Stacking sequence optimizations for composite laminates using fractal branch and bound method: Application for supersonic panel flutter problem with buckling load condition

Advanced Composite Materials: The Official Journal of the Japan Society of Composite Materials

Volumn 13, Issue 2, 2004, Pages 89-106

  Hirano, Yoshiyasu ^a   Todoroki, Akira ^a  

^a TOKYO INSTITUTE OF TECHNOLOGY   (Japan)

Author keywords

Composites; Flutter; Optimization; Response surface; Stacking sequence; Supersonic

Indexed keywords

APPROXIMATION THEORY; BUCKLING; FRACTALS; FUNCTIONS; LOADS (FORCES); OPTIMIZATION; PARAMETER ESTIMATION; POLYNOMIALS; STRENGTH OF MATERIALS; SUPERSONIC FLOW;

FLUTTER; RESPONSE SURFACE; STACKING SEQUENCE; SUPERSONIC;

LAMINATED COMPOSITES;

EID: 4444231566     PISSN: 09243046     EISSN: None     Source Type: Journal    
DOI: 10.1163/1568551041718044     Document Type: Article

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