; Multi objective genetic algorithms; Pareto front side

Indexed keywords

AERODYNAMICS; AIR; DYNAMICS; GAS DYNAMICS; GENETIC ALGORITHMS; HYPERSONIC AERODYNAMICS; MANEUVERABILITY; PARETO PRINCIPLE; PHASE STABILITY; RADAR CROSS SECTION; SIGNAL PROCESSING; SOLUTIONS; TIME VARYING SYSTEMS; VEHICLES;

AEROHEATING; AIR-BREATHING; AIRFRAME/SCRAMJET INTEGRATION; COMPARISON RESULTS; CRUISE PHASE; DESIGN VARIABLES; HYPERSONIC CRUISE VEHICLE; INTEGRATED OPTIMIZATION DESIGN; MULTI-OBJECTIVE GENETIC ALGORITHMS; OPTIMIZATION ALGORITHMS; OPTIMIZATION DESIGNS; OPTIMIZATION PROCESSES; PARETO FRONT SIDE; PARETO FRONTS; PARETO SOLUTIONS; SHAPE PARAMETERS; STATIC STABILITY; WAVE RIDERS; WIND-TUNNEL TESTING;

OPTIMIZATION;

EID: 51849102540     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2008.01.008     Document Type: Article

References (10)

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