Design studies of aeroelastic tailoring of forward-swept composite aircraft using hybrid genetic algorithm

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 2, Issue , 2003, Pages 803-812

  Wan, Zhiqiang ^a   Yang, Chao ^a   Zou, Congqing ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

CONSTRAINT THEORY; FIGHTER AIRCRAFT; FUSELAGES; GENETIC ALGORITHMS; OPTIMIZATION; WINGS;

AEROELASTIC TAILORING; AILERON; FORWARD SWEPT COMPOSITE AIRCRAFT; HYBRID ALGORITHM;

FLUTTER (AERODYNAMICS);

EID: 0043014647     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-1491     Document Type: Conference Paper

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