Stacking-sequence optimization of composite delta wing to improve flutter limit using fractal branch and bound method

JSME International Journal, Series A: Solid Mechanics and Material Engineering

Volumn 48, Issue 2, 2005, Pages 65-72

  Hirano, Yoshiyasu ^a   Todoroki, Akira ^b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b TOKYO INSTITUTE OF TECHNOLOGY   (Japan)

Author keywords

Composite material; Flutter; Optimum design; Response surface; Stacking sequence

Indexed keywords

APPROXIMATION THEORY; BUCKLING; FLUTTER (AERODYNAMICS); FRACTALS; OPTIMIZATION; POLYNOMIALS;

COMPOSITE DELTA WING; LAMINATION PARAMETERS; QUADRATIC POLYNOMIALS; STACKING SEQUENCES;

COMPOSITE MATERIALS;

BUCKLING;

EID: 21244447920     PISSN: 13447912     EISSN: None     Source Type: Journal    
DOI: 10.1299/jsmea.48.65     Document Type: Article

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