Stacking sequence optimization to maximize the buckling load of blade-stiffened panels with strength constraints using the iterative fractal branch and bound method

Composites Part B: Engineering

Volumn 39, Issue 5, 2008, Pages 842-850

  Todoroki, Akira ^a   Sekishiro, Masato ^a  

^a TOKYO INSTITUTE OF TECHNOLOGY   (Japan)

Author keywords

A. Polymer matrix composites; B. Buckling; B. Strength; Stacking sequences

Indexed keywords

AEROSPACE ENGINEERING; BUCKLING; ITERATIVE METHODS; LAMINATES; OPTIMIZATION; POLYNOMIAL APPROXIMATION;

BUCKLING LOADS; CARBON FIBER REINFORCED POLYMER (CFRP); COMPUTATIONAL COSTS; STACKING SEQUENCES;

CARBON FIBER REINFORCED PLASTICS;

EID: 43049106866     PISSN: 13598368     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compositesb.2007.10.003     Document Type: Article

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