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Volumn 69, Issue 2, 2003, Pages 239-244
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Stacking sequence optimizations of composites to improve panel flutter at supersonic flow using fractal branch and bound method
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Author keywords
Composites; Flutter; Optimizations; Response surface; Stacking sequence; Supersonic
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Indexed keywords
APPROXIMATION THEORY;
BUCKLING;
COMPOSITE STRUCTURES;
FLUTTER (AERODYNAMICS);
FRACTALS;
LAMINATED COMPOSITES;
OPTIMIZATION;
POLYNOMIALS;
STACKING FAULTS;
STRUCTURAL PANELS;
SUPERSONIC FLOW;
OBJECTIVE FUNCTION;
QUADRATIC POLYNOMIALS;
RESPONSE SURFACE;
STACKING SEQUENCE;
STRUCTURAL ANALYSIS;
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EID: 0038327876
PISSN: 03875008
EISSN: None
Source Type: Journal
DOI: 10.1299/kikaia.69.239 Document Type: Article |
Times cited : (6)
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References (12)
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